1833:
dislocation motion. This high APB energy makes it so that a second dislocation has to undo the APB energy created by the first. In doing so, this significantly reduces the mobility of dislocations in the material which should inhibit dislocation activated creep. These dislocation pairs (also called superdislocations) have been described as being either weakly or strongly coupled, the spacing between the dislocations compared to the size of the particle diameter being the determining factor between weak and strong. A weakly coupled dislocation has a relatively large spacing between the dislocations compared to the particle diameter while a strongly coupled dislocation has a relatively comparable spacing compared to the particle diameter. This is determined not by the dislocation spacing, but by the size of the 𝛾’ particles. A weakly coupled dislocation occurs when the particle size is relatively small while a strongly coupled dislocation occurs when the particle size is relatively large (such as when a superalloy has been aged for too long). Weakly coupled dislocations exhibit pinning and bowing of the dislocation line on the 𝛾’-particles. Strongly coupled dislocation behavior depends greatly on the dislocation line lengths and the resistances benefits they offer disappear once the particle size becomes large enough.
2048:, and nickel-chromium. For aluminide bond coatings, the coating's final composition and structure depends on the substrate composition. Aluminides lack ductility below 750 °C, and exhibit limited thermomechanical fatigue strength. Pt-aluminides are similar to the aluminide bond coats except for a layer of Pt (5—10 μm) deposited on the blade. The Pt aids in oxide adhesion and contributes to hot corrosion, increasing blade lifespan. MCrAlY does not strongly interact with the substrate. Normally applied by plasma spraying, MCrAlY coatings from secondary aluminum oxides. This means that the coatings form an outer chromia layer and a secondary alumina layer underneath. These oxide formations occur at high temperatures in the range of those that superalloys usually encounter. The chromia provides oxidation and hot-corrosion resistance. The alumina controls oxidation mechanisms by limiting oxide growth by self-passivating. The yttrium enhances oxide adherence to the substrate, and limits the growth of grain boundaries (which can lead to coat flaking). Addition of rhenium and tantalum increases oxidation resistance.
351:
dispersion between these known as secondary γ'. In order to improve the oxidation resistance of these alloys, Al, Cr, B, and Y are added. The Al and Cr form oxide layers that passivate the surface and protect the superalloy from further oxidation while B and Y are used to improve the adhesion of this oxide scale to the substrate. Cr, Fe, Co, Mo and Re all preferentially partition to the γ matrix while Al, Ti, Nb, Ta, and V preferentially partition to the γ' precipitates and solid solution strengthen the matrix and precipitates respectively. In addition to solid solution strengthening, if grain boundaries are present, certain elements are chosen for grain boundary strengthening. B and Zr tend to segregate to the grain boundaries which reduces the grain boundary energy and results in better grain boundary cohesion and ductility. Another form of grain boundary strengthening is achieved through the addition of C and a carbide former, such as Cr, Mo, W, Nb, Ta, Ti, or Hf, which drives precipitation of carbides at grain boundaries and thereby reduces grain boundary sliding.
1699:
temperature (~750 °C), SX alloys exhibits mostly primary creep behavior. Matan et al. concluded that the extent of primary creep deformation depends strongly on the angle between the tensile axis and the <001>/<011> symmetry boundary. At temperatures above 850 °C, tertiary creep dominates and promotes strain softening behavior. When temperature exceeds 1000 °C, the rafting effect is prevalent where cubic particles transform into flat shapes under tensile stress. The rafts form perpendicular to the tensile axis, since γ phase is transported out of the vertical channels and into the horizontal ones. Reed et al. studied unaxial creep deformation of <001> oriented CMSX-4 single crystal superalloy at 1105 °C and 100 MPa. They reported that rafting is beneficial to creep life since it delays evolution of creep strain. In addition, rafting occurs quickly and suppresses the accumulation of creep strain until a critical strain is reached.
2027:(TBCs) are used extensively in gas turbine engines to increase component life and engine performance. A coating of about 1-200 μm can reduce the temperature at the superalloy surface by up to 200 K. TBCs are a system of coatings consisting of a bond coat, a thermally grown oxide (TGO), and a thermally insulating ceramic top coat. In most applications, the bond coat is either a MCrAlY (where M=Ni or NiCo) or a Pt modified aluminide coating. A dense bond coat is required to provide protection of the superalloy substrate from oxidation and hot corrosion attack and to form an adherent, slow-growing surface TGO. The TGO is formed by oxidation of the aluminum that is contained in the bond coat. The current (first generation) thermal insulation layer is composed of 7wt %
2031:(7YSZ) with a typical thickness of 100–300 μm. Yttria-stabilized zirconia is used due to its low thermal conductivity (2.6W/mK for fully dense material), relatively high coefficient of thermal expansion, and high temperature stability. The electron beam-directed vapor deposition (EB-DVD) process used to apply the TBC to turbine airfoils produces a columnar microstructure with multiple porosity levels. Inter-column porosity is critical to providing strain tolerance (via a low in-plane modulus), as it would otherwise spall on thermal cycling due to thermal expansion mismatch with the superalloy substrate. This porosity reduces the thermal coating's conductivity.
1647:, a budget material with compromised temperature range and chemical resistance. It does not contain rhenium or ruthenium and its nickel content is limited. To reduce fabrication costs, it was chemically designed to melt in a ladle (though with improved properties in a vacuum crucible). Conventional welding and casting is possible before heat-treatment. The original purpose was to produce high-performance, inexpensive bomb casings, but the material has proven widely applicable to structural applications, including armor.
1165:
2056:/cobalt can be used due to excellent resistance to abrasion, corrosion, erosion, and heat. These cermet coatings perform well in situations where temperature and oxidation damage are significant concerns, such as boilers. One of cobalt cermet's unique advantages is minimal loss of coating mass over time, due to the strength of carbides. Overall, cermet coatings are useful in situations where mechanical demands are equal to chemical demands. Nickel-chromium coatings are used most frequently in boilers fed by
2287:). They comprise over 50% of the weight of advanced aircraft engines. The widespread use of superalloys in turbine engines coupled with the fact that the thermodynamic efficiency of turbine engines is a function of increasing turbine inlet temperatures has provided part of the motivation for increasing the maximum-use temperature of superalloys. From 1990-2020, turbine airfoil temperature capability increased on average by about 2.2 °C/year. Two major factors have made this increase possible:
900:(Ti,Al) are ordered systems with Ni atoms at the cube faces and either Al or Ti atoms at the cube edges. As particles of γ' precipitates aggregate, they decrease their energy states by aligning along the <100> directions forming cuboidal structures. This phase has a window of instability between 600 °C and 850 °C, inside of which γ' will transform into the HCP η phase. For applications at temperatures below 650 °C, the γ" phase can be utilized for strengthening.
124:
905:
1906:
2347:
2221:
27:
2064:, and waste incineration furnaces, where the danger of oxidizing agents and corrosive compounds in the vapor must be addressed. The specific method of spray-coating depends on the coating composition. Nickel-chromium coatings that also contain iron or aluminum provide better corrosion resistance when they are sprayed and laser glazed, while pure nickel-chromium coatings perform better when thermally sprayed exclusively.
519:, or carbides. GCP phases usually benefit mechanical properties, but TCP phases are often deleterious. Because TCP phases are not truly close packed, they have few slip systems and are brittle. Also they "scavenge" elements from GCP phases. Many elements that are good for forming γ' or have great solid solution strengthening may precipitate TCPs. The proper balance promotes GCPs while avoiding TCPs.
1967:" into a solid object with physically merged grains. Sintering occurs below the melting point, and causes adjacent particles to merge at their boundaries, creating a strong bond between them. In hot isostatic pressing, a sintered material is placed in a pressure vessel and compressed from all directions (isostatically) in an inert atmosphere to affect densification.
1785:, effectively halting further oxidation beneath this layer. In the ideal case, oxidation proceeds through two stages. First, transient oxidation involves the conversion of various elements, especially the majority elements (e.g. nickel or cobalt). Transient oxidation proceeds until the selective oxidation of the sacrificial element forms a complete barrier layer.
1991:
and a new batch of metal powder is rolled over the top. This layer is then sintered with the laser, and the process is repeated until all slices have been processed. Additive manufacturing can leave pores behind. Many products undergo a heat treatment or hot isostatic pressing procedure to densify the product and reduce porosity.
2319:. Because Carnot efficiency is limited by the temperature difference between the hot and cold reservoirs, higher operating temperatures increase energy conversion efficiency. Operating temperatures are limited by superalloys, limiting applications to around 1000 °C-1400 °C. Energy applications include:
2016:(EB-PVD). Thermal barrier coatings provide by far the best enhancement in working temperature and coating life. It is estimated that modern TBC of thickness 300 μm, if used in conjunction with a hollow component and cooling air, has the potential to lower metal surface temperatures by a few hundred degrees.
1615:) and improving high temperature performance and increasing service temperatures by 30 °C and 60 °C in second and third generation superalloys, respectively. Re promotes the formation of rafts of the γ' phase (as opposed to cuboidal precipitates). The presence of rafts can decrease creep rate in the
1640:
studies noted an opposite effect. Chen, et al., found that in two alloys differing significantly only in Ru content (USTB-F3 and USTB-F6) that the addition of Ru increased both the partitioning ratio as well as supersaturation in the γ matrix of Cr and Re, and thereby promoted the formation of TCP phases.
2298:
About 60% of the temperature increases related to advanced cooling, while 40% have resulted from material improvements. State-of-the-art turbine blade surface temperatures approach 1,150 C. The most severe stress and temperature combinations correspond to an average bulk metal temperature approaching
2159:
Thermal spraying involves heating a feedstock of precursor material and spraying it on a surface. Specific techniques depend on desired particle size, coat thickness, spray speed, desired area, etc. Thermal spraying relies on adhesion to the surface. As a result, the surface of the superalloy must be
1076:
The two major types of austenitic stainless steels are characterized by the oxide layer that forms on the steel surface: either chromia-forming or alumina-forming. Cr-forming stainless steel is the most common type. However, Cr-forming steels do not exhibit high creep resistance at high temperatures,
2431:
Stainless steel alloys remain a research target because of lower production costs, as well as the need for an austenitic stainless steel with high-temperature corrosion resistance in environments with water vapor. Research focuses on increasing high-temperature tensile strength, toughness, and creep
2186:
Failure of thermal barrier coating usually manifests as delamination, which arises from the temperature gradient during thermal cycling between ambient temperature and working conditions coupled with the difference in thermal expansion coefficient of substrate and coating. It is rare for the coating
2011:
or platinum-aluminide, is the most common. MCrAlX-based overlay coatings (M=Ni or Co, X=Y, Hf, Si) enhance resistance to corrosion and oxidation. Compared to diffusion coatings, overlay coatings are more expensive, but less dependent on substrate composition, since they must be carried out by air or
1832:
One of the main strengths of superalloys are their superior creep resistant properties when compared to most conventional alloys. To start, 𝛾’-strengthened superalloys have the benefit of requiring dislocations to move in pairs due to the phase creating a high antiphase boundary (APB) energy during
1064:
Gamma (γ): Fe-based alloys feature a matrix phase of austenite iron (FCC). Alloying elements include: Al, B, C, Co, Cr, Mo, Ni, Nb, Si, Ti, W, and Y. Al (oxidation benefits) must be kept at low weight fractions (wt.%) because Al stabilizes a ferritic (BCC) primary phase matrix, which is undesirable,
1990:
file. A shape is designed and then converted into slices. These slices are sent to a laser writer to print the final product. In brief, a bed of metal powder is prepared, and a slice is formed in the powder bed by a high energy laser sintering the particles together. The powder bed moves downwards,
1896:
is a metallurgical processing technique in which a wax form is fabricated and used as a template for a ceramic mold. A ceramic mold is poured around the wax form and solidifies, the wax form is melted out of the ceramic mold, and molten metal is poured into the void left by the wax. This leads to a
1884:
Jet turbine engines employ both crystalline component types to take advantage of their individual strengths. The disks of the high-pressure turbine, which are near the central hub of the engine are polycrystalline. The turbine blades, which extend radially into the engine housing, experience a much
985:
Co-based superalloys depend on carbide precipitation and solid solution strengthening for mechanical properties. While these strengthening mechanisms are inferior to gamma prime (γ') precipitation strengthening, cobalt has a higher melting point than nickel and has superior hot corrosion resistance
1848:
Diffusion is also a method of creep, and there are a few ways to limit diffusional creep. One primary way that superalloys can limit diffusional creep is by manipulating grain structure to reduce grain boundaries which tend to be pathways for easy diffusion. Typically this is done by manufacturing
1686:
Single crystal (SX) superalloys have wide application in the high-pressure turbine section of aero- and industrial gas turbine engines due to the unique combination of properties and performance. Since introduction of single crystal casting technology, SX alloy development has focused on increased
880:
Gamma (γ): This phase composes the matrix of Ni-based superalloy. It is a solid solution fcc austenitic phase of the alloying elements. The alloying elements most found in commercial Ni-based alloys are, C, Cr, Mo, W, Nb, Fe, Ti, Al, V, and Ta. During the formation of these materials, as they cool
844:
The United States became interested in gas turbine development around 1905. From 1910-1915, austenitic ( γ phase) stainless steels were developed to survive high temperatures in gas turbines. By 1929, 80Ni-20Cr alloy was the norm, with small additions of Ti and Al. Although early metallurgists did
2459:
reported a 3D-printed superalloy composed of 42% aluminum, 25% titanium, 13% niobium, 8% zirconium, 8% molybdenum and 4% tantalum. Most alloys are made chiefly of one primary element, combined with low amounts of other elements. In contrast MPES have substantial amounts of three or more elements.
