136:, a 10-cylinder engine, air-cooled like its predecessors, which, like other Anzani engines, was made with different size cylinders. One of the more powerful versions produced about 110 hp (82 kW) from 12.1 litres, a British-built Anzani 10 was rated at 125 hp and a smaller version with a displacement of 8.27 litres produced 80 hp (60 kW). It was a double row engine, built with two rows of five cylinders separated along the crankshaft by about a cylinder radius, giving the engine a slimmer profile than other contemporary two-row radial engines. Each half had its own crankpin, 180° apart, with the connecting rods, of chrome nickel steel, broad and flat to bring the two halves close together. Cylinder heads and pistons were made of cast iron, the latter machined inside and out and fitted with a pair of rings. Oil was forced through the crankshaft to the crankpins, then moved under centrifugal force to the cylinders and pistons from inside the crankcase which was a single light alloy casting.
140:
cooling of the mixture by the oncoming airflow. This arrangement placed the exhaust valves at the front of the engine, where they were operated from a cam in the rear of the crankcase via push rods and rockers. A single carburettor fed the crankcase chambers from below. Some versions used a single Gibaud magneto, running at 3,000 rpm, though others built by
British Anzani had a pair of Bosch magnetos, running slower. Plugs (K.L.G. for the British variant) were mounted in the sides of the cylinder heads, sloping upwards to avoid plug fouling by lubricating oil. The exhaust was collected by a prominent pair of semi-circular manifolds.
40:
160:, particularly the later ones in which the Anzani replaced the lower powered rotary Gnomes. Numbers of these are uncertain because of the engine change. Because they powered the 66 Caudron G.4s purchased by the American Expeditionary Force after September 1917, used largely as trainers, many Anzani 10s went to the USA. The first production aircraft built by
139:
Both inlet and exhaust valves were in the cylinder heads. The automatic inlet valves of earlier Anzani engines, opened by atmospheric pressure and closed by valve springs were retained, but fuel was fed from a mixing chamber in the crankcase via inlet tubes placed at the rear of the engine to avoid
190:
389:
Single carburettor mounted between lowest cylinders, mixing chamber in crankcase. Single magneto. Plugs were fitted in the upper side of the cylinder head to avoid fouling.
569:
In some images of the rear of the engine, it is initially difficult to see the narrow pushods against the background of the broader inlet tubes, e.g. Fig 4 in
823:
274:
264:
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299:
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129:'s successful Channel crossing flight of 1909, into a three-cylinder symmetric or 'Y' radial, and from that to a 6-cylinder double-row radial engine.
772:
533:
844:
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in 1914. Several early aircraft built singly or in small numbers flew with the Anzani 10, but the major users were the
740:
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765:
818:
813:
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One inlet and one exhaust valves/cylinder. Automatic inlet valves, push and rocker operated exhaust valves.
758:
168:
was powered by the Anzani 10, and 14 of these were made. Huff-Daland also used them in several aircraft.
717:
703:
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17:
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101:. It powered several experimental aircraft and also the later production versions of the
8:
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developed his upright 3-cylinder 'W' type motorcycle engine, which powered
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Anzani 10, propeller side. Image from
National Museum of the US Air Force
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One
British-built 125 hp Anzani 10 underwent exhaustive tests at
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bomber/trainer and the first production Cessna, the
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626:U.S. Army Aircraft (heavier-than-air) 1908–1946
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690:"Anzani engines and the new 200 h.p. model"
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662:. Vol. 2. London: Putnam Publishing.
645:. Vol. 1. London: Putnam Publishing.
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850:Aircraft air-cooled radial piston engines
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325:two-row ten-cylinder radial piston engine
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121:In the first decade of the 20th century
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467:
14:
837:
450:
285:London and Provincial Fuselage Biplane
143:
754:
620:
735:. Wellingborough: Patrick Stephens.
733:World Encyclopaedia of Aero Engines
191:Blackburn Type I Land/Sea monoplane
27:1910s French aircraft piston engine
24:
531:A History of Aeronautics Pt 4 Ch 3
25:
866:
704:"Aero engines at Paris show 1913"
628:. New York: Ships and Aircraft.
