133:
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27:
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was skipped over in favor of the I-40 powered P-80 as the US's first production jet fighter. In 1945, the license to actually produce the engine was not given to
General Electric, but to Allison instead. Allison, working largely from government-owned wartime factories, could produce the engine in
267:
Along with the I-16, GE also started work on an enlarged version, known as the I-40. As the name implied, the engine was designed to provide 4,000 lbf (18 kN). Apart from size, the main difference between I-16 and the I-40 was the combustion system: the I-16 had ten reverse-flow cans,
232:, enlarged to produce significantly greater thrust, starting at 4,000 lbf (18 kN) and ending at 4,600 lbf (20 kN) with an additional low-altitude boost to 5,400 lbf (24 kN) with water-alcohol injection.
256:, but after major changes to adapt it to US production and to increase thrust, it started limited production as the I-16 in 1942, the 16 referring to its 1,600 lbf (7.1 kN) thrust. Full production started as the
268:
whereas the I-40 had 14 straight-through combustors. The development cycle was remarkably rapid. Design work started in mid-1943 and the first prototype underwent static testing on 13 January 1944.
2771:
1857:
2298:
2278:
2263:
2106:
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2537:
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1996:
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318:
A model of the J33 intended for civil use, designated the
Allison 400-C4, in 1948 became the first US gas turbine certificated for commercial transport use.
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1381:
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By the time the production lines were shut down, Allison had built over 6,600 J33's and
General Electric another 300 (mostly the early runs).
2423:
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2011:
1127:
2253:
2036:
2026:
1986:
1843:
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ran into delays, and since the I-40 would dramatically improve performance, plans were made to fit the prototypes with the I-40 instead.
2835:
132:
312:
1826:
1374:
1350:
1067:
Turbojet
History and Development 1930-1960, Volume 2: USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary
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110:
810:
70:
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521:
4,600 lbf (20.46 kN) thrust / 5,400 lbf (24.02 kN) with water-alcohol injection, powers the
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48:
2408:
261:
77:
352:
Aircraft engines of the World 1953, Aircraft engines of the World 1957, Aircraft engines of the World 1953,
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1113:
44:
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912:
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275:
189:
185:
59:
141:
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1703:
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project at the time, originally intending to power their design with a US-produced version of the
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37:
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1916:
1865:
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1225:
856:
603:
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300:
In 1958, surplus J33s were used in jet donkeys pushing dead loads at 200 knots to test
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651:
Jane's all the World's
Aircraft 1955–56 and Aircraft engines of the World 1957.
536:
453:
381:
4,600 lbf (20 kN), (USN) Used as mixed propulsion engine system with
304:
290:
283:
749:
4,600 lbf (20 kN) static dry at 11,750 rpm at sea level for take-off
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976:(11th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 46–47.
956:(15th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 65–69.
938:(11th ed.). London: Sir Isaac Pitman & Sons Ltd. pp. 52–59.
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The I-40 became important to the USAAF's plans when the I-16 powered
991:(7th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 47.
26:
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1217:
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1147:
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of about 3,000 lbf (13 kN). Production of the H-1 by
1050:(2nd ed.). Cambridge, England: Patrick Stephens Limited.
1031:. London: Jane's all the World's Aircraft Publishing Co. Ltd.
545:
Company designation, for commercial use, similar to J33-A-21.
1135:
723:
913:"Here and There : U.S. Gas Turbine Approved by C.A.A"
1088:. London: Sir Isaac Pitman & Sons. pp. 272–273.
264:
introduced common naming for all their engine projects.
802:: 1,116.15 K (1,549 °F; 843 °C) ;
770:
3,900 lbf (17 kN) at 11,000 rpm at sea level
764:
5,400 lbf (24 kN) at 11,750 rpm at sea level
732:
wet sump, pressure spray at 42 psi (2.9 bar)
462:
similar to -35, 4,600 lbf (20.46 kN) thrust.
642:
404:
Similar to the -16A, 5,850 lbf (26.02 kN)
51:. Unsourced material may be challenged and removed.
907:
905:
478:6,100 lbf (27.13 kN) thrust, powers the
468:6,100 lbf (27.13 kN) thrust, powers the
244:as a follow-on to their work with the designs of
2817:
699:single-stage double-sided centrifugal compressor
902:
708:14 can type stainless steel combustion chambers
515:6,000 lbf (26.69 kN) re-heat thrust.