1541:
At elevated temperature, the free energy associated with the anti-phase boundary (APB) is considerably reduced if it lies on a particular plane, which by coincidence is not a permitted slip plane. One set of partial dislocations bounding the APB cross-slips so that the APB lies on the low-energy
1080:
Al-forming austenitic stainless steels feature a single-phase matrix of austenite iron (FCC) with an Al-oxide at the surface of the steel. Al is more thermodynamically stable in oxygen than Cr. More commonly, however, precipitate phases are introduced to increase strength and creep resistance. In
2177:
Gas phase coating is carried out at higher temperatures, about 1080 °C. The coating material is usually loaded onto trays without physical contact with the parts to be coated. The coating mixture contains active coating material and activator, but usually not thermal ballast. As in the pack
1844:
For Ni-based single-crystal superalloys, upwards of ten different kinds of alloying additions can be seen to improve creep-resistance and overall mechanical properties. Alloying elements include Cr, Co, Al, Mo, W, Ti, Ta, Re, and Ru. Elements such as Co, Re, and Ru have been described to improve
2168:
Plasma spraying offers versatility of usable coatings, and high-temperature performance. Plasma spraying can accommodate a wide range of materials, versus other techniques. As long as the difference between melting and decomposition temperatures is greater than 300 K, plasma spraying is viable.
1836:
Additionally, superalloys exhibit comparatively superior high temperature creep resistance due to thermally activated cross-slip of dislocations. When one of the dislocations in the pair cross-slips into another plane, the dislocations become pinned since they can no longer move as a pair. This
2463:
Such alloys promise improvements on high-temperature applications, strength-to-weight, fracture toughness, corrosion and radiation resistance, wear resistance, and others. They reported ratio of hardness and density of 1.8–2.6 GPa-cm/g, which surpasses all known alloys, including intermetallic
1639:
additions, making them more expensive than prior Re-containing alloys. The effect of Ru on the promotion of TCP phases is not well-determined. Early reports claimed that Ru decreased the supersaturation of Re in the matrix and thereby diminished the susceptibility to TCP phase formation. Later
1149:. An excess of vacancies in one of the sublattices may exist, which leads to deviations from stoichiometry. Sublattices A and B of the γ' phase can solute a considerable proportion of other elements. The alloying elements are dissolved in the γ phase. The γ' phase hardens the alloy through the
1021:
Gamma (γ): This is the matrix phase. While Co-based superalloys are less-used commercially, alloying elements include C, Cr, W, Ni, Ti, Al, Ir, and Ta. As in stainless steels, Chromium is used (occasionally up to 20 wt.%) to improve resistance to oxidation and corrosion via the formation of a
350:
promote the creation of the γ' phase. The γ' phase size can be precisely controlled by careful precipitation strengthening heat treatments. Many superalloys are produced using a two-phase heat treatment that creates a dispersion of cuboidal γ' particles known as the primary phase, with a fine
1916:
uses a thermal gradient to promote nucleation of metal grains on a low temperature surface, as well as to promote their growth along the temperature gradient. This leads to grains elongated along the temperature gradient, and significantly greater creep resistance parallel to the long grain
1897:
metal form in the same shape as the original wax form. Investment casting leads to a polycrystalline final product, as nucleation and growth of crystal grains occurs at numerous locations throughout the solid matrix. Generally, the polycrystalline product has no preferred grain orientation.
1698:
The creep deformation behavior of superalloy single crystal is strongly temperature-, stress-, orientation- and alloy-dependent. For a single-crystal superalloy, three modes of creep deformation occur under regimes of different temperature and stress: rafting, tertiary, and primary. At low
848:
Although Cr was great for protecting the alloys from oxidation and corrosion up to 700 °C, metallurgists began decreasing Cr in favor of Al, which had oxidation resistance at much higher temperatures. The lack of Cr caused issues with hot corrosion, so coatings needed to be developed.
2187:
to fail completely – some pieces remain intact, and significant scatter is observed in the time to failure if testing is repeated under identical conditions. Various degradation mechanisms affect thermal barrier coating, and some or all of these must operate before failure finally occurs:
1939:
is a class of modern processing techniques in which metals are first powdered, and then formed into the desired shape by heating below the melting point. This is in contrast to casting, which occurs with molten metal. Superalloy manufacturing often employs powder metallurgy because of its
1845:
creep resistance by facilitating the formation of stacking faults by reducing the stacking fault energy. Increasing number of stacking faults leading to the inhibition of dislocation motion. Other elements (Al, Ti, Ta) can favorably partition into and improve the nucleation of 𝛾’-phase.
2278:
Nickel-based superalloys are used in load-bearing structures requiring the highest homologous temperature of any common alloy system (Tm = 0.9, or 90% of their melting point). Among the most demanding applications for a structural material are those in the hot sections of
247:(Ni)-based superalloys are the material of choice for these applications because of their unique γ' precipitates. The properties of these superalloys can be tailored to a certain extent through the addition of various other elements, common or exotic, including not only
1880:
Casting and forging are traditional metallurgical processing techniques that can be used to generate both polycrystalline and monocrystalline products. Polycrystalline casts offer higher fracture resistance, while monocrystalline casts offer higher creep resistance.
1796:(e.g. if oxygen diffuses too quickly). If the layer is not continuous, its effectiveness as a diffusion barrier to oxygen is compromised. The stability of the oxide layer is strongly influenced by the presence of other minority elements. For example, the addition of
2039:
The bond coat adheres the thermal barrier to the substrate. Additionally, the bond coat provides oxidation protection and functions as a diffusion barrier against the motion of substrate atoms towards the environment. The five major types of bond coats are: the
956:
Carbide phases: Carbide formation is usually deleterious although in Ni-based superalloys they are used to stabilize the structure of the material against deformation at high temperatures. Carbides form at the grain boundaries, inhibiting grain boundary
1840:
Increasing the lattice misfit between 𝛾/𝛾' has also been shown to be beneficial for creep resistance. This is primarily since a high lattice misfit between the two phases results in a higher barrier to dislocation motion than a low lattice misfit.
1378:
between identical dislocations along the same plane is repulsive, which makes this a less favorable configuration. One possible mechanism involved one of the dislocations being pinned against the γ' phase while the other dislocation in the γ phase
2302:
Although Ni-based superalloys retain significant strength to 980 C, they tend to be susceptible to environmental attack because of the presence of reactive alloying elements. Surface attack includes oxidation, hot corrosion, and thermal fatigue.
1077:
especially in environments with water vapor. Exposure to water vapor at high temperatures can increase internal oxidation in Cr-forming alloys and rapid formation of volatile Cr (oxy)hydroxides, both of which can reduce durability and lifetime.
1595:
Modern superalloys were developed in the 1980s. First generation superalloys incorporated increased Al, Ti, Ta, and Nb content in order to increase the γ' volume fraction. Examples include: PWA1480, René N4 and SRR99. Additionally, the
1168:
Viewed from a <111> direction, this is the effect of a dislocation along <110> passing through the respective structures. Note how the APB swaps the order of the supercell of alternating nickel and aluminum atoms above the
1081:
Al-forming steels, NiAl precipitates are introduced to act as Al reservoirs to maintain the protective alumina layer. In addition, Nb and Cr additions help form and stabilize Al by increasing precipitate volume fractions of NiAl.
1748:
Selective oxidation is the primary strategy used to limit these deleterious processes. The ratio of alloying elements promotes formation of a specific oxide phase that then acts as a barrier to further oxidation. Most commonly,
1623:
phases, which has led to the strategy of reducing Co, W, Mo, and particularly Cr. Later generations of Ni-based superalloys significantly reduced Cr content for this reason, however with the reduction in Cr comes a reduction in
2464:
compounds, titanium aluminides, refractory MPEAs, and conventional Ni-based superalloys. This represents a 300% improvement over
Inconel 718 based on measured peak hardness of 4.5 GPa and density of 8.2 g/cm, (0.55 GPa-cm/g).
743:
The main issue with this phase is that it's not coherent with γ, but it is not inherently weak. It typically forms from decomposing γ'', but sometimes it's intentionally added in small amounts for grain boundary refinement.
543:(pronounced L-one-two), which means it has a certain atom on the face of the unit cell, and a certain atom on the corners of the unit cell. Ni-based superalloys usually present Ni on the faces and Ti or Al on the corners.
3240:
Brady, M. P.; Yamamoto, Y.; Santella, M. L.; Maziasz, P. J.; Pint, B. A.; Liu, C. T.; Lu, Z. P.; Bei, H. (July 2008). "The development of alumina-forming austenitic stainless steels for high-temperature structural use".
1030:
passive layer, which is critical for use in gas turbines, but also provides solid-solution strengthening due to the mismatch in the atomic radii of Co and Cr, and precipitation hardening due to the formation of MC-type
1823:
processes are common when operating environments include salts and sulfur compounds, or under chemical conditions that change dramatically over time. These issues are also often addressed through comparable coatings.
2178:
cementation process, gaseous aluminium chloride (or fluoride) is transferred to the surface of the part. However, in this case the diffusion is outwards. This kind of coating also requires diffusion heat treatment.
2150:
Pack cementation has reemerged when combined with other chemical processes to lower the temperatures of metal combinations and give intermetallic properties to different alloy combinations for surface treatments.
845:
not know it yet, they were forming small γ' precipitates in Ni-based superalloys. These alloys quickly surpassed Fe- and Co-based superalloys, which were strengthened by carbides and solid solution strengthening.
2100:
between the two metals. The surface alloy that is formed due to thermal-diffused ion migration has a metallurgical bond to the substrate and an intermetallic layer found in the gamma layer of the surface alloys.
2470:
The researchers acknowledged that the 3D printing process produces microscopic cracks when forming large parts, and that the feedstock includes metals that limit applicability in cost-sensitive applications.
1003:
The most recently discovered family of superalloys was computationally predicted by
Nyshadham et al. in 2017, and demonstrated by Reyes Tirado et al. in 2018. This γ' phase is W free and has the composition
1468:
1422:
2096:. The entire apparatus is placed inside a furnace and heated in a protective atmosphere to a lower than normal temperature that allows diffusion, due to the halide salts chemical reaction that causes a
2291:
Processing techniques that improved alloy cleanliness (thus improving reliability) and/or enabled the production of tailored microstructures such as directionally solidified or single-crystal material.
2748:
Rae, C.M.F.; Karunaratne, M.S.A.; Small, C.J.; Broomfield, R.W.; Jones, C.N.; Reed, R.C. (2000). "Topologically Close Packed Phases in an
Experimental Rhenium-Containing Single Crystal Superalloy".
1129:
Operating temperatures with oxidation in air and no water vapor are expected to be higher. In addition, an AFA superalloy grade exhibits creep strength approaching that of nickel alloy UNS N06617.
2435:
Oak Ridge
National Laboratory is researching austenitic alloys, achieving similar creep and corrosion resistance at 800 °C to that of other austenitic alloys, including Ni-based superalloys.
1536:
1604:
that enable grain boundaries to be entirely eliminated. Because the material contains no grain boundaries, carbides are unnecessary as grain boundary strengthers and were thus eliminated.
515:
Adding elements is usually helpful because of solid solution strengthening, but can result in unwanted precipitation. Precipitates can be classified as geometrically close-packed (GCP),
1478:
between these partial dislocations can further provide another obstacle to the movement of other dislocations, further contributing to the strength of the material. There are also more
4827:
Gell, M.; Vaidyanathan, K.; Barber, B.; Cheng, J.; Jordan, E. (1999). "Mechanism of spallation in platinum aluminide/electron beam physical vapor-deposited thermal barrier coatings".
1917:
direction. In polycrystalline turbine blades, directional solidification is used to orient the grains parallel to the centripetal force. It is also known as dendritic solidification.
2092:
Pack cementation is a widely used CVD technique that consists of immersing the components to be coated in a metal powder mixture and ammonium halide activators and sealing them in a
4206:
Graybill, Benjamin; Li, Ming; Malawey, David; Ma, Chao; Alvarado-Orozco, Juan-Manuel; Martinez-Franco, Enrique (18 June 2018). "Additive
Manufacturing of Nickel-Based Superalloys".
1068:
Gamma-prime (γ'): This phase is introduced as precipitates to strengthen the alloy. γ'-Ni3Al precipitates can be introduced with the proper balance of Al, Ni, Nb, and Ti additions.
976:
refractory elements (including Cr, Co, W, and Mo). These phases form as a result of kinetics after long periods of time (thousands of hours) at high temperatures (>750 °C).
1317:
1230:
1619:(controlled by dislocation climb), but can also potentially increase the creep rate if the dominant mechanism is particle shearing. Re tends to promote the formation of brittle
1508:
1258:
986:
and thermal fatigue. As a result, carbide-strengthened Co-based superalloys are used in lower stress, higher temperature applications such as stationary vanes in gas turbines.
342:
phase, when present in high volume fractions, increases the strength of these alloys due to its ordered nature and high coherency with the γ matrix. The chemical additions of
1928:
starts with a seed crystal that is used to template growth of a larger crystal. The overall process is lengthy, and machining is necessary after the single crystal is grown.
