148:
250:
231:, intake air entered the bypass duct, via a gap in the cold nozzle outer wall, and went through the fan, to be expelled through the intake. A small proportion of the bypass duct air entered the IP compressor, via a special diverter valve, to sustain the gas generator. Reverse thrust was obtained by the fan going through fine (rather than feather) pitch. Engine testing took place in the mid 1970s. The chief engineer of this project was
179:
31:
158:
The VFW 614 was designed to operate over short sectors with up to a dozen flights a day. The engines were optimized for 30-minute sectors at a cruise altitude of 21,000 feet at Mach 0.65. Only a few minutes would be spent at the cruise rating and most of the flight would be at the higher climb rating
162:
The engine was designed to be uprated without drastic redesign. Three options were water injection (+10% thrust), improved HP turbine (+10% thrust), addition of a zero-stage to the LP compressor (+25% thrust). The M45H-01 was to have a
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The engine was developed at the time of the Rolls-Royce bankruptcy which resulted in delays in developing the engine.
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or at a descent setting. The engine had a low turbine entry temperature and comparatively low rotational speed.
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227:, meant a low fan tip speed could be employed. A low hot jet velocity was another major design feature. In
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A derivative of the M45H-01 turbofan, designed to demonstrate ultra-quiet engine technologies, needed for
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239:. After the prototype engine was stored, it was given to McMurtry for safe keeping at the New Mills site.
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720:. 1976 Spring Convention: Seeds for Success in Civil Aircraft Design in the Next Two Decades.
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780:
769:"The M.45SD-02 variable pitch geared fan engine demonstrator test and evaluation experience"
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Rolls-Royce/SNECMA M45H engines are on display as part of the aero engine collection at the
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167:(TSFC) of 12.91 grams per kilonewton per second (0.456 pounds per pound-force per hour).
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125:
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58:
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566:. Springer Aerospace Technology. Springer Science+Business Media, LLC. p. 288.
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Military low bypass turbofan 13,200 lbf (58.72 kN) for take-off, wet.
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202:
Civil medium bypass turbofan 7,880 lbf (35.05 kN) for take-off, wet.
178:
108:
30:
792:
744:
182:
The M45SD-02 variable geometry fan engine at the New Mills
Technology Centre.
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613:(21st ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 165–167.
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269:. Additionally, an engine, with its cowl and pylon, is displayed at the
1316:
355:
273:; this museum also displays a VFW-614, which has two engines mounted.
190:
Civil low bypass turbofan 7,915 lbf (35.21 kN) for take-off.
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76:
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3-stage low pressure and single-stage high pressure turbines
717:
A variable pitch fan for an ultra quiet demonstrator engine
773:
835:
Rolls-Royce/SNECMA promotional film about the M45H engine
131:
The design was started as a collaborative effort between
332:
5-stage intermediate pressure and 7-stage high-pressure
219:
aircraft operating from city centre airports. A geared,
208:
Rolls-Royce designation for the M45SD-02 geared turbofan
372:
pressure return system at 207 kPa (30 psi)
124:
turbofan produced specifically for the twin-engined
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714:Davies, D. G. M.; Miller, D. C. (19–20 May 1976).
508:. 18 April 1974. pp. 485–488. Archived from
739:. Vol. 51, no. 764. pp. 376–377.
767:Wright, G. H.; Russell, J. G. (18 March 1980).
645:. 4 November 1971. p. 730. Archived from
860:
16:1970s British/French turbofan aircraft engine
8:
604:
602:
600:
481:. 6 January 1966. p. 28. Archived from
779:(836) (published September 1980): 268–277.
1321:
920:
889:
867:
853:
845:
731:"Rolls-Royce design for quieter airliners"
1383:Rolls-Royce aircraft gas turbine engines
560:Airbreathing propulsion: An introduction
464:
285:Jane's All the World's Aircraft 1971-72
271:Deutsches Museum Flugwerft Schleissheim
694:: CS1 maint: archived copy as title (
687:
531:
530:
519:
20:
729:Stevens, James Hay (12 August 1971).
611:Aircraft engines of the World 1966/77
494:
492:
151:An M45H in its overwing mount on the
7:
366:Aviation kerosene (JetA-1 typically)
267:Musée aéronautique et spatial Safran
351:Annular with 24 vapourising burners
14:
736:New Scientist and Science Journal
500:"M45H: Power for VFW-Fokker 614"
165:thrust-specific fuel consumption
29:
1373:Medium-bypass turbofan engines
263:Royal Air Force Museum Cosford
1:
755:. London: Pilot Press, 1971.
404:104 kg/s (230 lb/s)
235:, co-founder and Chairman of
128:aircraft in the early 1970s.
634:"614: VFW's jet feederliner"
277:Specifications (M45H Mk.501)
609:Wilkinson, Paul H. (1966).
1399:
1054:International Aero Engines
753:Air Enthusiast, Volume One
722:Royal Aeronautical Society
512:on 4 March 2016. Includes
473:"Bristol Siddeley engines"
120:is an Anglo-French medium
1285:MTU Turbomeca Rolls-Royce
785:10.1017/S0001924000031304
572:10.1007/978-1-4614-3532-7
37:
28:
23:
623:J W R Taylor 1971,p.650.
594:Swanborough 1971, p.371.
