196:
29:
660:
153:
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
116:
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
169:
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
465:
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.
195:
173:
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.
1996:
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2011:
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918:
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1604:
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2443:
907:
1444:
992:
187:, 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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with variable inlet guide vanes, and variable incidence stators in first three stages
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the combustor is a straight-through annular design, rather than reverse flow.
51:
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762:"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
2127:
1986:
1966:
1798:
1278:
563:
373:
338:
Licensed production and development of the T58 in the United
Kingdom.
2142:
1496:
1115:
1020:
599:
1418:
575:
150:
841:'Rodger Ward's Indy 500 Preview; Will the Turbines Takeover?'
165:
A number of unusual features are incorporated into the T58:
647:
6.1 hp/lb (10.0 kW/kg) without reduction gearbox
865:"About the General Electric T58 (series) Turbine Engine"
942:(Report). Type Certificate Data Sheet (16th ed.).
961:(Report). Type Certificate Data Sheet (1st ed.).
655:
199:
Inspection of a T58 engine before installation in a
946:
272:
1,400 hp (1,000 kW) 2-stage power turbine
308:1,500 hp (1,100 kW) commercial T58-GE-10
183:The main production version of the engine was the
2435:
927:
536:391 lb (177 kg) with reduction gearbox
475:There is a YT58-GE-2A cutaway on display at the
900:. Wellingborough: Patrick Stephens. p. 65.
801:"Military Turboshaft/Turboprop Specifications"
1469:
993:
886:. London: Sampson, Low, Marston & Co Ltd.
629:12.4 lb/s (5.62 kg/s) at 26,300 rpm
487:
1476:
1462:
1000:
986:
497:
16:American turboshaft engine for helicopters
882:Taylor, John W.R. FRHistS. ARAeS (1962).
875:
158:in 1957, and civil certification for the
144:
194:
895:
884:Jane's All the World's Aircraft 1962-63
571:with 16 burner nozzles on two manifolds
2436:
881:
716:, June 24, 1963, v. 78, no. 25, p. 79.
162:variant was obtained two years later.
1457:
981:
469:
714:Aviation Week & Space Technology
13:
898:World Encyclopedia of Aero Engines
529:285 lb (129 kg) without
323:Ishikawajima-Harima T58-IHI-8B BLC
317:Ishikawajima-Harima CT58-IHI-140-1
311:Ishikawajima-Harima CT58-IHI-110-1
149:Development commenced with a 1953
14:
2460:
2444:General Electric aircraft engines
966:
350:Aerospatiale SA 321K Super Frelon
1008:GE Aircraft Engines/GE Aviation/
854:. NEAM. Retrieved on 2013-08-16.
658:
27:
957:Federal Aviation Administration
938:Federal Aviation Administration
342:
857:
845:
834:
815:
793:
776:
754:
719:
703:
614:1,250 hp (932.12 kW)
605:
82:Boeing Vertol CH-46 Sea Knight
1:
1445:Joint development aeroengines
696:
543:
481:Bradley International Airport
320:1,400 hp (1,000 kW)
314:1,400 hp (1,000 kW)
302:1,350 hp (1,010 kW)
290:1,500 hp (1,100 kW)
284:1,500 hp (1,100 kW)
278:1,870 hp (1,390 kW)
266:1,400 hp (1,000 kW)
260:1,350 hp (1,010 kW)
254:1,350 hp (1,010 kW)
236:1,500 hp (1,100 kW)
1487:gas turbine aircraft engine
7:
651:
590:1× free power turbine stage
296:1,050 hp (780 kW)
248:1,250 hp (930 kW)
242:1,250 hp (930 kW)
225:1,290 hp (960 kW)
219:1,325 hp (988 kW)
213:1,290 hp (960 kW)
190:
133:, and also manufactured by
10:
2465:
569:Annular combustion chamber
514:55 in (1,397 mm)
444:for layer boundary control
2398:
2141:
1797:
1495:
1441:
1417:
1367:
1277:
1114:
1019:
787:January 15, 2008, at the
634:Specific fuel consumption
488:Specifications (T58-GE-8)
26:
21:
2449:1950s turboshaft engines
691:List of aircraft engines
520:16 in (406 mm)
449:
498:General characteristics
417:Sikorsky HH-52 Seaguard
401:Piasecki XH-21D Shawnee
380:Boeing CH-46 Sea Knight
131:Klöckner-Humboldt-Deutz
2400:Adaptive cycle engines
1485:United States military
896:Gunston, Bill (1986).