1542:
plane, and, since this low-energy plane is not a permitted slip plane, the dissociated dislocation is effectively locked. By this mechanism, the yield strength of γ' phase Ni
4765:
Mumm, D. R.; Evans, A. G.; Spitsberg, I. T. (2001). "Characterisation of a cyclic displacement instability for a thermally grown oxide in a thermal barrier coating system".
2636:
Shinagawa, K.; Omori, Toshihiro; Oikawa, Katsunari; Kainuma, Ryosuke; Ishida, Kiyohito (2009). "Ductility
Enhancement by Boron Addition in Co–Al–W High-temperature Alloys".
2333:
Alumina-forming stainless steel is weldable and has potential for use in automotive applications, such as for high temperature exhaust piping and in heat capture and reuse.
3775:
Matan, N.; Cox, D. C.; Carter, P.; Rist, M. A.; Rae, C. M. F.; Reed, R. C. (1999). "Creep of CMSX-4 superalloy single crystals: effects of misorientation and temperature".
2601:
Klein, L.; Shen, Y.; Killian, M. S.; Virtanen, S. (2011). "Effect of B and Cr on the high temperature oxidation behaviour of novel γ/γ'-strengthened Co-base superalloys".
2423:, it might be possible to expand research into other aspects of superalloys. Radiolysis produces polycrystalline alloys, which suffer from an unacceptable level of creep.
1264:
instead of FCC due to the substitution of aluminum into the vertices of the unit cell, the perfect burgers vector along that direction in γ' is twice that of γ. For the
4715:
Baufeld, B.; Bartsch, M.; Broz, P.; Schmucker, M. (2004). "Microstructural changes as postmortem temperature indicator in Ni-Co-Cr-Al-Y oxidation protection coatings".
996:
The next family of Co-based superalloys was discovered in 2015 by
Makineni et al. This family has a similar γ/γ' microstructure, but is W-free and has a γ' phase of Co
2854:
Doi, M.; Miki, D.; Moritani, T.; Kozakai, T. (2004). "Gamma/Gamma-Prime
Microstructure Formed by Phased Separation of Gamma-Prime Precipitates in a Ni-Al-Ti Alloy".
1369:
4980:
Mumm, D. R.; Watanabe, M.; Evans, A. G.; Pfaendtner, J. A. (2004). "The influence of test method on failure mechanisms and durability of a thermal barrier system".
1865:
allowed for fine control of the chemical composition of superalloys and reduction in contamination and in turn led to a revolution in processing techniques such as
1611:, for increased temperature capability. Re is a slow diffuser and typically partitions the γ matrix, decreasing the rate of diffusion (and thereby high temperature
1592:
technologies were introduced in the 1950s. This process significantly improved cleanliness, reduced defects, and increased the strength and temperature capability.
4897:
Schulz, U; Menzebach, M; Leyens, C; Yang, Y.Q (September 2001). "Influence of substrate material on oxidation behavior and cyclic lifetime of EB-PVD TBC systems".
4448:
Kawahara, Yuuzou (January 1997). "Development and application of high-temperature corrosion-resistant materials and coatings for advanced waste-to-energy plants".
1374:
It is thus rather energy prohibitive for the dislocation to enter the γ' phase unless there are two of them in close proximity along the same plane. However, the
1145:
are placed at the vertices of the cubic cell and form sublattice A. Ni atoms are located at centers of the faces and form sublattice B. The phase is not strictly
4920:
Chen, X; Wang, R; Yao, N; Evans, A.G; Hutchinson, J.W; Bruce, R.W (July 2003). "Foreign object damage in a thermal barrier system: mechanisms and simulations".
1999:
In modern gas turbines, the turbine entry temperature (~1750K) exceeds superalloy incipient melting temperature (~1600K), with the help of surface engineering.
1084:
At least 5 grades of alumina-forming austenitic (AFA) alloys, with different operating temperatures at oxidation in air + 10% water vapor have been realized:
3853:
Reed, R. C.; Matan, N.; Cox, D. C.; Rist, M. A.; Rae, C. M. F. (1999). "Creep of CMSX-4 superalloy single crystals: effects of rafting at high temperature".
1375:
504:
Refractory metals, added in small amounts for solid solution strengthening (and carbide formation). They are heavy, but have extremely high melting points.
1046:
Ta, though both W and Al integrate into these cuboidal precipitates. Ta, Nb, and Ti integrate into the γ' phase and are stabilize it at high temperatures.
1000:(Al,Mo,Nb). Since W is heavy, its elimination makes Co-based alloys increasingly viable in turbines for aircraft, where low density is especially valued.
4390:
Tawancy, H.M.; Abbas, N.M.; Bennett, A. (December 1994). "Role of Y during high temperature oxidation of an M-Cr-Al-Y coating on an Ni-base superalloy".
482:
Boron and zirconium provide strength to grain boundaries. This is not essential in single-crystal turbine blades, because there are no grain boundaries.
2080:, and physical vapor deposition. In most cases, after the coating process, near-surface regions of parts are enriched with aluminium in a matrix of the
4603:
Evans, A. G.; Mumm, D. R.; Hutchinson, J. W.; Meier, G. H.; Pettit, F. S. (2001). "Mechanisms controlling the durability of thermal barrier coatings".
4163:
Gu, D D; Meiners, W; Wissenbach, K; Poprawe, R (May 2012). "Laser additive manufacturing of metallic components: materials, processes and mechanisms".
1885:
greater centripetal force, necessitating creep resistance, typically adopting monocrystalline or polycrystalline with a preferred crystal orientation.
1837:
pinning reduces the ability for the dislocations to move in dislocation activated creep and improving the creep resistant properties of the material.
2893:
Dunand, David C. "Materials
Science & Engineering 435: High Temperature Materials". Northwestern University, Evanston. 25 February 2016. Lecture.
1788:
The protective effect of selective oxidation can be undermined. The continuity of the oxide layer can be compromised by mechanical disruption due to
2207:
Additionally, TBC life is sensitive to the combination of materials (substrate, bond coat, ceramic) and processes (EB-PVD, plasma spraying) used.
2007:
The three types of coatings are: diffusion coatings, overlay coatings, and thermal barrier coatings. Diffusion coatings, mainly constituted with
2664:
4792:
Mumm, D. R.; Evans, A. G. (2000). "On the role of imperfections in the failure of a thermal barrier coating made by electron beam deposition".
3682:
Chen, J. Y.; Feng, Q.; Sun, Z. Q. (October 2010). "Topologically close-packed phase promotion in a Ru-containing single crystal superalloy".
2294:
Alloy development resulting in higher temperature materials primarily through the additions of refractory elements such as Re, W, Ta, and Mo.
3927:
Klein, L.; Bauer, S.; Neumeier, S.; Göken, M.; Virtanan, S. (2011). "High temperature oxidation of γ/γ'-strengthened Co-based superalloys".
3567:"Analysis of dislocation structures after double shear creep deformation of CMSX6-superalloy single crystals at temperatures above 1000 °C"
1663:. The mechanical properties of most other alloys depend on the presence of grain boundaries, but at high temperatures, they participate in
5127:
Shahsavari, H. A.; Kokabi, A. H.; Nategh, S. (2007). "Effect of preweld microstructure on HAZ liquation cracking of Rene 80 superalloy".
1061:
Steel superalloys are of interest because some present creep and oxidation resistance similar to Ni-based superalloys, at far less cost.
953:
which, together with order hardening, are the primary strengthening mechanisms. The γ" phase is unstable above approximately 650 °C.
929:(BCT), and the phase precipitates as 60 nm by 10 nm discs with the (001) planes in γ" parallel to the {001} family in γ. These
925:
V and is used to strengthen Ni-based superalloys at lower temperatures (<650 °C) relative to γ'. The crystal structure of γ" is
4870:
Evans, A.G.; He, M.Y.; Hutchinson, J.W. (January 2001). "Mechanics-based scaling laws for the durability of thermal barrier coatings".
4555:
Niranatlumpong, P.; Ponton, C. B.; Evans, H. E. (2000). "The
Failure of Protective Oxides on Plasma-Sprayed NiCrAlY Overlay Coatings".
4524:
4367:
Warnes, Bruce Michael (January 2003). "Improved aluminide/MCrAlX coating systems for super alloys using CVD low activity aluminizing".
4341:
2443:
Development of AFA superalloys with a 35 wt.% Ni-base have shown potential for use in operating temperatures upwards to 1,100 °C.
1323:, which will need another such dislocation along the plane to restore order (as the sum of the two dislocations would have the perfect
2197:
Thermal stresses from mismatch in thermal expansion coefficient and growth stress due to the formation of thermally grown oxide layer;
1948:
is a process by which reinforcing particles are incorporated into the superalloy matrix material by repeated fracture and welding.
1719:
phases, generally at the alloy surface. If unmitigated, oxidation can degrade the alloy over time in a variety of ways, including:
1944:- typically much less waste metal must be machined away from the final product—and its ability to facilitate mechanical alloying.
1435:
1389:
1052:
Topologically Close-Packed (TCP) phases may appear in some Co-based superalloys, but embrittle the alloy and are thus undesirable.
5027:"Long-Term Oxidation of Candidate Cast Iron and Stainless Steel Exhaust System Alloys from 650 to 800 °C in Air with Water Vapor"
1383:
into close proximity of the pinned dislocation from another plane, allowing the pair of dislocations to push into the γ' phase.
3437:"On the formation of 〈010〉-dislocations in the γ′-phase of superalloy single crystals during high temperature low stress creep"
896:
structure. The γ' phase is coherent with the matrix of the superalloy having a lattice parameter that varies by around 0.5%. Ni
4413:
D. Chuanxian; H. Bingtang; L. Huiling (24 August 1984). "Plasma-sprayed wear-resistant ceramic and cermet coating materials".
5117:
4223:
3362:
3012:
Nyshadham, Chandramouli; Oses, Corey; Hansen, Jacob E.; Takeuchi, Ichiro; Curtarolo, Stefano; Hart, Gus L.W. (January 2017).
691:
This precipitate is coherent with γ'. It is the main strengthening phase in IN-718, but γ'' dissolves at high temperatures.
385:
Fe and Co have higher melting points than Ni and offer solid solution strengthening. Fe is also much cheaper than Ni or Co.
4742:
Nychka, J.A; Clarke, D.R (September 2001). "Damage quantification in TBCs by photo-stimulated luminescence spectroscopy".
4308:
Clarke, David R. (January 2003). "Materials selection guidelines for low thermal conductivity thermal barrier coatings".
3526:
Dodaran, M.; Ettefagh, A. Hemmasian; Guo, S. M.; Khonsari, M. M.; Meng, W. J.; Shamsaei, N.; Shao, S. (1 February 2020).
3175:
Suzuki, A.; Pollock, Tresa M. (2008). "High-temperature strength and deformation of γ/γ' two-phase Co–Al–W-base alloys".
2480:
864:
764:
This TCP is usually considered to have the worst mechanical properties. It is never desirable for mechanical properties.
197:
Superalloy development relies on chemical and process innovations. Superalloys develop high temperature strength through
91:
1632:
accompanying the decreased Cr contents. Examples of second generation superalloys include PWA1484, CMSX-4 and René N5.
3148:
Coutsouradis, D.; Davin, A.; Lamberigts, M. (April 1987). "Cobalt-based superalloys for applications in gas turbines".
1471:
63:
2985:
Makineni, S. K.; Nithin, B.; Chattopadhyay, K. (March 2015). "A new tungsten-free γ–γ' Co–Al–Mo–Nb-based superalloy".
323:
are some examples of the alloying additions used. Each addition serves a particular purpose in optimizing properties.
4964:
4539:
3759:
3644:
2871:
2765:
2585:
2386:
2260:
1049:
Carbide Phases: Carbides strengthen the alloy through precipitation hardening but decrease low-temperature ductility.
110:
1513:
1260:
slip plane initially in the γ phase, where it is a perfect dislocation in that FCC structure. Since the γ' phase is
4692:
Pint, B.A. (November 2004). "The role of chemical composition on the oxidation performance of aluminide coatings".
1635:
Third generation alloys include CMSX-10, and René N6. Fourth, fifth, and sixth generation superalloys incorporate
70:
2791:
1601:
856:
became commercialized, which allowed metallurgists to create higher purity alloys with more precise composition.
147:
with the ability to operate at a high fraction of its melting point. Key characteristics of a superalloy include
4483:
Longa, Y.; Takemoto, M. (July 1992). "High-Temperature Corrosion of Laser-Glazed Alloys in Na 2 SO 4 -V 2 O 5".
4098:
3917:. DMIC report 214. 1 March 1965. Defense Metals Information Center, Batelle Memorial Institute, Columbus, Ohio.
3380:"Dislocation network with pair-coupling structure in {111} γ/γ′ interface of Ni-based single crystal superalloy"
2072:
Several kinds of coating process are available: pack cementation process, gas phase coating (both are a type of
1479:
1034:
Gamma Prime (γ'): Constitutes the precipitate used to strengthen the alloy. It is usually close-packed with a L1
3291:
Muralidharan, G.; Yamamoto, Y.; Brady, M. P.; Walker, L. R.; Meyer III, H. M.; Leonard, D. N. (November 2016).
2368:
2242:
48:
5025:
Brady, M. P.; Muralidharan, G.; Leonard, D. N.; Haynes, J. A.; Weldon, R. G.; England, R. D. (December 2014).
3663:
381: Materials for Energy-Efficient Technology. Northwestern University, Evanston. 3 February 2015. Lecture.
