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A single-stage fan, driven by a three-stage LP turbine, supercharged the nine-stage HP compressor, which was driven by a two-stage air-cooled HP turbine. The combustor was annular and the exhaust separate jets. The HP compressor was based on a scale-up of the
87:
HP compressor, with a ninth stage added at the rear. Fan diameter was restricted to 60 in (1,524 mm), because of the relatively short undercarriage of the 737. Even then, the engine nacelle required an oblate shape so as to improve ground clearance.
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Although two prototype engines were built and ground tested, the project was cancelled in the early 1980s.
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254:. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited.
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71:(JAEC) consortium hoped to develop for aircraft like the
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was a 20,000 lbf (89 kN) civil turbofan which
272:. Cambridge, England. Patrick Stephens Limited, 1989.
312:
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252:World Encyclopedia of Aero Engines, 5th Edition
298:
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107:
94:
249:
803:
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13:
14:
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42:Japanese Aero Engines Corporation
128:59 in (1,499 mm) (fan)
69:Japanese Aero Engine Corporation
147:Single-stage fan, nine-stage HP
230:
169:
1:
218:
138:
134:4,081 lb (1,851 kg)
182:20,000 lbf (89 kN)
165:Three-stage LP, two-stage HP
7:
201:
122:101 in (2,571 mm)
10:
827:
492:International Aero Engines
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723:MTU Turbomeca Rolls-Royce
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270:Rolls-Royce Aero Engines
213:List of aircraft engines
103:Rolls-Royce Aero Engines
108:General characteristics
77:McDonnell Douglas MD-80
811:1980s turbofan engines
680:Europrop International
250:Gunston, Bill (2006).
193:Thrust-to-weight ratio
95:Specifications (RJ500)
61:Rolls-Royce/JAEC RJ500
737:Rolls-Royce Turbomeca
601:Rolls-Royce Turbomeca
460:GE Honda Aero Engines
236:Gunston 1989, p. 218.
764:Pratt & Whitney
666:Pratt & Whitney
519:Pratt & Whitney
367:Rolls-Royce Limited
188:635 lb/s (288 kg/s)
446:EuroJet Turbo GmbH
313:Joint development
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782:CFM International
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409:CFM International
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85:Rolls-Royce RB401
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474:General Electric
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207:Related lists
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585:Rolls-Royce/
561:Rolls-Royce/
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315:aero engines
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244:Bibliography
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49:Number built
634:Turbo-Union
478:Rolls Royce
395:CFE Company
342:Olympus 593
332:Rolls-Royce
170:Performance
145:Compressor:
132:Dry weight:
65:Rolls-Royce
38:Rolls-Royce
696:/Turbomeca
417:CFM56/F108
219:References
152:Combustors
139:Components
620:Turbomeca
563:MAN Turbo
354:Turbofans
323:Turbojets
126:Diameter:
100:Data from
805:Category
755:Propfans
715:T800-LHT
686:TP400-D6
672:T800-APW
533:PowerJet
500:SuperFan
202:See also
176:Maximum
116:Turbofan
75:and the
67:and the
28:Turbofan
768:Allison
525:RTF-180
363:Allison
161:Turbine
156:Annular
120:Length:
774:578-DX
743:RTM322
729:MTR390
626:Larzac
616:Snecma
587:Snecma
576:RB.193
571:RB.153
539:SaM146
438:GP7000
401:CFE738
336:Snecma
276:
258:
178:thrust
19:RJ500
709:LHTEC
640:RB199
608:Adour
554:RJ500
505:V2500
466:HF120
452:EJ200
387:BR700
224:Notes
197:4.9:1
114:Type:
24:Type
788:RISE
662:Avco
654:T900
648:ATEC
593:M45H
548:JAEC
484:F136
422:LEAP
373:TF41
274:ISBN
256:ISBN
59:The
694:HAL
515:MTU
807::
79:.
53:2
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334:/
306:e
299:t
292:v
264:.
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