831:Retrieved 28 June 2011
619:Overall pressure ratio
477:New England Air Museum
407:Sikorsky SH-3 Sea King
204:
145:Design and development
90:Sikorsky SH-3 Sea King
931:(September 4, 2018).
643:Power-to-weight ratio
612:Maximum power output:
507:Free power turboshaft
456:Maverick TwinJet 1200
198:
905:GE Aviation T58 page
766:www.flightglobal.com
483:, Windsor Locks, CT
412:Sikorsky HH-3B/C/E/F
396:Kaman SH-2 Seasprite
110:General Electric T58
86:Kaman SH-2 Seasprite
950:(August 10, 1970).
948:Ishikawajima-Harima
710:Production Briefing
673:Related development
1489:designation system
1369:Aeroderivative gas
921:2010-09-26 at the
910:2011-06-20 at the
827:2016-03-05 at the
805:www.jet-engine.net
587:turbine stages and
470:Engines on display
205:
154:was on a modified
77:Major applications
2431:
2430:
1451:
1450:
852:Engine Collection
742:Missing or empty
729:: 52. March 1960.
679:Rolls-Royce Gnome
600:Aviation kerosene
531:reduction gearbox
364:AgustaBell AB204B
354:Israeli Air Force
334:Rolls-Royce Gnome
121:in the UK as the
106:
105:
100:Rolls-Royce Gnome
2456:
1478:
1471:
1464:
1455:
1454:
1013:aircraft engines
1002:
995:
988:
979:
978:
973:Minijets website
962:
943:
929:General Electric
916:T58 history page
901:
888:
887:
879:
873:
872:
867:. Archived from
861:
855:
849:
843:
838:
832:
822:MiniJets Website
819:
813:
812:
807:. Archived from
797:
791:
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773:
768:. Archived from
758:
752:
751:
745:
740:
738:
730:
723:
717:
707:
668:
663:
662:
661:
442:Shin Meiwa US-1A
422:Sikorsky S-61L/N
369:Bell UH-1F/TH-1F
78:
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1371:turbine engines
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923:Wayback Machine
912:Wayback Machine
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666:Aviation portal
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328:Shin Meiwa PS-1
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139:IHI Corporation
112:is an American
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871:on 2011-11-24.