77:
5199:
4120:
Atkinson, H. V.; Davies, S. (December 2000). "Fundamental aspects of hot isostatic pressing: An overview".
2404:
2312:
973:
719:
The phase is not the worst, but it is not as good as γ'. It can be useful in controlling grain boundaries.
379:
These elements form the base matrix γ phase of the superalloy. Ni is necessary because it also forms γ' (Ni
218:
198:
2311:
High temperature materials are valuable for energy conversion and energy production applications. Maximum
1065:
as it is inferior to the high temperature strength exhibited by an austenitic (FCC) primary phase matrix.
993:(Al, W). Mo, Ti, Nb, V, and Ta partition to the γ' phase, while Fe, Mn, and Cr partition to the matrix γ.
2364:
2238:
1267:
1180:
663:
There are many carbides, but they all provide dispersion strengthening and grain boundary stabilization.
202:
44:
4630:
Wright, P. K.; Evans, A. G. (1999). "Mechanisms governing the performance of thermal barrier coatings".
1485:
1235:
539:
The main GCP phase is γ'. Almost all superalloys are Ni-based because of this phase. γ' is an ordered L1
3210:
2028:
1913:
1866:
860:
59:
3527:
3436:
3378:
Ru, Yi; Li, Shusuo; Zhou, Jian; Pei, Yanling; Wang, Hui; Gong, Shengkai; Xu, Huibin (11 August 2016).
1104:
High Performance AFA Grade: (45-55)Fe-(25-30)Ni-(14-15)Cr(3.5-4.5)Al-(1-3)Nb-(0.02-0.1)Hf/Y wt.% base
2073:
2013:
1562:
1115:
750-1100 °C operating temperatures at oxidation in air + 10% water vapor, depending upon Ni wt.%
964:
refers to any member of a family of phases (including the σ phase, the χ phase, the μ phase, and the
5002:
4318:
2467:
The material is stable at 800 °C, hotter than the 570+ °C found in typical coal-based power plants.
546:
Another "good" GCP phase is γ''. It is also coherent with γ, but it dissolves at high temperatures.
335:
2452:
1862:
1586:
989:
Co's γ/γ' microstructure was rediscovered and published in 2006 by Sato et al. That γ' phase was Co
938:
926:
853:
1819:
Oxidation is the most basic form of chemical degradation superalloys may experience. More complex
4029:"Microstructural evolution and creep mechanisms in Ni-based single crystal superalloys: A review"
4028:
3987:
Tian, Sugui; Zhang, Jinghua; Xu, Yongbo; Hu, Zhuangqi; Yang, Hongcai; Wu, Xin (1 December 2001).
3476:"Nucleation of superlattice intrinsic stacking faults via cross-slip in nickel-based superalloys"
2357:
2231:
2061:
2024:
1975:
1320:
1158:
950:
516:
37:
2415:
synthesis to create alloys and superalloys. This process holds promise as a universal method of
884:
Gamma prime (γ'): This phase constitutes the precipitate used to strengthen the alloy. It is an
4997:
4313:
4060:
1983:
1960:
1744:
of key alloying elements, affecting mechanical properties and possibly compromising performance
1150:
969:
221:, which decrease creep resistance (even though they may provide strength at low temperatures).
2683:
2456:
1987:
1849:
the superalloys as single crystals oriented parallel to the direction of the applied force.
1429:
4956:
4345:
3900:
2863:
2757:
2524:
1861:
of cobalt base alloys significantly raised operating temperatures. The 1950s development of
1326:
5194:
5136:
4989:
4836:
4801:
4639:
4457:
4422:
4282:
4172:
4129:
3936:
3862:
3819:
3784:
3487:
3304:
3250:
3184:
3084:
3035:
2943:
2828:
2610:
256:
972:
stacking. TCP phases tend to be highly brittle and deplete the γ matrix of strengthening,
881:
from the melt, carbides precipitate, and at even lower temperatures γ' phase precipitates.
859:
In the 60s and 70s, metallurgists changed focus from alloy chemistry to alloy processing.
8:
5189:
1945:
1941:
1793:
1770:
1664:
1620:
1612:
1425:
961:
942:
240:
167:
152:
148:
5171:
5140:
4993:
4840:
4805:
4643:
4461:
4426:
4286:
4176:
4133:
3962:
3940:
3866:
3823:
3788:
3528:"Effect of alloying elements on the γ' antiphase boundary energy in Ni-base superalloys"
3491:
3474:
León-Cázares, F.D.; Schlütter, R.; Monni, F.; Hardy, M.C.; Rae, C.M.F. (December 2022).
3308:
3254:
3188:
3088:
3039:
2947:
2832:
2614:
1757:
are used in this role, because they form relatively thin and continuous oxide layers of
1687:
temperature capability, and major improvements in alloy performance are associated with
84:
5152:
5080:
5054:
4852:
4572:
4229:
4188:
4145:
3835:
3732:
3412:
3379:
3328:
3266:
3053:
3025:
2967:
2485:
2104:
The traditional pack consists of four components at temperatures below (750 °C):
1893:
1858:
1789:
1735:
4933:
4906:
4883:
4813:
4778:
4751:
4678:
4651:
4616:
4376:
4327:
3914:
3874:
3796:
3452:
2551:
2515:
Sims, C.T. (1984). "A History of Superalloy Metallurgy for Superalloy Metallurgists".
396:
Cr is necessary for oxidation and corrosion resistance; it forms a protective oxide Cr
5156:
5113:
5058:
5046:
4960:
4856:
4576:
4535:
4434:
4399:
4233:
4219:
4192:
4149:
4008:
3839:
3755:
3695:
3640:
3605:
3586:
3582:
3547:
3505:
3456:
3417:
3399:
3358:
3332:
3320:
3270:
3161:
2998:
2959:
2867:
2761:
2649:
2581:
1936:
1616:
231:
Superalloys have made much of very-high-temperature engineering technology possible.
3736:
3727:
3710:
3057:
2971:
1643:
The current trend is to avoid very expensive and very heavy elements. An example is
823:
This phase has typical TCP issues. It is never desirable for mechanical properties.
796:
This phase has typical TCP issues. It is never desirable for mechanical properties.
5144:
5038:
5007:
4952:
4929:
4902:
4879:
4844:
4809:
4774:
4747:
4724:
4701:
4697:
4674:
4647:
4612:
4564:
4492:
4469:
4465:
4430:
4395:
4372:
4323:
4290:
4211:
4184:
4180:
4137:
4041:
4000:
3944:
3896:
3870:
3827:
3792:
3722:
3691:
3578:
3543:
3539:
3495:
3448:
3407:
3391:
3312:
3258:
3192:
3157:
3128:
3092:
3043:
2994:
2951:
2904:
2859:
2836:
2753:
2727:
2695:
2645:
2618:
2547:
2520:
2420:
2097:
2081:
2077:
2053:
1782:
968:), which are not atomically close-packed but possess some close-packed planes with
946:
934:
5011:
4045:
3500:
3196:
3097:
3072:
3048:
3013:
2113:
Ferrous and non-ferrous powdered alloy: (Ti and/or Al, Si and/or Zn, B and/ or Cr)
1872:
Processing methods vary widely depending on the required properties of each item.
493:
Nb can form γ'', a strengthening phase at lower (below 700 °C) temperatures.
3948:
3071:
Reyes Tirado, Fernando L.; Perrin Toinin, Jacques; Dunand, David C. (June 2018).
2819:
Sabol, G. P.; Stickler, R. (1969). "Microstructure of Nickel-Based Superalloys".
2622:
2194:
Depletion of aluminum in bond coat due to oxidation and diffusion with substrate;
1680:
1672:
1659:
using a modified version of the directional solidification technique, leaving no
1597:
1261:
1164:
904:
868:
618:
The main strengthening phase. γ' is coherent with γ, which allows for ductility.
4534:. Park Ridge, NJ: Noyes Pub.; Norwich, NY: William Andrew Pub. pp. 77–107.
3989:"Features and effect factors of creep of single-crystal nickel-base superalloys"
3891:
Pettit, F.S.; Meier, G.H. (1984). "Oxidation and Hot Corrosion of Superalloys".
3672:
O'Hara, K. S., Walston, W. S., Ross, E. W., Darolia, R. US Patent 5482789, 1996.
3475:
2731:
2718:
Belan, Juraj (2016). "GCP and TCP Phases Presented in Nickel-base Superalloys".
1857:
Superalloys were originally iron-based and cold wrought prior to the 1940s when
4947:
Walston, W.S. (2004). "Coating and Surface Technologies for Turbine Airfoils".
4728:
4532:
Handbook of Hard Coatings: Deposition Technologies, Properties and Applications
3566:
3133:
3116:
2280:
2191:
Oxidation at the interface of thermal barrier coating and underlying bond coat;
1925:
1741:
1668:
1656:
1607:
Second and third generation superalloys introduce about 3 and 6 weight percent
1578:
1475:
1174:
1146:
5042:
4848:
4568:
4141:
4004:
3606:"Microstructure development of Nimonic 80A superalloys during hot deformation"
3316:
3262:
5183:
5148:
4294:
4086:
Superalloys II: High Temperature Materials for Aerospace and Industrial Power
4012:
3590:
3551:
3509:
3460:
3403:
2840:
2284:
1905:
1731:
1715:
involves chemical reactions of the alloying elements with oxygen to form new
885:
339:
3988:
2955:
1123:
750-850 °C operating temperatures at oxidation in air + 10% water vapor
1107:
850-900 °C operating temperatures at oxidation in air + 10% water vapor
1091:
750-800 °C operating temperatures at oxidation in air + 10% water vapor
615:
cubes, rounded cubes, spheres, or platelets (depending on lattice mismatch)
330:
motion within a crystal structure. In modern Ni-based superalloys, the γ'-Ni
4059:
Cambridge, Department of Materials Science and Metallurgy - University of.
3421:
2963:
2416:
2412:
2316:
2057:
1963:
are processing techniques used to densify materials from a loosely packed "
4215:
535:
usually form sharp plate or needle-like morphologies which nucleate cracks
239:
Because these alloys are intended for high temperature applications their
4665:
Wright, P. K. (1998). "Influence of cyclic strain on life of a PVD TBC".
4210:. College Station, Texas, USA: American Society of Mechanical Engineers.
2700:
2323:
Solar thermal power plants (stainless steel rods containing heated water)
1676:
1667:
and require other mechanisms. In many such alloys, islands of an ordered
1660:
1644:
1550:
1154:
965:
327:
228:. Creep is typically the lifetime-limiting factor in gas turbine blades.
225:
123:
1734:
through the introduction of oxide phases, promoting crack formation and
1319:
dislocation to enter the γ' phase, it will have to create a high energy
1099:
650 °C operating temperatures at oxidation in air + 10% water vapor
5081:"Heat-loving lightweight superalloy promises higher turbine efficiency"
3831:
2408:
2371: in this section. Unsourced material may be challenged and removed.
2245: in this section. Unsourced material may be challenged and removed.
1964:
1557:
series alloys in the 1940s. The early Nimonic series incorporated γ' Ni
1380:
1088:
AFA Grade: (50-60)Fe-(20-25)Ni-(14-15)Cr-(2.5-3.5)Al-(1-3)Nb wt.% base
930:
863:
was developed to allow columnar or even single-crystal turbine blades.
272:
217:. Superalloys are often cast as a single crystal in order to eliminate
171:
5050:
5026:
4496:
3395:
3324:
3292:
1581:
for additional grain boundary strength. Turbine blade components were
590:
The matrix phase, provides ductility and a structure for precipitates
471:= metal) carbides are the strengthening phase in the absence of γ'.
2538:
Carter, Tim J (April 2005). "Common failures in gas turbine blades".
2041:
2008:
1956:
1820:
1712:
1708:
1692:
1636:
1629:
1625:
292:
284:
252:
210:
175:
160:
156:
3659:
Dunand, David C. "High-Temperature Materials for Energy Conversion"
3014:"A computational high-throughput search for new ternary superalloys"
2346:
2220:
1600:
of the γ' precipitates increased to about 50–70% with the advent of
209:. Oxidation or corrosion resistance is provided by elements such as
26:
5110:
High Temperature Strain of Metals and Alloys: Physical Fundamentals
4208:
Volume 1: Additive Manufacturing; Bio and Sustainable Manufacturing
3030:
2684:"A Review on Superalloys and IN718 Nickel-Based INCONEL Superalloy"
1813:
1809:
1754:
1750:
1724:
423:, which provides oxidation resistance at higher temperature than Cr
347:
343:
308:
288:
280:
276:
260:
224:
The primary application for such alloys is in aerospace and marine
214:
206:
183:
1655:
Single-crystal superalloys (SX or SC superalloys) are formed as a
1096:
Low Nickel AFA Grade: 63Fe-12Ni-14Cr-2.5Al-0.6Nb-5Mn3Cu wt.% base
4509:
G. R. Heath, P. Heimgartner, G. Irons, R. Miller, S. Gustafsson,
4412:
3293:"Development of Cast Alumina-Forming Austenitic Stainless Steels"
3073:"γ+γ' microstructures in the Co-Ta-V and Co-Nb-V ternary systems"
1805:
1801:
1758:
1688:
1608:
1589:
1582:
1566:
1554:
1112:
Cast AFA Grade: (35-50)Fe-(25-35)Ni-14Cr-(3.5-4)Al-1Nb wt.% base
320:
304:
300:
296:
191:
187:
179:
4026:
Xia, Wanshun; Zhao, Xinbao; Yue, Liang; Zhang, Ze (April 2020).
