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requirement for a helicopter turboshaft to weigh under 400 lb (180 kg) while delivering 800 hp (600 kW). The engine
General Electric eventually built weighed only 250 lb (110 kg) and delivered 1,050 hp (780 kW) and was soon ordered into production. First flight
127:
engine developed for helicopter use. First run in 1955, it remained in production until 1984, by which time some 6,300 units had been built. On July 1, 1959, it became the first turbine engine to gain FAA certification for civil helicopter use. The engine was license-built and further developed by
206:
180:
an all-axial compressor. Most other turboshafts in this power bracket have a centrifugal unit as a final compressor stage. As a result, the blades at the rear of the compressor are very small (less than 0.5in high) and extremely
476:
turbine cars entered in the 1968 Indianapolis 500 race were powered by T58s. The cars were found to be using variable inlets to get around the USAC regulations on the maximum allowable inlet size and were disqualified.
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compressor handling at part speed is facilitated by several rows of variable pitch stators at the front part of the unit. This was a fairly novel feature when the engine was first introduced.
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a single stage power turbine. which delivers power to the rear of the engine. The hot exhaust stream is diverted sideways, away from the output shaft.
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198:, developing 1,400 hp (1,044 kW). The most powerful version, the T58-GE-16, produces 1,870 hp (1,390 kW).
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Two T58s, converted to turbojets by the removal of the power turbines, were used as the engines on the
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the combustor is a straight-through annular design, rather than reverse flow.
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819:
773:"gas generator | tw snalt | reduction gear | 1958 | 0077 | Flight Archive"
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0.64 lb/(hp⋅h) (0.39 kg/(kW⋅h)) at maximum continuous rating
349:
Licensed production and development of the T58 in the United
Kingdom.
205:
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992:
852:'Rodger Ward's Indy 500 Preview; Will the Turbines Takeover?'
176:
A number of unusual features are incorporated into the T58:
658:
6.1 hp/lb (10.0 kW/kg) without reduction gearbox
876:"About the General Electric T58 (series) Turbine Engine"
953:(Report). Type Certificate Data Sheet (16th ed.).
972:(Report). Type Certificate Data Sheet (1st ed.).
210:
Inspection of a T58 engine before installation in a
2409:
2152:
1808:
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1,400 hp (1,000 kW) 2-stage power turbine
319:1,500 hp (1,100 kW) commercial T58-GE-10
194:The main production version of the engine was the
547:391 lb (177 kg) with reduction gearbox
486:There is a YT58-GE-2A cutaway on display at the
911:. Wellingborough: Patrick Stephens. p. 65.
812:"Military Turboshaft/Turboprop Specifications"
1480:
1004:
897:. London: Sampson, Low, Marston & Co Ltd.
640:12.4 lb/s (5.62 kg/s) at 26,300 rpm
8:
1487:
1473:
1465:
1011:
997:
989:
27:American turboshaft engine for helicopters
893:Taylor, John W.R. FRHistS. ARAeS (1962).
169:in 1957, and civil certification for the
895:Jane's All the World's Aircraft 1962-63
713:
582:with 16 burner nozzles on two manifolds
754:
743:
727:, June 24, 1963, v. 78, no. 25, p. 79.
173:variant was obtained two years later.
29:
7:
725:Aviation Week & Space Technology
909:World Encyclopedia of Aero Engines
540:285 lb (129 kg) without
334:Ishikawajima-Harima T58-IHI-8B BLC
328:Ishikawajima-Harima CT58-IHI-140-1
322:Ishikawajima-Harima CT58-IHI-110-1
160:Development commenced with a 1953
25:
2455:General Electric aircraft engines
361:Aerospatiale SA 321K Super Frelon
1019:GE Aircraft Engines/GE Aviation/
865:. NEAM. Retrieved on 2013-08-16.
669:
38:
968:Federal Aviation Administration
949:Federal Aviation Administration
625:1,250 hp (932.12 kW)
93:Boeing Vertol CH-46 Sea Knight
1:
1456:Joint development aeroengines
492:Bradley International Airport
331:1,400 hp (1,000 kW)
325:1,400 hp (1,000 kW)
313:1,350 hp (1,010 kW)
301:1,500 hp (1,100 kW)
295:1,500 hp (1,100 kW)
289:1,870 hp (1,390 kW)
277:1,400 hp (1,000 kW)
271:1,350 hp (1,010 kW)
265:1,350 hp (1,010 kW)
247:1,500 hp (1,100 kW)
1498:gas turbine aircraft engine
601:1× free power turbine stage
307:1,050 hp (780 kW)
259:1,250 hp (930 kW)
253:1,250 hp (930 kW)
236:1,290 hp (960 kW)
230:1,325 hp (988 kW)
224:1,290 hp (960 kW)
144:, and also manufactured by
2476:
580:Annular combustion chamber
525:55 in (1,397 mm)
455:for layer boundary control
18:General Electric T58-GE-16
1452:
798:January 15, 2008, at the
645:Specific fuel consumption
499:Specifications (T58-GE-8)
37:
32:
2460:1950s turboshaft engines
702:List of aircraft engines
531:16 in (406 mm)
509:General characteristics
428:Sikorsky HH-52 Seaguard
412:Piasecki XH-21D Shawnee
391:Boeing CH-46 Sea Knight
142:Klöckner-Humboldt-Deutz
2411:Adaptive cycle engines
1496:United States military
907:Gunston, Bill (1986).
842:Retrieved 28 June 2011
630:Overall pressure ratio
488:New England Air Museum
418:Sikorsky SH-3 Sea King
215:
156:Design and development
101:Sikorsky SH-3 Sea King
942:(September 4, 2018).