856:
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685:Related lists
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432:Sikorsky S-67
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1010:GE Aerospace
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744:|title=
735:cite journal
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359:Agusta A.101
343:Applications
206:
184:
182:
164:
159:
148:
127:West Germany
119:de Havilland
109:
107:
1804:Turboshafts
1284:turboshafts
606:Performance
550:Compressor:
524:Dry weight:
391:Kaman K-16B
71:April 1955
62:GE Aviation
2438:Categories
2118:LHTEC T800
1799:Turboprops
1279:Turboprops
697:References
597:Fuel type:
564:Combustors
557:compressor
554:axial-flow
544:Components
403:(Model 71)
352:- Used by
330:BLC system
305:CT58-140-1
299:CT58-110-1
293:CT58-100-1
287:T58-GE-402
281:T58-GE-100
203:helicopter
135:Alfa Romeo
114:turboshaft
68:First run
40:Turboshaft
2143:Turbofans
1497:Turbojets
1233:F404/F412
1116:Turbofans
1021:Turbojets
552:10-stage
518:Diameter:
493:Data from
374:Bell X-22
275:T58-GE-16
269:T58-GE-14
263:T58-GE-10
257:T58-GE-8F
251:T58-GE-8E
245:T58-GE-8B
185:T58-GE-10
125:, in the
96:Variants
2123:APW T800
1941:variants
1419:Propfans
1322:H-Series
1292:Catalyst
1194:Passport
1156:CJ805-23
1124:Affinity
919:Archived
908:Archived
825:Archived
785:Archived
652:See also
239:T58-GE-6
233:T58-GE-5
228:T58-GE-4
222:T58-GE-3
216:T58-GE-2
210:T58-GE-1
191:Variants
160:CT58-100
137:and the
1939: (
576:Turbine
512:Length:
151:US Navy
1409:LMS100
1404:LM9000
1399:LM6000
1394:LM2500
1389:LM1600
1384:LM1500
1176:GP7000
1144:CFE738
1044:GE4/J5
387:(YT58)
376:(YT58)
2423:XA103
2418:XA102
2413:XA101
2408:XA100
2278:YF120
1755:YJ101
1379:LM500
1269:XA102
1264:XA100
1222:YF120
1182:HF120
1150:CFM56
1139:CF700
1106:YJ101
1034:CJ805
1029:CJ610
959:(FAA)
940:(FAA)
712:. //
623:8.3:1
504:Type:
450:Other
170:thin.
123:Gnome
36:Type
2390:F415
2385:F414
2380:F412
2375:F408
2370:F405
2365:F404
2360:F402
2355:F401
2350:F400
2343:F138
2338:F137
2333:F136
2328:F135
2323:F130
2318:F129
2313:F128
2308:F127
2303:F126
2298:F125
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2273:F119
2268:F118
2263:F117
2258:F113
2253:F112
2248:F110
2243:F109
2238:F108
2233:F107
2228:F106
2223:F105
2218:F104
2213:F103
2208:F102
2203:F101
2198:F100
2191:TF41
2186:TF39
2181:TF37
2176:TF35
2171:TF34
2166:TF33
2161:TF32
2156:TF31
2151:TF30
2133:T901
2128:T900
2113:T708
2108:T706
2103:T703
2098:T702
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1789:J700
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1777:J402
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1767:J400
1760:J102
1750:J100
1730:YJ93
1600:XJ49
1560:XJ41
1545:XJ38
1432:RISE
1427:GE36
1359:T901
1354:T700
1349:T408
1344:T407
1317:GE38
1312:GE27
1307:CT64
1302:CT58
1282:and
1259:TF39
1254:TF34
1249:RM16
1243:RM12
1238:F414
1227:F136
1217:F118
1212:F110
1206:F108
1201:F101
1188:LEAP
1171:GEnx
1166:GE9X
1161:GE90
1134:CF34
1096:YJ93
952:E1PC
914:and
748:help
461:The
326:For
108:The
22:T58
2042:T80
2037:T78
2032:T76
2027:T74
2022:T73
2017:T72
2012:T71
2007:T70
2002:T69
1997:T68
1992:T67
1987:T66
1982:T65
1977:T64
1972:T63
1967:T62
1962:T61
1957:T60
1952:T58
1947:T57
1937:T56
1932:T55
1927:T54
1922:T53
1917:T52
1912:T51
1907:T50
1902:T49
1897:T48
1892:T47
1887:T46
1882:T45
1877:T44
1872:T43
1867:T42
1862:T41
1857:T40
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1842:T37
1837:T36
1832:T35
1827:T34
1822:T33
1817:T31
1812:T30
1745:J99
1740:J97
1735:J95
1725:J91
1720:J89
1715:J87
1710:J85
1705:J83
1700:J81
1695:J79
1690:J75
1685:J73
1680:J71
1675:J69
1670:J67
1665:J65
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1655:J61
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