2160:
cleaned and prepared, and usually polished, before application.
326:
Creep resistance is dependent, in part, on slowing the speed of
3473:
3290:
3070:
2093:
2049:
2045:
1679:-pinning behavior of grain boundaries, without introducing any
312:
268:
248:
244:
5024:
1707:
For superalloys operating at high temperatures and exposed to
4273:
Boone, D. H. (1986). "Physical vapour deposition processes".
2747:
1797:
1716:
1671:
phase sit in a matrix of disordered phase, all with the same
1142:
1120:
AFA superalloy (40-50)Fe-(30-35)Ni-(14-19)Cr-(2.5-3.5)Al-3Nb
415:
Al is the main γ' former. It also forms a protective oxide Al
316:
144:
128:
3752:
The Physics of creep : creep and creep-resistant alloys
3239:
2665:"Development of Single Crystal Superalloys: A Brief History"
2446:
1463:{\displaystyle {\frac {a}{6}}\left\langle 211\right\rangle }
1417:{\displaystyle {\frac {a}{2}}\left\langle 110\right\rangle }
338:
acts as a barrier to dislocation. For this reason, this γ;'
4979:
4826:
4714:
4061:"Designing for Creep Resistance - Nickel Based Superalloys"
3147:
3011:
2984:
2635:
2203:
Various other complicating factors during engine operation.
1986:
procedure used to create intricately detailed forms from a
1157:
dissociate in the γ' phase, leading to the formation of an
264:
4591:
Modelling of Plasma Spraying of Ceramic Films and Coatings
4263:(Materials Park, OH: The ASM Thermal Spray Society, 2004).
4162:
3603:
3525:
205:
from secondary phase precipitates such as gamma prime and
4896:
4593:, Ed. Vinenzini, Pub. Elsevier State Publishers B.V 1991.
4554:
3604:
Bombač, D.; Fazarinc, M.; Kugler, G.; Spajić, S. (2008).
532:
are surrounded by a "depletion zone" where there is no γ'
4602:
2600:
1546:
Al increases with temperature up to about 1000 °C.
3926:
3810:
Nabarro, Frank R. N. (1996). "Rafting in Superalloys".
2934:
Sato, J (2006). "Cobalt-Base High-Temperature Alloys".
2419:
formation. By developing an understanding of the basic
2052:-cermet-based coatings consisting of materials such as
1951:
5126:
3711:"New single crystal superalloys – overview and update"
3639:. Cambridge: Cambridge University Press. p. 121.
3211:"Review: precipitation in austenitic stainless steels"
2853:
1549:
Initial material selection for blade applications in
1516:
1488:
1438:
1392:
1329:
1270:
1238:
1183:
194:, MP98T, TMS alloys, and CMSX single crystal alloys.
4632:
Current Opinion in Solid State and Materials Science
2315:
is desired in such applications, in accord with the
2123:
Relatively inert filler powder (Al2O3, SiO2, or SiC)
1424:
family of dislocations are likely to decompose into
243:
and oxidation resistance are of primary importance.
4389:
4205:
3117:"A New Co-Base Superalloy Strengthened by γ' Phase"
917:
Gamma double prime (γ"): This phase typically is Ni
51:. Unsourced material may be challenged and removed.
4764:
4027:
3915:"Oxidation of Nickel- and Cobalt-Base Superalloys"
3774:
3749:
2326:Steam turbines (turbine blades and boiler housing)
2012:vacuum plasma spraying (APS/VPS) or electron beam
1530:
1502:
1462:
1432:, such as dislocations with burgers vector of the
1416:
1363:
1311:
1252:
1224:
1173:To give an example, consider a dislocation with a
960:Topologically close-packed (TCP) phases: The term
4869:
3564:
2432:resistance to compete with Ni-based superalloys.
1628:. Advanced coating techniques offset the loss of
522:TCP phase formation areas are weak because they:
5181:
4949:Superalloys 2004 (Tenth International Symposium)
4919:
3963:"Nickel based superalloy: dislocation structure"
3893:Superalloys 1984 (Fifth International Symposium)
3852:
3565:Mayr, C.; Eggeler, G.; Dlouhy, A. (March 1996).
2856:Superalloys 2004 (Tenth International Symposium)
2750:Superalloys 2000 (Ninth International Symposium)
2517:Superalloys 1984 (Fifth International Symposium)
584:Ni, Co, Fe and other elements in solid solution
4525:"Thermal Spraying and Detonation Gun Processes"
4025:
2929:
2927:
2925:
2688:Periodicals of Engineering and Natural Sciences
2200:Imperfections near thermally grown oxide layer;
1711:environments, oxidation behavior is a concern.
1565:in a γ matrix, as well as various metal-carbon
16:Alloy with higher durability than normal metals
5107:
4250:(Materials Park, OH: ASM International, 2002).
4119:
3750:Nabarro, F. R. N.; de Villiers, H. L. (1995).
3637:The Superalloys: Fundamentals and Applications
3110:
3108:
2578:The Superalloys: Fundamentals and Applications
1531:{\displaystyle \left\langle 110\right\rangle }
4482:
3986:
3434:
3174:
2818:
1900:
1792:or may be disrupted as a result of oxidation
1650:
4741:
3352:
2922:
2118:Halide salt activator: Ammonium halide salts
1723:sequential surface oxidation, cracking, and
716:may form cellular or Widmanstätten patterns
4629:
4099:"PIM International Vol. 7 No. 1 March 2013"
3890:
3681:
3377:
3353:Laughlin, David E.; Hono, Kazuhiro (2014).
3105:
2329:Heat exchangers for nuclear reactor systems
2019:
660:string-like clumps, like strings of pearls
4829:Metallurgical and Materials Transactions A
4122:Metallurgical and Materials Transactions A
3993:Metallurgical and Materials Transactions A
3812:Metallurgical and Materials Transactions A
3708:
3634:
3435:Eggeler, G.; Dlouhy, A. (1 October 1997).
2681:
2575:
2044:, the platinum-aluminides, MCrAlY, cobalt-
1869:of alloys and single crystal superalloys.
829:
526:have inherently poor mechanical properties
5001:
4791:
4317:
4101:. Powder Injection Moulding International
3886:
3884:
3726:
3653:
3499:
3411:
3132:
3096:
3047:
3029:
2902:
2889:
2887:
2885:
2883:
2785:
2783:
2781:
2779:
2777:
2699:
2580:. Cambridge: Cambridge University Press.
2447:Multi-principal-element superalloy (MPES)
2387:Learn how and when to remove this message
2261:Learn how and when to remove this message
1970:
111:Learn how and when to remove this message
4447:
4344:. University of Virginia. Archived from
2814:
2812:
2810:
2808:
2789:
2571:
2569:
2567:
2565:
2563:
2561:
1920:
1904:
1163:
903:
122:
4946:
4589:P. Fauchais, A. Vardelle, M. Vardelle,
3809:
1909:Schematic of directional solidification
1781:), respectively. They offer low oxygen
234:
5182:
4664:
4522:
4366:
4307:
4248:Protective Coatings for Turbine Blades
3881:
3709:Wahl, Jacqueline; Harris, Ken (2014).
3348:
3346:
3344:
3342:
2903:Institute, Cobalt (14 February 2018).
2880:
2774:
2662:
2537:
1875:
587:The background for other precipitates
5078:
5074:
5072:
5070:
5068:
4957:10.7449/2004/Superalloys_2004_579_588
4272:
4058:
3901:10.7449/1984/Superalloys_1984_651_687
3666:
3521:
3519:
3357:(5th ed.). Amsterdam: Elsevier.
3286:
3284:
3282:
3280:
3235:
3233:
3231:
2864:10.7449/2004/Superalloys_2004_109_114
2805:
2758:10.7449/2000/Superalloys_2000_767_776
2717:
2671:: 26–30 – via asminternational.
2558:
2525:10.7449/1984/Superalloys_1984_399_419
2181:
1888:
1602:monocrystal solidification techniques
4922:Materials Science and Engineering: A
4691:
4261:Handbook of Thermal Spray Technology
3571:Materials Science and Engineering: A
2933:
2743:
2741:
2713:
2711:
2514:
2510:
2508:
2506:
2504:
2502:
2500:
2369:adding citations to reliable sources
2340:
2306:
2243:adding citations to reliable sources
2214:
1952:Sintering and hot isostatic pressing
1931:
1808:to superalloys promotes oxide layer
892:(Ti,Al) which have an ordered FCC L1
49:adding citations to reliable sources
20:
3661:Materials Science & Engineering
3339:
3114:
2792:"Superalloys: A Primer and History"
2481:Oxide dispersion strengthened alloy
2426:
2154:
2087:
1312:{\displaystyle {\frac {a}{2}}\left}
1225:{\displaystyle {\frac {a}{2}}\left}
1132:
166:The crystal structure is typically
155:resistance, surface stability, and
13:
5065:
4334:
3516:
3277:
3228:
3064:
2978:
2669:Advanced Materials & Processes
2663:Giamei, Anthony (September 2013).
2438:
2163:
2067:
1503:{\displaystyle \left\{111\right\}}
1253:{\displaystyle \left\{111\right\}}
867:could obtain very fine grains and
510:
14:
5211:
5176:Extensive bibliography and links.
5164:
4717:Materials Science and Engineering
4667:Materials Science and Engineering
3150:Materials Science and Engineering
2738:
2708:
2552:10.1016/j.engfailanal.2004.07.004
2497:
1553:engines included alloys like the
1071:
355:Ni-based superalloy compositions
5129:Materials Science and Technology
4275:Materials Science and Technology
3696:10.1016/j.scriptamat.2010.06.019
2999:10.1016/j.scriptamat.2014.11.009
2682:Akca, Enes; Gursel, Ali (2015).
2650:10.1016/j.scriptamat.2009.05.037
2411:for making superalloys. It uses
2345:
2219:
1482:that can be involved beyond the
1386:Furthermore, the burgers vector
529:are incoherent with the γ matrix
517:topologically close-packed (TCP)
25:
5101:
5079:Blain, Loz (10 February 2023).
5018:
4973:
4940:
4913:
4899:Surface and Coatings Technology
4890:
4863:
4820:
4785:
4758:
4744:Surface and Coatings Technology
4735:
4708:
4694:Surface and Coatings Technology
4685:
4658:
4623:
4596:
4583:
4548:
4516:
4503:
4476:
4441:
4406:
4392:Surface and Coatings Technology
4383:
4369:Surface and Coatings Technology
4360:
4310:Surface and Coatings Technology
4301:
4266:
4253:
4240:
4199:
4165:International Materials Reviews
4156:
4113:
4091:
4084:C. Sims, N. Stoloff, W. Hagel,
4078:
4052:
4034:Journal of Alloys and Compounds
4019:
3980:
3955:
3920:
3907:
3846:
3803:
3768:
3754:. London: Talylor and Francis.
3743:
3702:
3675:
3628:
3597:
3558:
3467:
3428:
3371:
3203:
3168:
3141:
3005:
2896:
2847:
2356:needs additional citations for
2230:needs additional citations for
2210:
820:coarse Widmanstätten platelets
36:needs additional citations for
4702:10.1016/j.surfcoat.2004.08.007
4470:10.1080/09603409.1997.11689552
4450:Materials at High Temperatures
4185:10.1179/1743280411Y.0000000014
3544:10.1016/j.intermet.2019.106670
2675:
2656:
2629:
2594:
2531:
1347:
1295:
1208:
912:Nb) (Body Centered Tetragonal)
865:Oxide dispersion strengthening
174:. Examples of such alloys are
127:Nickel superalloy jet engine (
1:
5012:10.1016/j.actamat.2003.10.045
4934:10.1016/S0921-5093(02)00905-X
4907:10.1016/S0257-8972(01)01481-5
4884:10.1016/S0079-6425(00)00007-4
4872:Progress in Materials Science
4814:10.1016/s1359-6454(99)00473-5
4779:10.1016/s1359-6454(01)00071-4
4752:10.1016/S0257-8972(01)01455-4
4679:10.1016/S0921-5093(97)00850-2
4652:10.1016/s1359-0286(99)00024-8
4617:10.1016/s0079-6425(00)00020-7
4605:Progress in Materials Science
4377:10.1016/S0257-8972(02)00602-3
4328:10.1016/S0257-8972(02)00593-5
4088:, 1987, John Wiley & Sons
4046:10.1016/j.jallcom.2019.152954
3967:www.phase-trans.msm.cam.ac.uk
3875:10.1016/S1359-6454(99)00217-7
3797:10.1016/s1359-6454(99)00029-4
3728:10.1051/matecconf/20141417002
3501:10.1016/j.actamat.2022.118372
3453:10.1016/S1359-6454(97)00084-0
3215:www.phase-trans.msm.cam.ac.uk
3197:10.1016/j.actamat.2007.11.014
3098:10.1016/j.actamat.2018.03.057
3049:10.1016/j.actamat.2016.09.017
2491:
2399:
1852:
1727:, eroding the alloy over time
1472:Shockley partial dislocations
1428:in this alloy due to its low
4435:10.1016/0040-6090(84)90277-3
4400:10.1016/0257-8972(94)90130-9
3949:10.1016/j.corsci.2011.02.033
3610:Materials and Geoenvironment
3583:10.1016/0921-5093(96)80002-5
3162:10.1016/0025-5416(87)90061-9
2720:Materials Today: Proceedings
2623:10.1016/j.corsci.2011.04.020
2540:Engineering Failure Analysis
2451:Researchers at Sandia Labs,
2405:Sandia National Laboratories
2313:energy conversion efficiency
2172:
2034:
1816:and maintaining continuity.