503:8,200 lbf (36.48 kN) re-heat thrust.
1851:
1375:
1121:
1069:(1st ed.). Ramsbury: The Crowood Press.
806:: 958.15 K (1,265 °F; 685 °C)
1858:
1844:
1382:
1368:
1128:
1114:
887:
655:
456:with bleed air for boundary-layer control.
140:Allison J33 turbojet engine on display at
1083:
986:
971:
967:
965:
963:
951:
947:
945:
933:
793:90 lb/s (41 kg/s) at 11,750 rpm
111:Learn how and when to remove this message
1026:
726:, Kerosene (AN-F-32) or 100/130 gasoline
539:, 4,600 lbf (20.46 kN) thrust.
414:, 5,400 lbf (24.02 kN) thrust.
398:, 4,600 lbf (20.46 kN) thrust.
333:
325:
1045:
1029:Jane's all the World's Aircraft 1955–56
1020:
359:similar to -21 without water injection.
2818:
980:
960:
942:
927:
446:4,500 lbf (20.02 kN) thrust.
420:similar to -21 without water injection
252:. Their first engine was known as the
1839:
1363:
1109:
881:
624:
330:A J33 at the Finnish Air Force Museum
888:Dempewolff, Richard F. (June 1958).
240:The J33 was originally developed by
49:adding citations to reliable sources
20:
1064:
1048:World Encyclopaedia of Aero Engines
898:. Hearst Magazines. pp. 72–75.
294:quantity more quickly and cheaply.
13:
1086:Aircraft Engines of the world 1946
1039:
989:Aircraft engines of the World 1949
974:Aircraft engines of the World 1950
954:Aircraft engines of the World 1957
936:Aircraft engines of the World 1953
815:1.12 lb/(lbf⋅h) (32 g/(kN⋅s))
630:A J33 is on public display at the
375:4,600 lbf (20 kN), (USN)
14:
2847:
2836:Centrifugal-flow turbojet engines
1093:
643:Specifications (Allison J33-A-35)
535:A short life engine powering the
431:A short life engine powering the
394:A short life engine powering the
1390:GE Aircraft Engines/GE Aviation/
1174:
551:Company designation of J33-A-23.
131:
25:
1007:City of Norwich Aviation Museum
632:City of Norwich Aviation Museum
589:Lockheed F-94A / F-94B Starfire
567:
36:needs additional citations for
995:
736:
563:Company designation of the -33
557:Company designation of the -35
338:Allison J33 on display at the
235:
1:
1827:Joint development aeroengines
1351:Joint development aeroengines
874:
690:
365:4,600 lbf (20 kN),
262:United States Army Air Forces
1869:gas turbine aircraft engine
917:Flight and Aircraft Engineer
890:"Jet "Donkeys" for the Jets"
762:Take-off thrust, static wet:
680:50.5 in (128.3 cm)
497:(USAF), similar to the -16A,
219:General Electric/Allison J33
7:
1084:Wilkinson, Paul H. (1946).
987:Wilkinson, Paul H. (1949).
972:Wilkinson, Paul H. (1950).
952:Wilkinson, Paul H. (1957).
934:Wilkinson, Paul H. (1953).
828:
686:1,820 lb (830 kg)
674:107 in (271.8 cm)
584:Lockheed T-33 Shooting Star
579:Lockheed P-80 Shooting Star
321:
190:Lockheed T-33 Shooting Star
186:Lockheed P-80 Shooting Star
10:
2852:
1027:Bridgman, Leonard (1955).
923:(2059): 626. 10 June 1948.
797:Turbine inlet temperature:
142:Flugausstellung Hermeskeil
2780:
2523:
2179:
1877:
1823:
1799:
1749:
1659:
1496:
1401:
1347:
1328:
1250:
1216:
1183:
1172:
1146:
811:Specific fuel consumption
636:Horsham St Faith, Norfolk
194:Lockheed F-94A/B Starfire
139:
130:
125:
2826:Allison aircraft engines
1065:Kay, Anthony L. (2007).
