29:
173:, avoiding the high reduction gear of a single spool turboprop and allowing an easier starting since the gas generator is disengaged from the power turbine. The HP spool turns at 31,500 rpm while the LP spool turns at 19,444, reduced to 1,700 for the propeller: a 11.4 reduction ratio. Power can grow by 25% within the same size.
207:
The engine was originally called the TPE331-16, but by 1988 it was renamed to the TPF351-20. The "TPF" represented "Turbine PropFan", while the -20 suffix indicated the 2,000 shp (1,500 kW) nominal thermodynamic power rating.
1882:
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200:. A large-diameter bore hole running through the compressor and turbines allow a concentric shaft to connect the power turbine to a front-mounted gearbox to convert it to a
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It is assembled from six modules: accessory gearbox, compressor, combustor, gas-generator turbine, power turbine, and propeller gearbox. The
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in
September of the same year. Both programs were cancelled in 1992, when the TPF351 was nine months from engine certification.
680:
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528:
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trainers. The engine ran about 60 °F (33 °C) hotter than the TPE331-14 in the core. It was
Garrett's first
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121:, a high-speed commuter "pusher" aircraft. It was first tested on May 19, 1989 and then ground tested and
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on July 9, 1990. The first prototype CBA 123 was tested on July 18, 1990, followed by a flight to the
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117:. Initiated by Garrett in October 1987, the TPF351-20 engine was selected by Embraer to power the
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157:, already of the right size. The two-stage centrifugal compressor is scaled-up from the
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593:
Lambert, Mark (May 1988). "TPF351-20, the
Garrett free turbine turboprop".
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39:
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444:"Garrett TPF351-20 Engine Flight Test and Ground Test Performance"
297:
154:
28:
625:
The history of North
American small gas turbine aircraft engines
557:
Elliott, Simon (November 11, 1992). "Small-turbine directory".
192:
and auto-relight. It could have powered growth versions of the
181:
142:
890:
177:
622:Leyes, Richard A., II; Fleming, William A. (1999).
634:American Institute of Aeronautics and Astronautics
588:
586:
141:It was built on the 1,310 kW (1,760 hp)
476:
474:
472:
422:
420:
62:Garrett Engine Division of AlliedSignal Aerospace
1928:
583:
341:0.495 lb/(hp⋅h) (301 g/kWh) in cruise
563:. Vol. 142, no. 4344. pp. 39+.
497:
495:
469:
454:
417:
265:800 lb (363 kg) with all accessories
962:
688:
323:, 2,110 hp (1,570 kW) thermodynamic
223:
664:: CS1 maint: multiple names: authors list (
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552:
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236:
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306:, three-stage free-power axial turbine
232:Flight International, 28 November 1990
950:
676:
1937:Honeywell Aerospace aircraft engines
13:
14:
1953:
482:"Vector pushes ahead with TPF351"
350:1.88 hp/lb (3.09 kW/kg)
503:"Garrett engine is redesignated"
388:Pratt & Whitney Canada PW100
27:
615:
211:
16:1980s American turboprop engine
937:AVCO Lycoming/Textron Lycoming
529:"Embraer unveils Time Machine"
435:
383:Pratt & Whitney Canada PT6
319:1,500 hp (1,120 kW)
310:
115:AlliedSignal Aerospace Company
1:
630:National Air and Space Museum
509:. February 1988. p. 12.
410:
269:
980:gas turbine aircraft engine
7:
531:. Regional Airline Report.
505:. Regional Airline Report.
442:Miller, R. (1 April 1991).
354:
10:
1958:
259:1.96 ft (0.60 m)
253:6.39 ft (1.95 m)
224:Specifications (TPF351-20)
218:Embraer/FMA CBA 123 Vector
119:Embraer/FMA CBA 123 Vector
82:Embraer/FMA CBA 123 Vector
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535:. July 1989. p. 15.
337:Specific fuel consumption
186:propeller synchronization
153:system and high pressure
136:
26:
21:
461:Leyes & Fleming 1999
427:Leyes & Fleming 1999
405:List of aircraft engines
302:Two-stage high-pressure
1942:1990s turboprop engines
237:General characteristics
171:free-turbine turboshaft
111:Garrett Engine Division
1893:Adaptive cycle engines
978:United States military
708:AlliedSignal/Honeywell
346:Thrust-to-weight ratio
328:Overall pressure ratio
280:centrifugal compressor
184:-limiting protection,
939:engines marked with *
317:Maximum power output:
202:tractor configuration
560:Flight International
486:Flight International
393:General Electric CT7
190:propeller feathering
167:Promavia Jet Squalus
145:-14 which power the
131:Farnborough Air Show
488:. 28 November 1990.
448:SAE Technical Paper
360:Related development
109:engine designed by
982:designation system
377:Comparable engines
77:Major applications
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818:Joint development
533:Airline Executive
507:Airline Executive
321:reduction gearbox
292:annular combustor
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161:turbofan of the
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599:. p. 484.
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628:. Reston, VA:
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198:Piaggio Avanti
194:Beech Starship
163:Fairchild T-46
149:, keeping its
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103:Garrett TPF351
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94:Garrett TPE331
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89:Developed from
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783:ALF 502/LF507
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399:Related lists
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71:May 19, 1989
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902:(Turboshaft)
875:F124/TFE1042
857:(Turboshaft)
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624:
616:Bibliography
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558:
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371:Garrett F109
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147:Jetstream 41
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1297:Turboshafts
882:(Turbofans)
848:/Honeywell:
826:CFE Company
723:Turboshafts
311:Performance
276:Compressor:
263:Dry weight:
1931:Categories
1611:LHTEC T800
1292:Turboprops
837:(Turbofan)
719:Turboprops
463:, p.
429:, p.
411:References
286:Combustors
278:Two-stage
270:Components
127:Boeing 720
68:First run
1636:Turbofans
990:Turbojets
775:Turbofans
660:cite book
652:247550535
605:0020-5168
596:Interavia
577:A12900382
569:0015-3710
541:0278-6702
515:0278-6702
257:Diameter:
246:Turboprop
229:Data from
180:provides
151:combustor
107:turboprop
40:Turboprop
1616:APW T800
1434:variants
636:(AIAA).
355:See also
1432: (
731:AGT1500
704:Garrett
298:Turbine
251:Length:
188:, auto-
155:turbine
22:TPF351
935:Note:
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765:TPF351
760:TPE331
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182:torque
143:TPE331
137:Design
1916:XA103
1911:XA102
1906:XA101
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1771:YF120
1248:YJ101
891:LHTEC
855:LV100
243:Type:
178:FADEC
125:on a
105:is a
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1659:TF33
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1626:T901
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1282:J700
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1253:J102
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1223:YJ93
1093:XJ49
1053:XJ41
1038:XJ38
920:T900
911:ATEC
880:F125
866:ITEC
794:F109
789:ATF3
666:link
648:OCLC
638:ISBN
632:and
601:ISSN
573:Gale
565:ISSN
537:ISSN
511:ISSN
332:14:1
165:and
101:The
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1320:T34
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1238:J99
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799:FX5
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465:710
431:711
196:or
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