38:
658:Jackson, Aubrey Joseph (1960).
641:Jackson, Aubrey Joseph (1959).
613:
597:
171:
660:British Civil Aircraft 1919–59
643:British Civil Aircraft 1919–59
585:
576:
563:
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399:
13:
1:
845:1910s aircraft piston engines
438:
371:
105:reconnaissance aircraft, the
7:
421:
10:
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352:12.12 litres (739.8 cu in)
55:10-cylinder radial piston
791:
560:, 24 January 1914 pp.97–8
132:By 1912 he had built the
46:
37:
32:
536:October 7, 2011, at the
443:
433:List of aircraft engines
855:Anzani aircraft engines
684:: 20–1. 4 January 1913.
417:0.59 kW/kg (0.36 hp/lb)
317:General characteristics
307:Specifications (110 hp)
731:Gunston, Bill (1989).
712:: 97. 24 January 1914.
676:"Aeronautical Engines"
197:Blackburn White Falcon
117:Design and development
99:radial aircraft engine
487:, 4 January 1913 p.21
413:Power-to-weight ratio
622:Fahey, James Charles
573:4 January 1913, p.21
698:: 748. 5 July 1913.
521:, 5 July 1913 p.748
290:Sopwith Grasshopper
259:Handley Page Type G
248:Deperdussin Seagull
144:Operational history
726:: 474. 2 May 1914.
504:, 2 May 1914 p.474
231:Central Centaur IV
832:
831:
594:, pp. 73, 79
275:Huff-Daland HD-9A
265:Huff-Daland HD-1B
209:Breda-Pensuti B.2
203:Blackburn Sidecar
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16:(Redirected from
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343:140 mm (5.51 in)
334:105 mm (4.13 in)
300:Vickers F.B. 12C
280:Huff-Daland TA-2
270:Huff-Daland HD-4
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538:Wayback Machine
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393:Cooling system:
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361:140 kg (308 lb)
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295:Timm Collegiate
237:Cessna Model AA
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61:National origin
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408:82 kW (110 hp)
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214:Caudron Type F
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91:was a 1913 10-
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427:Related lists
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785:aero engines
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614:Bibliography
604:Jackson 1960
599:
592:Jackson 1959
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468:Gunston 1989
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387:Fuel system:
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348:Displacement
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328:
322:
311:
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179:
172:Applications
162:Clyde Cessna
147:
138:
133:
131:
120:
88:
86:
400:Performance
243:Curtiss H-4
225:Caudron G.4
219:Caudron G.3
186:Bellanca CF
178:Avro 504 K
154:Caudron G.3
150:Farnborough
107:Caudron G.4
103:Caudron G.3
839:Categories
824:4 cylinder
439:References
395:air-cooled
379:Valvetrain
372:Components
357:Dry weight
96:air-cooled
78:First run
33:Anzani 10
668:221677465
367:A. Anzani
365:Designer:
312:Data from
134:Anzani 10
89:Anzani 10
18:Anzani 10
624:(1946).
534:Archived
422:See also
166:Model AA
111:Model AA
93:cylinder
718:"Notes"
651:1301918
634:1726749
127:Bleriot
73:Anzani
65:France
819:Y-type
782:Anzani
739:
723:Flight
709:Flight
695:Flight
681:Flight
666:
649:
632:
571:Flight
558:Flight
519:Flight
502:Flight
485:Flight
339:Stroke
180:G-EBWO
164:, the
123:Anzani
444:Notes
323:Type:
239:1920s
81:1913
52:Type
737:ISBN
664:OCLC
647:OCLC
630:OCLC
330:Bore
302:1917
261:1913
250:1913
233:1919
227:1915
221:1914
205:1921
199:1915
193:1915
156:and
87:The
814:W-3
158:G.4
841::
809:20
804:10
720:.
706:.
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678:.
544:^
509:^
492:^
475:^
452:^
113:.
799:6
774:e
767:t
760:v
745:.
670:.
653:.
636:.
415::
381::
359::
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332::
20:)
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