869:List of aircraft engines
599:North American AJ Savage
274:was in the midst of the
1100:J33 on LeteckeMotory.cz
664:centrifugal compressor
656:General characteristics
495:United States Air Force
228:, a development of the
2831:1940s turbojet engines
2782:Adaptive cycle engines
1867:United States military
1137:Allison Engine Company
1046:Gunston, Bill (1989).
820:Thrust-to-weight ratio
783:Overall pressure ratio
768:Normal thrust, static:
619:Vought SSM-N-8 Regulus
346:
331:
166:Allison Engine Company
433:Chance-Vought Regulus
396:Chance-Vought Regulus
337:
329:
840:General Electric J31
668:with water injection
609:Martin MGM-1 Matador
594:Lockheed T2V SeaStar
254:General Electric I-A
230:General Electric J31
210:General Electric J31
45:improve this article
857:Rolls-Royce Derwent
834:Related development
604:Martin P4M Mercator
1871:designation system
1751:Aeroderivative gas
852:de Havilland Ghost
846:Comparable engines
717:single-stage axial
625:Engines on display
614:Martin MGM-13 Mace
367:United States Navy
347:
340:Museum of Aviation
332:
181:Major applications
2813:
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1833:
1832:
1357:
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1057:978-1-85260-163-8
895:Popular Mechanics
215:
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302:aircraft carrier
242:General Electric
223:centrifugal-flow
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162:General Electric
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1040:Further reading
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221:is an American
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198:SSM-N-8 Regulus
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16:Turbojet engine
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1094:External links
1092:
1091:
1090:
1081:
1076:978-1861269393
1075:
1062:
1056:
1041:
1038:
1035:
1034:
1019:
1003:"Engines List"
994:
979:
959:
941:
926:
901:
879:
878:
876:
873:
872:
871:
860:
859:
854:
843:
842:
830:
827:
826:
825:
816:
807:
794:
791:Air mass flow:
788:
778:
777:
776:
775:
774:
773:
772:
771:
765:
752:
751:
738:
735:
734:
733:
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718:
709:
700:
692:
689:
688:
687:
681:
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552:
549:
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537:Martin Matador
533:
530:
519:
516:
513:
510:
509:similar to -35
507:
504:
501:
498:
492:
489:
488:similar to -35
486:
483:
476:
473:
466:
463:
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863:Related lists
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574:Convair XF-92
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554:Model 400-C13
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527:Lockheed T-33
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412:Grumman F9F-7
410:Powering the
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62: –
61:
60:"Allison J33"
57:
56:Find sources:
50:
46:
40:
39:
34:This article
32:
28:
23:
22:
19:
1901:
1442:
1392:GE Aerospace
1192:
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1010:. Retrieved
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646:
568:Applications
560:Model 400-D9
548:Model 400-C5
542:Model 400-C4
523:Lockheed T2V
480:Lockheed T2V
470:Lockheed T2V
349:
348:
317:
299:
296:
288:
270:
266:
250:World War II
239:
218:
216:
107:
98:
88:
81:
74:
67:
55:
43:Please help
38:verification
35:
18:
2186:Turboshafts
1666:turboshafts
1256:Turboshafts
737:Performance
730:Oil system:
697:Compressor:
684:Dry weight:
307:cables and
280:Halford H-1
236:Development
2820:Categories
2500:LHTEC T800
2181:Turboprops
1661:Turboprops
1252:Turboprops
875:References
721:Fuel type:
704:Combustors
691:Components