1702:
908:Crystal structure for γ" (Ni
199:solid solution strengthening
7:
4530:. In Bunshah, R. F. (ed.).
2732:10.1016/j.matpr.2016.03.024
2704:– via pen.ius.edu.ba.
2474:
2336:
2273:
1994:
1056:
1015:
980:
834:
203:precipitation strengthening
10:
5216:
4729:10.1016/j.msea.2004.05.052
3134:10.2320/matertrans.47.2099
2029:yttria-stabilized zirconia
2014:physical vapour deposition
1914:Directional solidification
1901:Directional solidification
1867:directional solidification
1651:Single-crystal superalloys
933:discs form as a result of
861:Directional solidification
839:
5043:10.1007/s11085-014-9496-1
4849:10.1007/s11661-999-0332-1
4342:"Wadley Research Group '"
4142:10.1007/s11661-000-0078-2
4005:10.1007/s11661-001-0169-8
3624:– via ResearchGate.
3317:10.1007/s11837-016-2094-8
3263:10.1007/s11837-008-0083-2
2074:chemical vapor deposition
874:
153:thermal creep deformation
5149:10.1179/174328407x179539
4295:10.1179/mst.1986.2.3.220
3715:MATEC Web of Conferences
2841:10.1002/pssb.19690350102
2453:Ames National Laboratory
2025:Thermal barrier coatings
2020:Thermal barrier coatings
2002:
1827:
1675:. This approximates the
927:body-centered tetragonal
5174:. Cambridge University.
5108:Levitin, Valim (2006).
4569:10.1023/A:1004549219013
4511:Materials Science Forum
2956:10.1126/science.1121738
2909:www.cobaltinstitute.org
2821:Physica Status Solidi B
2127:This process includes:
1976:Selective laser melting
830:Families of superalloys
740:acicular (needle-like)
3121:Materials Transactions
1984:additive manufacturing
1971:Additive manufacturing
1961:hot isostatic pressing
1910:
1532:
1504:
1464:
1418:
1365:
1364:{\displaystyle a\left}
1313:
1254:
1226:
1170:
1151:yield strength anomaly
913:
793:globules or platelets
141:high-performance alloy
132:
4216:10.1115/MSEC2018-6666
2457:Iowa State University
1926:Single crystal growth
1921:Single crystal growth
1908:
1533:
1505:
1465:
1430:stacking fault energy
1419:
1366:
1314:
1255:
1227:
1167:
907:
126:
4951:. pp. 579–588.
4901:. 146–147: 117–123.
4746:. 146–147: 110–116.
4371:. 163–164: 106–111.
3895:. pp. 651–687.
2858:. pp. 109–114.
2801:– via tms.org.
2752:. pp. 767–776.
2701:10.21533/pen.v3i1.43
2519:. pp. 399–419.
2365:improve this article
2239:improve this article
1683:into the structure.
1630:oxidation resistance
1626:oxidation resistance
1514:
1486:
1436:
1426:partial dislocations
1390:
1327:
1268:
1236:
1181:
941:precipitate and the
235:Chemical development
45:improve this article
5200:Aerospace materials
5141:2007MatST..23..547S
5031:Oxidation of Metals
4994:2004AcMat..52.1123M
4841:1999MMTA...30..427G
4806:2000AcMat..48.1815M
4644:1999COSSM...4..255W
4557:Oxidation of Metals
4523:Knotek, O. (2001).
4462:1997MaHT...14..261K
4427:1984TSF...118..485C
4287:1986MatST...2..220B
4177:2012IMRv...57..133G
4134:2000MMTA...31.2981A
3941:2011Corro..53.2027K
3867:1999AcMat..47.3367R
3824:1996MMTA...27..513N
3789:1999AcMat..47.1549M
3635:Reed, R. C (2006).
3492:2022AcMat.24118372L
3355:Physical metallurgy
3309:2016JOM....68k2803M
3255:2008JOM....60g..12B
3189:2008AcMat..56.1288S
3089:2018AcMat.151..137R
3040:2017AcMat.122..438N
2948:2006Sci...312...90S
2833:1969PSSBR..35...11S
2615:2011Corro..53.2713K
2576:Reed, R. C (2008).
1946:Mechanical alloying
1942:material efficiency
1876:Casting and forging
1376:Peach-Koehler force
1321:anti-phase boundary
1159:anti-phase boundary
761:elongated globules
758:FeCr, FeCrMo, CrCo
551:
356:
168:face-centered cubic
149:mechanical strength
4696:. 188–189: 71–78.
4348:on 7 December 2015
4312:. 163–164: 67–74.
4259:J. R. Davis, ed.,
4065:www.doitpoms.ac.uk
3832:10.1007/BF02648942
3684:Scripta Materialia
3384:Scientific Reports
2987:Scripta Materialia
2638:Scripta Materialia
2486:Titanium aluminide
2182:Failure mechanisms
2108:Substrate or parts
1911:
1894:Investment casting
1889:Investment casting
1859:investment casting
1528:
1500:
1460:
1414:
1361:
1309:
1250:
1232:traveling along a
1222:
1171:
914:
550:Superalloy phases
549:
498:Re, W, Hf, Mo, Ta
354:
133:
5119:978-3-527-31338-9
4773:(12): 2329–2340.
4513:1997, 251–54, 809
4497:10.5006/1.3315978
4225:978-0-7918-5135-7
4128:(12): 2981–3000.
3999:(12): 2947–2957.
3929:Corrosion Science
3913:Lund and Wagner.
3861:(12): 3367–3381.
3447:(10): 4251–4262.
3396:10.1038/srep29941
3364:978-0-444-53770-6
3303:(11): 2803–2810.
2603:Corrosion Science
2397:
2396:
2389:
2307:Energy production
2271:
2270:
2263:
1980:powder bed fusion
1937:Powder metallurgy
1932:Powder metallurgy
1447:
1401:
1371:burgers vector).
1350:
1298:
1279:
1211:
1192:
951:coherency strains
888:phase based on Ni
827:
826:
727:not close-packed
688:very small disks
508:
507:
363:Composition range
121:
120:
113:
95:
5207:
5175:
5160:
5123:
5096:
5095:
5093:
5091:
5076:
5063:
5062:
5037:(5–6): 359–381.
5022:
5016:
5015:
5005:
4988:(5): 1123–1131.
4977:
4971:
4970:
4944:
4938:
4937:
4928:(1–2): 221–231.
4917:
4911:
4910:
4894:
4888:
4887:
4878:(3–4): 249–271.
4867:
4861:
4860:
4824:
4818:
4817:
4800:(8): 1815–1827.
4789:
4783:
4782:
4762:
4756:
4755:
4739:
4733:
4732:
4723:(1–2): 162–171.
4712:
4706:
4705:
4689:
4683:
4682:
4662:
4656:
4655:
4627:
4621:
4620:
4600:
4594:
4587:
4581:
4580:
4563:(3–4): 241–258.
4552:
4546:
4545:
4529:
4520:
4514:
4507:
4501:
4500:
4480:
4474:
4473:
4445:
4439:
4438:
4415:Thin Solid Films
4410:
4404:
4403:
4394:. 68–69: 10–16.
4387:
4381:
4380:
4364:
4358:
4357:
4355:
4353:
4338:
4332:
4331:
4321:
4305:
4299:
4298:
4270:
4264:
4257:
4251:
4244:
4238:
4237:
4203:
4197:
4196:
4160:
4154:
4153:
4117:
4111:
4110:
4108:
4106:
4095:
4089:
4082:
4076:
4075:
4073:
4071:
4056:
4050:
4049:
4031:
4023:
4017:
4016:
3984:
3978:
3977:
3975:
3973:
3959:
3953:
3952:
3935:(5): 2027–2034.
3924:
3918:
3911:
3905:
3904:
3888:
3879:
3878:
3850:
3844:
3843:
3807:
3801:
3800:
3783:(5): 1549–1563.
3772:
3766:
3765:
3747:
3741:
3740:
3730:
3706:
3700:
3699:
3679:
3673:
3670:
3664:
3657:
3651:
3650:
3632:
3626:
3625:
3623:
3621:
3601:
3595:
3594:
3562:
3556:
3555:
3523:
3514:
3513:
3503:
3471:
3465:
3464:
3432:
3426:
3425:
3415:
3375:
3369:
3368:
3350:
3337:
3336:
3288:
3275:
3274:
3237:
3226:
3225:
3223:
3221:
3207:
3201:
3200:
3172:
3166:
3165:
3145:
3139:
3138:
3136:
3127:(8): 2099–2102.
3112:
3103:
3102:
3100:
3068:
3062:
3061:
3051:
3033:
3009:
3003:
3002:
2982:
2976:
2975:
2931:
2920:
2919:
2917:
2915:
2900:
2894:
2891:
2878:
2877:
2851:
2845:
2844:
2816:
2803:
2802:
2800:
2798:
2787:
2772:
2771:
2745:
2736:
2735:
2715:
2706:
2705:
2703:
2679:
2673:
2672:
2660:
2654:
2653:
2633:
2627:
2626:
2598:
2592:
2591:
2573:
2556:
2555:
2535:
2529:
2528:
2512:
2427:Austenitic steel
2421:material science
2392:
2385:
2381:
2378:
2372:
2349:
2341:
2266:
2259:
2255:
2252:
2246:
2223:
2215:
2155:Thermal spraying
2088:Pack cementation
2082:nickel aluminide
2078:thermal spraying
2054:tungsten carbide
1661:grain boundaries
1617:power-law regime
1587:vacuum induction
1579:grain boundaries
1538:slip direction.
1537:
1535:
1534:
1529:
1527:
1509:
1507:
1506:
1501:
1499:
1469:
1467:
1466:
1461:
1459:
1448:
1440:
1423:
1421:
1420:
1415:
1413:
1402:
1394:
1370:
1368:
1367:
1362:
1360:
1356:
1352:
1351:
1343:
1318:
1316:
1315:
1310:
1308:
1304:
1300:
1299:
1291:
1280:
1272:
1259:
1257:
1256:
1251:
1249:
1231:
1229:
1228:
1223:
1221:
1217:
1213:
1212:
1204:
1193:
1185:
947:lattice mismatch
935:lattice mismatch
552:
548:
365:(weight %)
357:
353:
219:grain boundaries
116:
109:
105:
102:
96:
94:
53:
29:
21:
5215:
5214:
5210:
5209:
5208:
5206:
5205:
5204:
5180:
5179:
5170:
5167:
5120:
5104:
5099:
5089:
5087:
5077:
5066:
5023:
5019:
5003:10.1.1.514.3611
4982:Acta Materialia
4978:
4974:
4967:
4945:
4941:
4918:
4914:
4895:
4891:
4868:
4864:
4825:
4821:
4794:Acta Materialia
4790:
4786:
4767:Acta Materialia
4763:
4759:
4740:
4736:
4713:
4709:
4690:
4686:
4663:
4659:
4628:
4624:
4601:
4597:
4588:
4584:
4553:
4549:
4542:
4527:
4521:
4517:
4508:
4504:
4481:
4477:
4446:
4442:
4411:
4407:
4388:
4384:
4365:
4361:
4351:
4349:
4340:
4339:
4335:
4319:10.1.1.457.1304
4306:
4302:
4271:
4267:
4258:
4254:
4245:
4241:
4226:
4204:
4200:
4161:
4157:
4118:
4114:
4104:
4102:
4097:
4096:
4092:
4083:
4079:
4069:
4067:
4057:
4053:
4024:
4020:
3985:
3981:
3971:
3969:
3961:
3960:
3956:
3925:
3921:
3912:
3908:
3889:
3882:
3855:Acta Materialia
3851:
3847:
3808:
3804:
3777:Acta Materialia
3773:
3769:
3762:
3748:
3744:
3707:
3703:
3680:
3676:
3671:
3667:
3658:
3654:
3647:
3633:
3629:
3619:
3617:
3602:
3598:
3563:
3559:
3524:
3517:
3480:Acta Materialia
3472:
3468:
3441:Acta Materialia
3433:
3429:
3376:
3372:
3365:
3351:
3340:
3289:
3278:
3238:
3229:
3219:
3217:
3209:
3208:
3204:
3177:Acta Materialia
3173:
3169:
3146:
3142:
3115:Cui, C (2006).
3113:
3106:
3077:Acta Materialia
3069:
3065:
3018:Acta Materialia
3010:
3006:
2983:
2979:
2942:(5770): 90–91.
2932:
2923:
2913:
2911:
2901:
2897:
2892:
2881:
2874:
2852:
2848:
2817:
2806:
2796:
2794:
2788:
2775:
2768:
2746:
2739:
2716:
2709:
2680:
2676:
2661:
2657:
2634:
2630:
2609:(9): 2713–720.
