40:
386:
667:
133:(APU), it was soon adapted to aircraft propulsion, and found a niche as a powerplant for turboshaft-driven helicopters in the 1950s. Artoustes were licence-built by
173:
helicopters, had a two-stage axial-centrifugal compressor and a three-stage turbine, with gearbox-limited power of 420–440 kW (560–590 hp).
905:
724:
838:
522:
437 kW (586 shp) (equivalent) (410 kW (550 shp) + 0.39 kN (88 lbf)) at 33,500 rpm, to 5,000 m (16,000 ft)
770:
675:
161:
helicopter, had a one-stage centrifugal compressor and a two-stage turbine, with gearbox-limited power of 300 kW (400 hp). The
647:
1124:
17:
222:(Without gearbox limit, sea level ratings are 640 kW (858 hp) for takeoff and 515 kW (690 hp) continuous)
213:(Without gearbox limit, sea level ratings are 640 kW (858 hp) for takeoff and 515 kW (690 hp) continuous)
1119:
831:
516:
437 kW (586 shp) (equivalent) (410 kW (550 shp) + 0.39 kN (88 lbf)) at 33,500 rpm, de-rated
749:
629:
1114:
708:
554:
204:(Without gearbox limit, ratings are 390 kW (523 hp) for takeoff and 353 kW (473 hp) continuous)
766:
745:
643:
625:
243:
variant, the
Marcadau was a development of the Artouste II, producing 300 kW (402 hp) through a 2.3:1
824:
371:
244:
142:
1068:
965:
267:
166:
101:
1062:
698:
262:
158:
97:
219:
440 kW (590 hp) for takeoff, 405 kW (543 hp) continuous (limited by engine gearbox)
210:
420 kW (563 hp) for takeoff, 405 kW (543 hp) continuous (limited by engine gearbox)
201:
300 kW (400 hp) for takeoff, 245 kW (330 hp) continuous (limited by engine gearbox)
1033:
595:
356:
1088:
301:
530:
1053:
915:
867:
563:
330:
859:
344:
305:
296:
130:
900:
277:
170:
8:
292:
287:
39:
943:
872:
718:
138:
996:
938:
890:
704:
272:
1011:
1006:
1001:
985:
980:
895:
282:
134:
1016:
933:
910:
850:
583:
335:
225:
150:
113:
970:
1108:
975:
320:
231:
340:
325:
195:
300 kW (400 hp) for takeoff, 245 kW (330 hp) continuous
146:
816:
315:
1042:
957:
126:
55:
765:
642:
953:
847:
744:
624:
456:
240:
77:
925:
882:
791:(21st ed.). Washington D.C.: Paul H. Wilkinson. p. 178.
481:
465:
310:
1079:
385:
67:
477:
485:
230:
Licence production and development of the
Artouste in the
493:
Pressure spray at 4.6 bar (66 psi) with return
153:. Two major versions of the Artouste were produced. The
129:
engine, first run in 1947. Originally conceived as an
703:. New York: McGraw-Hill Book Company. p. 460.
697:Taylor, John W. R., F.R.Hist.S., A.R.Ae.S. (1965).
559:
0.46 kg/kWh (0.76 lb/(hp⋅h)) (equivalent)
380:
1106:
812:. Wellingborough: Patrick Stephens. p. 163.
568:2.84 kW/kg (1.73 hp/lb) (equivalent)
376:Aviodrome - Lelystad Airport - The Netherlands
367:A Turbomeca Artouste is on public display at:
832:
761:
759:
723:: CS1 maint: multiple names: authors list (
690:
662:
660:
620:
618:
846:
839:
825:
780:
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738:
736:
734:
399:
786:
756:
636:
657:
615:
384:
807:
771:"Type-Certificate Data Sheet No. E.091"
731:
700:Jane's All the World's Aircraft 1965-66
648:"Type-Certificate Data Sheet No. E.137"
630:"Type Certificate Data Sheet No. E-300"
14:
1107:
767:European Aviation Safety Agency (EASA)
696:
644:European Aviation Safety Agency (EASA)
550:773 K (500 °C) at 33,500 rpm
165:family, mainly used in Aérospatiale's
820:
746:Federal Aviation Administration (FAA)
626:Federal Aviation Administration (FAA)
389:Turbomeca Artouste on an Alouette III
362:
198:Artouste IIC, IIC1, IIC2, IIC5, IIC6
452:1-stage axial + 1-stage centrifugal
24:
810:World Encyclopedia of Aero Engines
789:Aircraft engines of the World 1970
750:"Type Certificate Data Sheet E1IN"
420:~450 mm (18 in) (casing)
396:Aircraft engines of the World 1970
25:
1136:
38:
251:
1125:Aircraft auxiliary power units
497:
381:Specifications (Artouste IIIB)
372:The Helicopter Museum (Weston)
27:Early French turboshaft engine
13:
1:
601:
541:4.3 kg/s (9.5 lb/s)
443:
143:Hindustan Aeronautics Limited
414:1,815 mm (71.5 in)
7:
787:Wilkinson, Paul H. (1970).