387:Martin P4M
350:Data from:
344:Robins AFB
226:jet engine
172:First run
71:newspapers
2525:Turbofans
1879:Turbojets
1615:F404/F412
1498:Turbofans
1403:Turbojets
1218:Turbofans
1185:Turbojets
1148:V engines
1012:29 August
678:Diameter:
648:Data from
475:J33-A-24A
428:J33-A-18A
423:J33-A-17A
407:J33-A-16A
313:Lakehurst
309:tailhooks
260:when the
101:July 2012
2505:APW T800
2323:variants
1801:Propfans
1704:H-Series
1674:Catalyst
1576:Passport
1538:CJ805-23
1506:Affinity
1293:variants
829:See also
743:Maximum
666:turbojet
532:J33-A-37
518:J33-A-35
512:J33-A-33
506:J33-A-31
500:J33-A-29
491:J33-A-27
485:J33-A-25
465:J33-A-24
459:J33-A-23
449:J33-A-22
443:J33-A-21
438:J33-A-20
417:J33-A-17
401:J33-A-16
391:J33-A-14
378:J33-A-10
322:Variants
272:Lockheed
152:Turbojet
2321: (
1330:Propfan
1291: (
1269:AE 2100
1264:250/T63
1231:AR.168R
1226:AE 3007
1156:VG-1410
713:Turbine
672:Length:
372:J33-A-8
362:J33-A-6
356:J33-A-4
248:during
85:scholar
1791:LMS100
1786:LM9000
1781:LM6000
1776:LM2500
1771:LM1600
1766:LM1500
1558:GP7000
1526:CFE738
1426:GE4/J5
1338:578-DX
1166:V-3420
1161:V-1710
1073:
1054:
745:thrust
87:
80:
73:
66:
58:
2805:XA103
2800:XA102
2795:XA101
2790:XA100
2660:YF120
2137:YJ101
1761:LM500
1651:XA102
1646:XA100
1604:YF120
1564:HF120
1532:CFM56
1521:CF700
1488:YJ101
1416:CJ805
1411:CJ610
787:4.4:1
662:Type:
369:(USN)
276:XP-80
175:1942
148:Type
92:JSTOR
78:books
2772:F415
2767:F414
2762:F412
2757:F408
2752:F405
2747:F404
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2605:F105
2600:F104
2595:F103
2590:F102
2585:F101
2580:F100
2573:TF41
2568:TF39
2563:TF37
2558:TF35
2553:TF34
2548:TF33
2543:TF32
2538:TF31
2533:TF30
2515:T901
2510:T900
2495:T708
2490:T706
2485:T703
2480:T702
2475:T701
2470:T700
2463:T408
2458:T407
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2443:T400
2436:T101
2431:T100
2171:J700
2164:J403
2159:J402
2154:J401
2149:J400
2142:J102
2132:J100
2112:YJ93
1982:XJ49
1942:XJ41
1927:XJ38
1814:RISE
1809:GE36
1741:T901
1736:T700
1731:T408
1726:T407
1699:GE38
1694:GE27
1689:CT64
1684:CT58
1664:and
1641:TF39
1636:TF34
1631:RM16
1625:RM12
1620:F414
1609:F136
1599:F118
1594:F110
1588:F108
1583:F101
1570:LEAP
1553:GEnx
1548:GE9X
1543:GE90
1516:CF34
1478:YJ93
1319:T800
1314:T701
1309:T406
1242:TF41
1237:TF32
1208:J102
1102:(cs)
1071:ISBN
1052:ISBN
1014:2023
921:Llll
824:2.53
724:JP-4
525:and
291:P-59
217:The
126:J33
64:news
2424:T80
2419:T78
2414:T76
2409:T74
2404:T73
2399:T72
2394:T71
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2199:T31
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2127:J99
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2117:J95
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2102:J89
2097:J87
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2072:J75
2067:J73
2062:J71
2057:J69
2052:J67
2047:J65
2042:J63
2037:J61
2032:J60
2027:J59
2022:J58
2017:J57
2012:J56
2007:J55
2002:J54
1997:J53
1992:J52
1987:J51
1977:J48
1972:J47
1967:J46
1962:J45
1957:J44
1952:J43
1947:J42
1937:J40
1932:J39
1922:J37
1917:J36
1912:J35
1907:J34
1902:J33
1897:J32
1892:J31
1887:J30
1721:T64
1716:T58
1711:T31
1679:CT7
1511:CF6
1483:J97
1473:J87
1468:J85
1463:J79
1458:J73
1453:J47
1448:J35
1443:J33
1438:J31
1431:I-A
1421:GE1
1304:T78
1299:T61
1289:T56
1284:T54
1279:T40
1274:T38
1203:J71
1198:J35
1193:J33
804:JPT
800:TIT
634:in
385:on
311:at
258:J31
47:by
2822::
1825:†
1349:†
1005:.
962:^
944:^
919:.
915:.
904:^
892:.
342:,
315:.
2325:)
2183:/
1859:e
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1816:†
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1254:/
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114:)
108:(
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99:(
89:·
82:·
75:·
68:·
41:.
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