654:Power-to-weight ratio
623:Maximum power output:
518:Free power turboshaft
467:Maverick TwinJet 1200
209:
916:GE Aviation T58 page
777:www.flightglobal.com
494:, Windsor Locks, CT
423:Sikorsky HH-3B/C/E/F
407:Kaman SH-2 Seasprite
121:General Electric T58
97:Kaman SH-2 Seasprite
961:(August 10, 1970).
959:Ishikawajima-Harima
721:Production Briefing
684:Related development
1500:designation system
1380:Aeroderivative gas
932:2010-09-26 at the
921:2011-06-20 at the
838:2016-03-05 at the
816:www.jet-engine.net
598:turbine stages and
481:Engines on display
216:
165:was on a modified
88:Major applications
2442:
2441:
1462:
1461:
863:Engine Collection
753:Missing or empty
740:: 52. March 1960.
690:Rolls-Royce Gnome
611:Aviation kerosene
542:reduction gearbox
375:AgustaBell AB204B
365:Israeli Air Force
345:Rolls-Royce Gnome
132:in the UK as the
117:
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111:Rolls-Royce Gnome
16:(Redirected from
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1024:aircraft engines
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984:Minijets website
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940:General Electric
927:T58 history page
912:
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878:. Archived from
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833:MiniJets Website
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818:. Archived from
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779:. Archived from
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380:Bell UH-1F/TH-1F
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339:Shin Meiwa PS-1
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123:is an American
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696:Related lists
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1021:GE Aerospace
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755:|title=
746:cite journal
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370:Agusta A.101
354:Applications
217:
195:
193:
175:
170:
159:
138:West Germany
130:de Havilland
120:
118:
1815:Turboshafts
1295:turboshafts
617:Performance
561:Compressor:
535:Dry weight:
402:Kaman K-16B
82:April 1955
73:GE Aviation
2449:Categories
2129:LHTEC T800
1810:Turboprops
1290:Turboprops
708:References
608:Fuel type:
575:Combustors
568:compressor
565:axial-flow
555:Components
414:(Model 71)
363:- Used by
341:BLC system
316:CT58-140-1
310:CT58-110-1
304:CT58-100-1
298:T58-GE-402
292:T58-GE-100
214:helicopter
146:Alfa Romeo
125:turboshaft
79:First run
51:Turboshaft
2154:Turbofans
1508:Turbojets
1244:F404/F412
1127:Turbofans
1032:Turbojets
563:10-stage
529:Diameter:
504:Data from
385:Bell X-22
286:T58-GE-16
280:T58-GE-14
274:T58-GE-10
268:T58-GE-8F
262:T58-GE-8E
256:T58-GE-8B
196:T58-GE-10
136:, in the
107:Variants
2134:APW T800
1952:variants
1430:Propfans
1333:H-Series
1303:Catalyst
1205:Passport
1167:CJ805-23
1135:Affinity
930:Archived
919:Archived
836:Archived
796:Archived
663:See also
250:T58-GE-6
244:T58-GE-5
239:T58-GE-4
233:T58-GE-3
227:T58-GE-2
221:T58-GE-1
202:Variants
171:CT58-100
148:and the
1950: (
587:Turbine
523:Length:
162:US Navy
1420:LMS100
1415:LM9000
1410:LM6000
1405:LM2500
1400:LM1600
1395:LM1500
1187:GP7000
1155:CFE738
1055:GE4/J5
398:(YT58)
387:(YT58)
2434:XA103
2429:XA102
2424:XA101
2419:XA100
2289:YF120
1766:YJ101
1390:LM500
1280:XA102
1275:XA100
1233:YF120
1193:HF120
1161:CFM56
1150:CF700
1117:YJ101
1045:CJ805
1040:CJ610
970:(FAA)
951:(FAA)
723:. //
634:8.3:1
515:Type:
461:Other
181:thin.
134:Gnome
47:Type
2401:F415
2396:F414
2391:F412
2386:F408
2381:F405
2376:F404
2371:F402
2366:F401
2361:F400
2354:F138
2349:F137
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2229:F104
2224:F103
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2214:F101
2209:F100
2202:TF41
2197:TF39
2192:TF37
2187:TF35
2182:TF34
2177:TF33
2172:TF32
2167:TF31
2162:TF30
2144:T901
2139:T900
2124:T708
2119:T706
2114:T703
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1771:J102
1761:J100
1741:YJ93
1611:XJ49
1571:XJ41
1556:XJ38
1443:RISE
1438:GE36
1370:T901
1365:T700
1360:T408
1355:T407
1328:GE38
1323:GE27
1318:CT64
1313:CT58
1293:and
1270:TF39
1265:TF34
1260:RM16
1254:RM12
1249:F414
1238:F136
1228:F118
1223:F110
1217:F108
1212:F101
1199:LEAP
1182:GEnx
1177:GE9X
1172:GE90
1145:CF34
1107:YJ93
963:E1PC
925:and
759:help
472:The
337:For
119:The
33:T58
2053:T80
2048:T78
2043:T76
2038:T74
2033:T73
2028:T72
2023:T71
2018:T70
2013:T69
2008:T68
2003:T67
1998:T66
1993:T65
1988:T64
1983:T63
1978:T62
1973:T61
1968:T60
1963:T58
1958:T57
1948:T56
1943:T55
1938:T54
1933:T53
1928:T52
1923:T51
1918:T50
1913:T49
1908:T48
1903:T47
1898:T46
1893:T45
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1878:T42
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1833:T33
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