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Turbomeca Turmo

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was widely investigated. To provide large mass-flow air for efficient operation of the tip-jets, Turbomeca developed a gas turbine driven gas producer, powered by the free power-turbine of the Turmo to deliver the required gas flow.
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The Turmo was initially developed with a single-stage centrifugal compressor, annular combustion chamber and single stage turbine. Power output was from a single-stage free power turbine and was initially 200 kW (270 hp).
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Turboprop engine with two axial stages, one centrifugal compressor stage and two free power turbine stages, rated at 1,300 kW (1,800 hp) at 32,000 rpm.
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With 2-stage free power-turbine, pressure ratio 5.7:1 ;Maximum shaft output 560 kW (750 shp), max continuous 450 kW (600 shp) at 33,400 rpm
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The initial version of the Turmo; max continuous gearbox output 200 kW (270 shp) at 3,000 rpm, at 33,750 rpm gas generator speed.
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Developed version of the Turmo I; max continuous gearbox output 240 kW (320 shp) at 34,000 rpm gas generator speed.
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Maximum rating 1,100 kW (1,500 hp) at 33,500 rpm for production Super Frelon helicopters
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Developed from the IIIC delivering 970 kW (1,300 hp) maximum output
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Licence production at the Changzhou Lan Xiang Machinery Works in the
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engines manufactured for helicopter use. Developed from the earlier
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STOL transport, maximum rating 913 kW (1,225 hp).
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A 890 kW (1,200 hp) turboshaft powering the
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Two-stage compressor turbine, two-stage power turbine
284:996 kW (1,335 hp) at 22,460 free turbine 598:. London: Sampson Low, Marston & Company, Ltd. 1269: 647:. Wellingborough: Patrick Stephens. p. 163. 428: 128:Current versions are built in partnership with 967: 679: 602: 485:Single-stage axial, single-stage centrifugal 589: 587: 585: 583: 296:1,080 kW (1,450 hp) at 33,500 rpm 164:development, the use of cold and hot rotor 974: 960: 693: 686: 672: 445: 151: 610:"International turbine engine directory" 593: 580: 180:Jane's all the World's Aircraft 1957–58 642: 596:Jane's all the World's Aircraft 1957–58 121:version was developed for use with the 1270: 955: 667: 983:People's Republic of China military 134:Changzhou Lan Xiang Machinery Works 13: 645:World Encyclopedia of Aero Engines 636: 14: 1299: 652: 540:3.74 kW/kg (2.27 hp/lb) 354:Aérospatiale SA 321 Super Frelon 78:Aérospatiale SA 321 Super Frelon 24: 594:Bridgman, Leonard, ed. (1957). 531:6.2 kg/s (820 lb/min) 337: 507: 1: 1288:Mixed-compressor gas turbines 573: 516:1,217 kW (1,632 hp) 476: 466:71.6 cm (28.19 in) 7: 544: 460:182 cm (71.65 in) 349:Sud-Est SE.3140 Alouette II 271:Turboprop for the proposed 172: 10: 1304: 1278:Turbomeca aircraft engines 620:(3590): 69. 7 January 1978 429:Specifications (Turmo IIIC 331:People's Republic of China 1211: 1140: 1083: 1025: 992: 925: 899: 881:MTU Turbomeca Rolls-Royce 879: 872: 799: 771: 728: 704: 472:325 kg (717 lb) 32: 23: 18: 1283:1950s turboshaft engines 568:List of aircraft engines 359:Aérospatiale SA 330 Puma 82:Aérospatiale SA 330 Puma 446:General characteristics 401:Breguet Br 940 Integral 98:Bristol Siddeley Nimbus 643:Gunston, Bill (1986). 521:Overall pressure ratio 423:Renault Étoile Filante 314:Licence production in 160:During early post-war 152:Design and development 109:is a family of French 901:Rolls-Royce Turbomeca 707:Auxiliary power units 536:Power-to-weight ratio 514:Maximum power output: 494:Annular, reverse-flow 441:Flight International. 