2599:
2595:
2588:
2574:
2559:
2536:
2532:
2513:
2498:
2494:
2477:
2449:
2441:
2439:AFA superalloys
2429:
2402:
2393:
2382:
2376:
2373:
2362:
2350:
2339:
2309:
2281:turbine engines
2276:
2267:
2256:
2250:
2247:
2236:
2224:
2213:
2184:
2175:
2166:
2164:Plasma spraying
2157:
2090:
2070:
2068:Process methods
2037:
2022:
2005:
1997:
1978:(also known as
1973:
1954:
1934:
1923:
1903:
1891:
1878:
1855:
1830:
1780:
1776:
1768:
1764:
1705:
1681:amorphous solid
1673:crystal lattice
1653:
1598:volume fraction
1576:
1572:
1560:
1545:
1517:
1515:
1512:
1511:
1510:slip plane and
1489:
1487:
1484:
1483:
1476:stacking faults
1449:
1439:
1437:
1434:
1433:
1403:
1393:
1391:
1388:
1387:
1342:
1341:
1337:
1333:
1328:
1325:
1324:
1290:
1289:
1285:
1281:
1271:
1269:
1266:
1265:
1262:primitive cubic
1239:
1237:
1234:
1233:
1203:
1202:
1198:
1194:
1184:
1182:
1179:
1178:
1140:
1135:
1074:
1059:
1045:
1041:
1038:structure of Co
1037:
1029:
1025:
1018:
1011:
1007:
999:
992:
983:
924:
920:
911:
899:
895:
891:
877:
869:superplasticity
842:
837:
832:
817:
813:
789:
785:
781:
736:
712:
705:
684:
677:
652:
645:
641:
611:
604:
581:disordered FCC
564:Composition(s)
558:Classification
542:
513:
511:Phase formation
466:
462:
430:
426:
422:
418:
403:
399:
384:
382:
364:
333:
237:
226:turbine engines
131:) turbine blade
117:
106:
100:
97:
54:
52:
42:
30:
17:
12:
11:
5:
5213:
5203:
5202:
5197:
5192:
5178:
5177:
5166:
5165:External links
5163:
5162:
5161:
5135:(5): 547–555.
5124:
5118:
5103:
5100:
5098:
5097:
5064:
5017:
4972:
4965:
4939:
4912:
4889:
4862:
4835:(2): 427–435.
4819:
4784:
4757:
4734:
4707:
4684:
4673:(2): 191–200.
4657:
4638:(3): 255–265.
4622:
4611:(5): 505–553.
4595:
4582:
4547:
4540:
4515:
4502:
4491:(7): 599–607.
4475:
4456:(3): 261–268.
4440:
4421:(4): 485–493.
4405:
4382:
4359:
4333:
4300:
4281:(3): 220–224.
4265:
4252:
4239:
4224:
4198:
4171:(3): 133–164.
4155:
4112:
4090:
4077:
4051:
4018:
3979:
3954:
3919:
3906:
3880:
3845:
3818:(3): 513–530.
3802:
3767:
3760:
3742:
3701:
3690:(8): 795–798.
3674:
3665:
3652:
3645:
3627:
3596:
3557:
3532:Intermetallics
3515:
3466:
3427:
3370:
3363:
3338:
3276:
3227:
3202:
3183:(6): 1288–97.
3167:
3140:
3104:
3063:
3004:
2977:
2921:
2895:
2879:
2872:
2846:
2804:
2790:Randy Bowman.
2773:
2766:
2737:
2726:(4): 936–941.
2707:
2674:
2655:
2628:
2593:
2586:
2557:
2546:(2): 237–247.
2530:
2495:
2493:
2490:
2489:
2488:
2483:
2476:
2473:
2448:
2445:
2440:
2437:
2428:
2425:
2401:
2398:
2395:
2394:
2353:
2351:
2344:
2338:
2335:
2331:
2330:
2327:
2324:
2308:
2305:
2296:
2295:
2292:
2275:
2272:
2269:
2268:
2227:
2225:
2218:
2212:
2209:
2205:
2204:
2201:
2198:
2195:
2192:
2183:
2180:
2174:
2171:
2165:
2162:
2156:
2153:
2148:
2147:
2144:
2141:
2138:
2135:
2132:
2125:
2124:
2120:
2119:
2115:
2114:
2110:
2109:
2089:
2086:
2069:
2066:
2036:
2033:
2021:
2018:
2004:
2001:
1996:
1993:
1972:
1969:
1953:
1950:
1933:
1930:
1922:
1919:
1902:
1899:
1890:
1887:
1877:
1874:
1863:vacuum melting
1854:
1851:
1829:
1826:
1778:
1774:
1766:
1762:
1746:
1745:
1739:
1728:
1704:
1701:
1657:single crystal
1652:
1649:
1574:
1570:
1558:
1543:
1526:
1523:
1520:
1498:
1495:
1492:
1458:
1455:
1452:
1446:
1443:
1412:
1409:
1406:
1400:
1397:
1359:
1355:
1349:
1346:
1340:
1336:
1332:
1307:
1303:
1297:
1294:
1288:
1284:
1278:
1275:
1248:
1245:
1242:
1220:
1216:
1210:
1207:
1201:
1197:
1191:
1188:
1175:burgers vector
1147:stoichiometric
1138:
1134:
1133:Microstructure
1131:
1127:
1126:
1125:
1124:
1118:
1117:
1116:
1110:
1109:
1108:
1102:
1101:
1100:
1094:
1093:
1092:
1073:
1072:Microstructure
1070:
1058:
1055:
1054:
1053:
1050:
1047:
1043:
1039:
1035:
1032:
1027:
1023:
1017:
1014:
1009:
1005:
997:
990:
982:
979:
978:
977:
974:solid solution
958:
954:
949:leads to high
922:
918:
909:
902:
901:
897:
893:
889:
882:
876:
873:
854:vacuum melting
841:
838:
836:
833:
831:
828:
825:
824:
821:
818:
815:
811:
808:
805:
802:
798:
797:
794:
791:
787:
783:
779:
776:
773:
770:
766:
765:
762:
759:
756:
753:
750:
746:
745:
741:
738:
734:
731:
728:
725:
721:
720:
717:
714:
710:
707:
706:(ordered HCP)
703:
700:
697:
693:
692:
689:
686:
682:
679:
678:(ordered BCT)
675:
672:
669:
665:
664:
661:
658:
650:
643:
639:
630:
627:
624:
620:
619:
616:
613:
609:
606:
605:(ordered FCC)
602:
599:
596:
592:
591:
588:
585:
582:
579:
576:
572:
571:
568:
565:
562:
559:
556:
540:
537:
536:
533:
530:
527:
512:
509:
506:
505:
502:
499:
495:
494:
491:
488:
484:
483:
480:
477:
473:
472:
464:
460:
451:
448:
444:
443:
440:
437:
433:
432:
428:
424:
420:
416:
413:
410:
406:
405:
401:
397:
394:
391:
387:
386:
380:
377:
374:
370:
369:
366:
361:
331:
236:
233:
119:
118:
33:
31:
24:
15:
9:
6:
4:
3:
2:
5212:
5201:
5198:
5196:
5193:
5191:
5188:
5187:
5185:
5173:
5172:"Superalloys"
5169:
5168:
5158:
5154:
5150:
5146:
5142:
5138:
5134:
5130:
5125:
5121:
5115:
5112:. WILEY-VCH.
5111:
5106:
5105:
5086:
5082:
5075:
5073:
5071:
5069:
5060:
5056:
5052:
5048:
5044:
5040:
5036:
5032:
5028:
5021:
5013:
5009:
5004:
4999:
4995:
4991:
4987:
4983:
4976:
4968:
4966:0-87339-576-X
4962:
4958:
4954:
4950:
4943:
4935:
4931:
4927:
4923:
4916:
4908:
4904:
4900:
4893:
4885:
4881:
4877:
4873:
4866:
4858:
4854:
4850:
4846:
4842:
4838:
4834:
4830:
4823:
4815:
4811:
4807:
4803:
4799:
4795:
4788:
4780:
4776:
4772:
4768:
4761:
4753:
4749:
4745:
4738:
4730:
4726:
4722:
4718:
4711:
4703:
4699:
4695:
4688:
4680:
4676:
4672:
4668:
4661:
4653:
4649:
4645:
4641:
4637:
4633:
4626:
4618:
4614:
4610:
4606:
4599:
4592:
4586:
4578:
4574:
4570:
4566:
4562:
4558:
4551:
4543:
4541:9780815514381
4537:
4533:
4526:
4519:
4512:
4506:
4498:
4494:
4490:
4486:
4479:
4471:
4467:
4463:
4459:
4455:
4451:
4444:
4436:
4432:
4428:
4424:
4420:
4416:
4409:
4401:
4397:
4393:
4386:
4378:
4374:
4370:
4363:
4347:
4343:
4337:
4329:
4325:
4320:
4315:
4311:
4304:
4296:
4292:
4288:
4284:
4280:
4276:
4269:
4262:
4256:
4249:
4243:
4235:
4231:
4227:
4221:
4217:
4213:
4209:
4202:
4194:
4190:
4186:
4182:
4178:
4174:
4170:
4166:
4159:
4151:
4147:
4143:
4139:
4135:
4131:
4127:
4123:
4116:
4100:
4094:
4087:
4081:
4066:
4062:
4055:
4047:
4043:
4039:
4035:
4030:
4022:
4014:
4010:
4006:
4002:
3998:
3994:
3990:
3983:
3968:
3964:
3958:
3950:
3946:
3942:
3938:
3934:
3930:
3923:
3916:
3910:
3902:
3898:
3894:
3887:
3885:
3876:
3872:
3868:
3864:
3860:
3856:
3849:
3841:
3837:
3833:
3829:
3825:
3821:
3817:
3813:
3806:
3798:
3794:
3790:
3786:
3782:
3778:
3771:
3763:
3761:9780850668520
3757:
3753:
3746:
3738:
3734:
3729:
3724:
3720:
3716:
3712:
3705:
3697:
3693:
3689:
3685:
3678:
3669:
3662:
3656:
3648:
3646:9780521070119
3642:
3638:
3631:
3615:
3611:
3607:
3600:
3592:
3588:
3584:
3580:
3576:
3572:
3568:
3561:
3553:
3549:
3545:
3541:
3537:
3533:
3529:
3522:
3520:
3511:
3507:
3502:
3497:
3493:
3489:
3485:
3481:
3477:
3470:
3462:
3458:
3454:
3450:
3446:
3442:
3438:
3431:
3423:
3419:
3414:
3409:
3405:
3401:
3397:
3393:
3389:
3385:
3381:
3374:
3366:
3360:
3356:
3349:
3347:
3345:
3343:
3334:
3330:
3326:
3322:
3318:
3314:
3310:
3306:
3302:
3298:
3294:
3287:
3285:
3283:
3281:
3272:
3268:
3264:
3260:
3256:
3252:
3248:
3244:
3236:
3234:
3232:
3216:
3212:
3206:
3198:
3194:
3190:
3186:
3182:
3178:
3171:
3163:
3159:
3155:
3151:
3144:
3135:
3130:
3126:
3122:
3118:
3111:
3109:
3099:
3094:
3090:
3086:
3082:
3078:
3074:
3067:
3059:
3055:
3050:
3045:
3041:
3037:
3032:
3027:
3023:
3019:
3015:
3008:
3000:
2996:
2992:
2988:
2981:
2973:
2969:
2965:
2961:
2957:
2953:
2949:
2945:
2941:
2937:
2930:
2928:
2926:
2910:
2906:
2905:"Superalloys"
2899:
2890:
2888:
2886:
2884:
2875:
2873:0-87339-576-X
2869:
2865:
2861:
2857:
2850:
2842:
2838:
2834:
2830:
2826:
2822:
2815:
2813:
2811:
2809:
2793:
2786:
2784:
2782:
2780:
2778:
2769:
2767:0-87339-477-1
2763:
2759:
2755:
2751:
2744:
2742:
2733:
2729:
2725:
2721:
2714:
2712:
2702:
2697:
2693:
2689:
2685:
2678:
2670:
2666:
2659:
2651:
2647:
2644:(6): 612–15.