572:
476:Aviation Kerosene, such as
176:
157:family, mainly used in the
145:in India, and developed by
10:
1141:
1120:Turbomeca aircraft engines
545:Turbine inlet temperature:
461:Annular combustion chamber
433:627 mm (24.7 in)
427:507 mm (20.0 in)
1078:
1052:
1034:MTU Turbomeca Rolls-Royce
1032:
1025:
952:
924:
881:
857:
555:Specific fuel consumption
520:Maximum continuous power:
439:154 kg (340 lb)
268:Aérospatiale Alouette III
102:Aérospatiale Alouette III
46:
37:
32:
1115:1940s turboshaft engines
672:TURBOMECA - Safran Group
668:"Our products: Artouste"
596:List of aircraft engines
357:Morane-Saulnier Epervier
263:Aérospatiale Alouette II
159:Aérospatiale Alouette II
98:Aérospatiale Alouette II
47:Turbomeca Artouste IIIB
400:General characteristics
302:Hawker Siddeley Trident
808:Gunston, Bill (1986).
531:Overall pressure ratio
390:
18:Turbomeca Artouste IIB
1054:Rolls-Royce Turbomeca
860:Auxiliary power units
564:Power-to-weight ratio
504:Maximum power output:
388:
331:Piasecki VZ-8 Airgeep
216:Artouste IIIB1, IIID
131:auxiliary power unit
678:on 18 December 2008
578:Related development
293:Handley Page Victor
288:Curtiss-Wright VZ-7
125:is an early French
391:
363:Engines on display
236:Turbomeca Marcadau
192:Artouste IIB, IIB1
123:Turbomeca Artouste
93:Major applications
1102:
1101:
1098:
1097:
1026:Joint development
769:(1 August 2016).
748:(20 March 2007).
646:(1 August 2016).
628:(20 March 2007).
278:Aerotécnica AC-14
273:Aerospatiale Lama
245:reduction gearbox
149:in the US as the
119:
118:
16:(Redirected from
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841:
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827:
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763:
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753:
742:
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694:
688:
687:
685:
683:
674:. Archived from
664:
655:
654:
652:
640:
634:
633:
622:
283:Atlas XH-1 Alpha
135:Bristol Siddeley
110:
94:
64:
42:
30:
29:
21:
1140:
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1103:
1094:
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1021:
948:
920:
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858:Gas generators/
853:
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773:
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711:
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681:
679:
666:
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623:
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584:Continental T51
575:
514:Take-off power:
506:
500:
470:3-stage turbine
446:
421:
402:
383:
365:
336:SNCASO Farfadet
254:
226:Continental T51
179:
151:Continental T51
147:Continental CAE
114:Continental T51
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100:
92:
63:National origin
62:
28:
23:
22:
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11:
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539:Air mass flow:
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109:Developed into
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710:9780531039151
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590:Related lists
585:
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321:Merckle SM 67
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232:United States
229:
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207:Artouste IIIB
206:
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141:) in the UK,
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74:Manufacturer
73:
72:
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61:
60:
57:
54:
51:
50:
45:
41:
36:
31:
19:
1071:(Turboshaft)
1045:(Turboshaft)
990:
851:aero engines
809:
800:Bibliography
788:
782:
699:
692:
680:. Retrieved
676:the original
671:
638:
589:
588:
577:
576:
562:
553:
547:
544:
538:
529:
519:
513:
503:
490:
473:
464:
455:
449:
436:
430:
424:
417:
411:
405:
393:
392:
366:
341:Vickers VC10
326:Nord Norelfe
252:Applications
167:Alouette III
163:Artouste III
162:
154:
122:
120:
1082:/Turbomeca:
958:Turboshafts
682:1 September
498:Performance
491:Oil system:
450:Compressor:
437:Dry weight:
187:Artouste II
155:Artouste II
1109:Categories
1091:(Turbofan)
1065:(Turbofan)
954:Turboprops
602:References
474:Fuel type:
457:Combustors
444:Components
408:Turboshaft
182:Artouste I
137:(formerly
127:turboshaft
84:First run
56:Turboshaft
993:/Marcadau
926:Turbofans
883:Turbojets
848:Turbomeca
719:cite book
418:Diameter:
394:Data from
241:turboprop
139:Blackburn
78:Turbomeca
33:Artouste
991:Artouste
944:Aubisque
873:Palouste
573:See also
351:Marcadau
257:Artouste
177:Variants
997:Astazou
971:Ardiden
939:Astafan
901:Marboré
891:Arbizon
482:Jet A-1
466:Turbine
431:Height:
412:Length:
316:IAR 317
311:IAR 316
1089:Larzac
1080:Snecma
1069:RTM322
1043:MTR390
1012:TM 333
1007:Makila
1002:Bastan
986:Arrius
981:Arriel
976:Arrano
916:Piméné
896:Gabizo
868:Orédon
707:
425:Width:
68:France
1063:Adour
1017:Turmo
966:Aneto
934:Aspin
911:Palas
906:Ossau
774:(PDF)
651:(PDF)
607:Notes
535:5.2:1
478:Jet A
406:Type:
343:- as
304:- as
295:- as
87:1947
52:Type
725:link
705:ISBN
684:2021
486:JP-4
171:Lama
169:and
121:The
548:JPT
484:or
345:APU
306:APU
297:APU
1111::
758:^
733:^
721:}}
717:{{
670:.
659:^
617:^
480:,
239:A
1056::
1036::
956:/
840:e
833:t
826:v
776:.
752:.
727:)
713:.
686:.
653:.
632:.
566::
557::
533::
468::
459::
247:.
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.