453:List of aircraft engines
542:CS1 maint: postscript (
336:with a single-stage fan
291:General characteristics
118:Rolls-Royce/SNECMA M45H
38:M45H engine on display
1378:1970s turbofan engines
1242:Europrop International
409:Thrust-to-weight ratio
394:Overall pressure ratio
258:
183:
155:
143:Design and development
1299:Rolls-Royce Turbomeca
1163:Rolls-Royce Turbomeca
1022:GE Honda Aero Engines
751:Swanborough, Gordon.
441:General Electric CF34
252:
181:
150:
828:Flight International
824:Stol Fans from Dowty
642:Flight International
505:Flight International
485:on 10 November 2013.
478:Flight International
1326:Pratt & Whitney
1228:Pratt & Whitney
1081:Pratt & Whitney
929:Rolls-Royce Limited
423:Related development
389:7,300 lbf (32.4 kN)
1008:EuroJet Turbo GmbH
875:Joint development
435:Comparable engines
307:2,600 mm (102.4in)
259:
245:Engines on display
221:variable pitch fan
184:
156:
92:Major applications
1360:
1359:
1356:
1355:
1344:CFM International
1311:
1310:
971:CFM International
910:
909:
581:978-1-4614-3531-0
557:Bose, T. (2012).
532:|postscript=
529:External link in
319:673 kg (1,483 lb)
114:
113:
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1036:General Electric
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724:. pp. 1–18.
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669:. Archived from
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334:axial compressor
313:909 mm (35.8 in)
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133:Bristol Siddeley
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707:Further reading
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664:"Archived copy"
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818:External links
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676:on 6 June 2011
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514:engine cutaway
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253:Cutout at the
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233:David McMurtry
229:reverse thrust
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153:VFW-Fokker 614
144:
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126:VFW-Fokker 614
112:
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104:Developed from
100:
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97:VFW-Fokker 614
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59:United Kingdom
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826:a 1971-01-21
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761:0-385-08171-5
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522:cite magazine
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447:Related lists
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340:Bypass ratio:
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69:Manufacturer
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27:
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1147:Rolls-Royce/
1123:Rolls-Royce/
1108:Rolls-Royce/
877:aero engines
827:
776:
772:
752:
734:
721:
716:
678:. Retrieved
671:the original
658:
647:the original
640:
628:
619:
610:
590:
559:
552:
510:the original
503:
483:the original
476:
467:
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369:
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296:
284:
281:
280:
260:
255:Aeronauticum
237:Renishaw PLC
225:bypass ratio
169:
161:
157:
130:
122:bypass ratio
117:
115:
18:
1196:Turbo-Union
1040:Rolls Royce
957:CFE Company
904:Olympus 593
894:Rolls-Royce
377:Performance
370:Oil system:
330:Compressor:
317:Dry weight:
73:Rolls-Royce
1367:Categories
1258:/Turbomeca
979:CFM56/F108
801:8272365305
680:21 October
459:References
429:SNECMA M45
364:Fuel type:
347:Combustors
324:Components
109:SNECMA M45
83:First run
1182:Turbomeca
1125:MAN Turbo
916:Turbofans
885:Turbojets
809:245674662
793:0001-9240
745:0369-5808
311:Diameter:
282:Data from
1317:Propfans
1277:T800-LHT
1248:TP400-D6
1234:T800-APW
1095:PowerJet
1062:SuperFan
690:cite web
418:See also
383:Maximum
300:Turbofan
265:and the
211:M45SD-02
174:Variants
47:Turbofan
1330:Allison
1087:RTF-180
925:Allison
840:YouTube
830:article
356:Turbine
305:Length:
1336:578-DX
1305:RTM322
1291:MTR390
1188:Larzac
1178:Snecma
1149:Snecma
1138:RB.193
1133:RB.153
1101:SaM146
1000:GP7000
963:CFE738
898:Snecma
807:
799:
791:
759:
743:
578:
398:16.5:1
385:thrust
342:2.85:1
257:museum
205:RB.410
137:SNECMA
77:SNECMA
63:France
1271:LHTEC
1202:RB199
1170:Adour
1116:RJ500
1067:V2500
1028:HF120
1014:EJ200
949:BR700
805:S2CID
674:(PDF)
667:(PDF)
650:(PDF)
637:(PDF)
564:(PDF)
413:4.9:1
297:Type:
86:1970
43:Type
24:M45H
1350:RISE
1224:Avco
1216:T900
1210:ATEC
1155:M45H
1110:JAEC
1046:F136
984:LEAP
935:TF41
797:OCLC
789:ISSN
757:ISBN
741:ISSN
696:link
682:2007
576:ISBN
544:link
537:help
217:STOL
199:M45H
193:M45G
187:M45F
135:and
116:The
1256:HAL
1077:MTU
838:on
781:doi
568:doi
1369::
803:.
795:.
787:.
777:84
775:.
771:.
733:.
692:}}
688:{{
639:.
599:^
574:.
526::
524:}}
520:{{
502:.
491:^
475:.
139:.
61:/
1328:/
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1165::
1079:/
1038:/
927:/
896:/
868:e
861:t
854:v
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747:.
698:)
684:.
584:.
570::
546:)
539:)
535:(
516:.
411::
396::
387::
358::
349::
287:.
75:/
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