374:SNCASE SE.3200 Frelon 33:Turbomeca Turmo IIIB 614:Flight International 454:Two-shaft turboshaft 144:, Bucharest, as the 125:transport aircraft. 550:Related development 212:Sud-Aviation Frelon 115:Turbomeca Artouste 73:Major applications 1265: 1264: 949: 948: 945: 944: 873:Joint development 659:Turbomeca website 556:Turbomeca Turmo I 384:SNCF Class T 2000 241:Military variant. 103: 102: 1295: 986:aircraft engines 976: 969: 962: 953: 952: 877: 876: 688: 681: 674: 665: 664: 648: 630: 629: 627: 625: 606: 600: 599: 591: 302:Military Variant 94: 74: 54: 28: 16: 15: 1303: 1302: 1298: 1297: 1296: 1294: 1293: 1292: 1268: 1267: 1266: 1261: 1215:Abbreviations: 1207: 1136: 1079: 1021: 988: 980: 950: 941: 921: 895: 868: 795: 767: 724: 705:Gas generators/ 700: 692: 655: 639: 637:Further reading 634: 633: 623: 621: 608: 607: 603: 592: 581: 576: 547: 510: 479: 448: 435: 432: 389:N.300 Naviplane 340: 293: 281: 263: 255: 247: 238: 229: 220: 175: 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Retrieved 617: 613: 604: 595: 561: 560: 549: 548: 534: 528: 519: 513: 497: 488: 482: 469: 463: 457: 451: 440: 437: 436: 411:Breguet 941S 364:Bölkow Bo 46 338:Applications 177: 176: 159: 155: 145: 137: 127: 106: 104: 1255:- WoZhou - 1246:- WoShan - 1219:- HuoSai - 1089:Turboshafts 929:/Turbomeca: 805:Turboshafts 508:Performance 483:Compressor: 470:Dry weight: 406:Bréguet 941 311:Turmo IV-CA 214:prototypes. 178:Data from:- 146:Turmo IV-CA 130:Rolls-Royce 123:Bréguet 941 86:Bréguet 941 1272:Categories 1257:Turboshaft 1237:- WoPen - 1085:Turboprops 938:(Turbofan) 912:(Turbofan) 801:Turboprops 574:References 490:Combustors 477:Components 417:Automobile 379:Turbotrain 343:Turboshaft 290:Turmo IIID 278:Turmo IIID 268:Turmo IIID 260:Turmo IIIC 252:Turmo IIIC 244:Turmo IIIC 235:Turmo IIIC 226:Turmo IIIC 217:Turmo IIIC 207:Turmo IIIC 202:Turmo IIIB 162:helicopter 111:turboshaft 46:turboprope 42:Turboshaft 1230:Turboprop 1142:Turbofans 1027:Turbojets 840:/Marcadau 773:Turbofans 730:Turbojets 695:Turbomeca 464:Diameter: 438:Data from 395:Turboprop 305:Turmo IVC 299:Turmo IVB 196:Turmo III 119:turboprop 66:Turbomeca 1248:Turbofan 1239:Turbojet 838:Artouste 791:Aubisque 720:Palouste 624:12 March 545:See also 320:Turmo VI 190:Turmo II 173:Variants 166:tip-jets 1203:Minshan 844:Astazou 818:Ardiden 786:Astafan 748:Marboré 738:Arbizon 499:Turbine 458:Length: 369:IAR 330 316:Romania 184:Turmo I 136:as the 57:France 936:Larzac 927:Snecma 916:RTM322 890:MTR390 859:TM 333 854:Makila 849:Bastan 833:Arrius 828:Arriel 823:Arrano 763:Piméné 743:Gabizo 715:Orédon 19:Turmo 1198:WS-20 1193:WS-19 1188:WS-18 1184:WS-17 1180:WS-15 1175:WS-13 1170:WS-11 1165:WS-10 1132:WZ-16 1075:WP-15 1070:WP-14 1065:WP-13 1060:WP-11 910:Adour 864:Turmo 813:Aneto 781:Aspin 758:Palas 753:Ossau 525:5.9:1 452:Type: 38:Type 1160:WS-9 1155:WS-8 1150:WS-6 1127:WZ-9 1122:WZ-8 1117:WZ-6 1112:WZ-5 1107:WJ-9 1102:WJ-6 1097:WJ-5 1055:WP-8 1050:WP-7 1045:WP-6 1040:WP-5 1035:PF-1 1017:HS-8 1012:HS-7 1007:HS-6 1002:HS-5 626:2019 326:WZ-6 138:WZ-6 105:The 618:113 286:rpm 1274:: 1253:WZ 1244:WS 1235:WP 1226:WJ 1217:HS 616:. 612:. 582:^ 148:. 1087:/ 975:e 968:t 961:v 903:: 883:: 803:/ 687:e 680:t 673:v 628:. 538:: 523:: 501:: 492:: 433:) 431:7 333:. 292:3 280:2 262:7 254:6 246:5 237:4 228:3 219:2 44:/

Index


Turboshaft
turboprope
Turbomeca
Aérospatiale SA 321 Super Frelon
Aérospatiale SA 330 Puma
Bréguet 941
Bristol Siddeley Nimbus
turboshaft
Turbomeca Artouste
turboprop
Bréguet 941
Rolls-Royce
Changzhou Lan Xiang Machinery Works
Turbomecanica
helicopter
tip-jets
Sud-Aviation Frelon
Breguet Br 942
rpm
Romania
People's Republic of China
Sud-Est SE.3140 Alouette II
Aérospatiale SA 321 Super Frelon
Aérospatiale SA 330 Puma
Bölkow Bo 46
IAR 330
SNCASE SE.3200 Frelon
Turbotrain
SNCF Class T 2000

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