2643:
2639:
2632:
2624:
2620:
2616:
2612:
2608:
2604:
2597:
2589:
2587:9780521070119
2583:
2579:
2572:
2570:
2568:
2566:
2564:
2562:
2553:
2549:
2545:
2541:
2534:
2526:
2522:
2518:
2511:
2509:
2507:
2505:
2503:
2501:
2496:
2487:
2484:
2482:
2479:
2478:
2472:
2468:
2465:
2461:
2458:
2454:
2444:
2436:
2433:
2424:
2422:
2418:
2414:
2410:
2406:
2391:
2388:
2380:
2370:
2366:
2360:
2359:
2354:This section
2352:
2348:
2343:
2342:
2334:
2328:
2325:
2322:
2321:
2320:
2318:
2314:
2304:
2300:
2293:
2290:
2289:
2288:
2286:
2285:turbine blade
2282:
2265:
2262:
2254:
2244:
2240:
2234:
2233:
2228:This section
2226:
2222:
2217:
2216:
2208:
2202:
2199:
2196:
2193:
2190:
2189:
2188:
2179:
2170:
2161:
2152:
2146:Titaniumizing
2145:
2142:
2139:
2136:
2133:
2130:
2129:
2128:
2122:
2121:
2117:
2116:
2112:
2111:
2107:
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2105:
2102:
2099:
2098:eutectic bond
2095:
2085:
2083:
2079:
2075:
2065:
2063:
2059:
2055:
2051:
2047:
2043:
2032:
2030:
2026:
2017:
2015:
2010:
2000:
1992:
1989:
1985:
1981:
1977:
1968:
1966:
1962:
1958:
1949:
1947:
1943:
1938:
1929:
1927:
1918:
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1784:
1783:diffusivities
1772:
1760:
1756:
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1737:
1733:
1732:embrittlement
1729:
1726:
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1718:
1714:
1710:
1700:
1696:
1694:
1690:
1684:
1682:
1678:
1674:
1670:
1669:intermetallic
1666:
1662:
1658:
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1633:
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1627:
1622:
1618:
1614:
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1431:
1427:
1410:
1407:
1404:
1398:
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1384:
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1377:
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1357:
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1344:
1338:
1334:
1330:
1322:
1305:
1301:
1292:
1286:
1282:
1276:
1273:
1263:
1246:
1243:
1240:
1218:
1214:
1205:
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1195:
1189:
1186:
1176:
1166:
1162:
1160:
1156:
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1148:
1144:
1130:
1122:
1121:
1119:
1114:
1113:
1111:
1106:
1105:
1103:
1098:
1097:
1095:
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1087:
1086:
1085:
1082:
1078:
1069:
1066:
1062:
1051:
1048:
1033:
1020:
1019:
1013:
1008:(Nb,V) and Co
1001:
994:
987:
975:
971:
967:
963:
959:
955:
952:
948:
945:matrix. This
944:
940:
936:
932:
928:
916:
915:
906:
887:
886:intermetallic
883:
879:
878:
872:
870:
866:
862:
857:
855:
852:Around 1950,
850:
846:
822:
819:
809:
807:rhombohedral
806:
803:
800:
799:
795:
792:
777:
774:
771:
768:
767:
763:
760:
757:
754:
751:
748:
747:
742:
739:
732:
730:orthorhombic
729:
726:
723:
722:
718:
715:
708:
701:
698:
695:
694:
690:
687:
680:
673:
670:
667:
666:
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631:
628:
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621:
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531:
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492:
489:
486:
485:
481:
478:
475:
474:
470:
459:
455:
452:
449:
446:
445:
442:Ti forms γ'.
441:
438:
435:
434:
414:
411:
408:
407:
395:
392:
389:
388:
378:
375:
372:
371:
367:
362:
359:
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352:
349:
345:
341:
340:intermetallic
337:
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83:
79:
76:
72:
69:
65:
62: –
61:
57:
56:Find sources:
50:
46:
40:
39:
34:This article
32:
28:
23:
22:
19:
5132:
5128:
5109:
5102:Bibliography
5088:. Retrieved
5084:
5034:
5030:
5020:
4985:
4981:
4975:
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4921:
4915:
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4608:
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4484:
4478:
4453:
4449:
4443:
4418:
4414:
4408:
4391:
4385:
4368:
4362:
4350:. Retrieved
4346:the original
4336:
4309:
4303:
4278:
4274:
4268:
4260:
4255:
4247:
4246:Y. Tamarin,
4242:
4207:
4201:
4168:
4164:
4158:
4125:
4121:
4115:
4103:. Retrieved
4093:
4085:
4080:
4068:. Retrieved
4064:
4054:
4037:
4033:
4021:
3996:
3992:
3982:
3970:. Retrieved
3966:
3957:
3932:
3928:
3922:
3909:
3892:
3858:
3854:
3848:
3815:
3811:
3805:
3780:
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3745:
3718:
3714:
3704:
3687:
3683:
3677:
3668:
3660:
3655:
3636:
3630:
3618:. Retrieved
3616:(3): 319–328
3613:
3609:
3599:
3577:(1): 51–63.
3574:
3570:
3560:
3535:
3531:
3483:
3479:
3469:
3444:
3440:
3430:
3390:(1): 29941.
3387:
3383:
3373:
3354:
3300:
3296:
3249:(7): 12–18.
3246:
3242:
3218:. Retrieved
3214:
3205:
3180:
3176:
3170:
3153:
3149:
3143:
3124:
3120:
3080:
3076:
3066:
3021:
3017:
3007:
2990:
2986:
2980:
2939:
2935:
2912:. Retrieved
2908:
2898:
2855:
2849:
2827:(1): 11–52.
2824:
2820:
2795:. Retrieved
2749:
2723:
2719:
2694:(1): 15–27.
2691:
2687:
2677:
2668:
2658:
2641:
2637:
2631:
2606:
2602:
2596:
2577:
2543:
2539:
2533:
2516:
2469:
2466:
2462:
2450:
2442:
2434:
2430:
2417:nanoparticle
2413:nanoparticle
2407:is studying
2403:
2383:
2374:
2363:Please help
2358:verification
2355:
2332:
2317:Carnot cycle
2310:
2301:
2297:
2277:
2257:
2248:
2237:Please help
2232:verification
2229:
2211:Applications
2206:
2185:
2176:
2167:
2158:
2149:
2140:Sherardizing
2137:Siliconizing
2126:
2103:
2091:
2071:
2058:fossil fuels
2038:
2023:
2006:
1998:
1979:
1974:
1955:
1935:
1924:
1912:
1892:
1883:
1879:
1871:
1856:
1847:
1843:
1839:
1835:
1831:
1818:
1787:
1747:
1706:
1697:
1685:
1654:
1642:
1634:
1606:
1594:
1563:precipitates
1548:
1540:
1480:slip systems
1385:
1373:
1172:
1155:Dislocations
1141:Al phase Al
1136:
1128:
1083:
1079:
1075:
1067:
1063:
1060:
1042:Ti or FCC Co
1002:
995:
988:
984:
937:between the
858:
851:
847:
843:
755:tetrahedral
654:
647:
636:
632:
545:
538:
521:
514:
468:
457:
453:
325:
238:
230:
223:
196:
165:
163:resistance.
140:
136:
134:
107:
98:
88:
81:
74:
67:
60:"Superalloy"
55:
43:Please help
38:verification
35:
18:
5195:Superalloys
5090:12 February
3083:: 137–148.
3024:: 438–447.
2914:10 December
2131:Aluminizing
2060:, electric
1812:, reducing
1677:dislocation
1645:Eglin steel
1551:gas turbine
1381:cross-slips
966:Laves phase
962:"TCP phase"
931:anisotropic
657:= metal)
567:Appearance
373:Ni, Fe, Co
328:dislocation
251:, but also
188:Rene alloys
5190:Metallurgy
5184:Categories
4040:: 152954.
3538:: 106670.
3486:: 118372.
3031:1603.05967
2492:References
2409:radiolysis
2400:Radiolysis
2377:April 2022
2299:1,000 C..
2251:April 2022
2143:Boronizing
2134:Chromizing
2042:aluminides
1965:green body
1853:Processing
1137:In pure Ni
775:hexagonal
561:Structure
450:0.05-0.2%
273:molybdenum
253:metalloids
172:austenitic
137:superalloy
101:March 2018
71:newspapers
5157:135755442
5085:New Atlas
5059:136677636
4998:CiteSeerX
4857:137312835
4577:136826569
4485:Corrosion
4314:CiteSeerX
4234:139639438
4193:137144519
4150:137660703
4013:1543-1940
3840:137172614
3721:: 17002.
3591:0921-5093
3552:0966-9795
3510:1359-6454
3461:1359-6454
3404:2045-2322
3333:137160315
3271:137354503
3156:: 11–19.
2993:: 36–39.
2173:Gas phase
2035:Bond coat
2009:aluminide
1957:Sintering
1821:corrosion
1742:depletion
1713:Oxidation
1709:corrosive
1703:Oxidation
1693:ruthenium
1691:(Re) and
1637:ruthenium
1577:) at the
1348:¯
1296:¯
1209:¯
1169:boundary.
1031:carbides.
293:zirconium
285:aluminium
257:nonmetals
211:aluminium
176:Hastelloy
161:oxidation
157:corrosion
3737:55396795
3422:27511822
3058:11222811
2972:23877638
2964:16601187
2475:See also
2337:Research
2274:Turbines
2076:(CVD)),
2062:furnaces
1995:Coatings
1982:) is an
1814:spalling
1810:adhesion
1794:kinetics
1755:chromium
1751:aluminum
1730:surface
1725:spalling
1569:(e.g. Cr
1567:carbides
1561:(Al,Ti)
1525:⟩
1519:⟨
1470:family (
1457:⟩
1451:⟨
1411:⟩
1405:⟨
1057:Fe-based
1012:(Ta,V).
981:Co-based
921:Nb or Ni
835:Ni-based
626:Carbide
623:Carbide
612:(Al,Ti)
368:Purpose
360:Element
348:titanium
344:aluminum
334:(Al,Ti)
309:vanadium
289:titanium
281:tantalum
277:tungsten
261:chromium
215:chromium
207:carbides
184:Waspaloy
143:, is an
5137:Bibcode
5051:1185421
4990:Bibcode
4837:Bibcode
4802:Bibcode
4640:Bibcode
4458:Bibcode
4423:Bibcode
4352:3 March
4283:Bibcode
4173:Bibcode
4130:Bibcode
4105:1 March
3937:Bibcode
3863:Bibcode
3820:Bibcode
3785:Bibcode
3620:8 March
3488:Bibcode
3413:4980694
3325:1362187
3305:Bibcode
3251:Bibcode
3220:2 March
3185:Bibcode
3085:Bibcode
3036:Bibcode
2944:Bibcode
2936:Science
2829:Bibcode
2797:6 March
2611:Bibcode
2046:cermets
1806:yttrium
1802:silicon
1771:chromia
1759:alumina
1738:failure
1736:fatigue
1689:rhenium
1609:rhenium
1590:casting
1555:Nimonic
1474:). The
957:motion.
840:History
810:(Fe,Co)
578:matrix
570:Effect
479:0-0.1%
412:0.5-6%
376:50-70%
321:hafnium
305:yttrium
301:rhenium
297:niobium
192:Incoloy
180:Inconel
85:scholar
5155:
5116:
5057:
5049:
5000:
4963:
4855:
4575:
4538:
4316:
4232:
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4191:
4148:
4070:13 May
4011:
3972:13 May
3838:
3758:
3735:
3643:
3589:
3550:
3508:
3459:
3420:
3410:
3402:
3361:
3331:
3323:
3269:
3056:
2970:
2962:
2870:
2764:
2584:
2283:(e.g.
2094:retort
2050:Cobalt
1804:, and
1790:stress
1769:) and
1695:(Ru).
1585:until
1583:forged
1016:Phases
875:Phases
814:(Mo,W)
801:Laves
786:Ti, Fe
782:Nb, Co
646:, and
555:Phase
501:1-10%
456:C and
393:5-20%
313:carbon
269:cobalt
249:metals
245:Nickel
170:(FCC)
87:
80:
73:
66:
58:
5153:S2CID
5055:S2CID
4853:S2CID
4573:S2CID
4528:(PDF)
4230:S2CID
4189:S2CID
4146:S2CID
3836:S2CID
3733:S2CID
3329:S2CID
3267:S2CID
3054:S2CID
3026:arXiv
2968:S2CID
2003:Types
1828:Creep
1798:boron
1717:oxide
1665:creep
1613:creep
1143:atoms
490:0-5%
476:B,Zr
439:1-4%
336:phase
317:boron
241:creep
145:alloy
139:, or
129:RB199
92:JSTOR
78:books
5114:ISBN
5092:2023
5047:OSTI
4961:ISBN
4671:A245
4536:ISBN
4354:2016
4220:ISBN
4107:2016
4072:2024
4009:ISSN
3974:2024
3756:ISBN
3641:ISBN
3622:2020
3587:ISSN
3548:ISSN
3506:ISSN
3457:ISSN
3418:PMID
3400:ISSN
3359:ISBN
3321:OSTI
3222:2018
2960:PMID
2916:2019
2868:ISBN
2799:2020
2762:ISBN
2582:ISBN
2455:and
1959:and
1753:and
804:TCP
772:TCP
752:TCP
699:GCP
671:GCP
668:γ''
629:FCC
598:GCP
383:Al).
346:and
265:iron
255:and
213:and
201:and
159:and
64:news
5145:doi
5039:doi
5008:doi
4953:doi
4930:doi
4926:352
4903:doi
4880:doi
4845:doi
4810:doi
4775:doi
4748:doi
4725:doi
4721:384
4698:doi
4675:doi
4648:doi
4613:doi
4565:doi
4493:doi
4466:doi
4431:doi
4419:118
4396:doi
4373:doi
4324:doi
4291:doi
4212:doi
4181:doi
4138:doi
4042:doi
4038:819
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3945:doi
3897:doi
3871:doi
3828:doi
3793:doi
3723:doi
3692:doi
3579:doi
3575:207
3540:doi
3536:117
3496:doi
3484:241
3449:doi
3408:PMC
3392:doi
3313:doi
3297:JOM
3259:doi
3243:JOM
3193:doi
3158:doi
3129:doi
3093:doi
3081:151
3044:doi
3022:122
2995:doi
2952:doi
2940:312
2860:doi
2837:doi
2754:doi
2728:doi
2696:doi
2646:doi
2619:doi
2548:doi
2521:doi
2367:by
2241:by
1988:CAD
1773:(Cr
1761:(Al
1621:TCP
1522:110
1494:111
1454:211
1408:110
1244:111
1177:of
1161:.
970:HCP
943:FCC
939:BCT
790:Ti
737:Nb
713:Ti
685:Nb
653:C (
635:C,
595:γ'
487:Nb
436:Ti
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390:Cr
319:or
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