525:
509:
253:
1973:
42:
692:
468:
A hybrid of the AE 2100A and AE 2100D3, sporting the torque-meter and interconnecting struts from the AE 2100A and the gearbox-mounted accessory gearbox from the AE 2100D3; also uses a stronger reduction gearbox, a Dowty six-bladed propeller for higher loads, and modified inlet and bypass section
286:, allowing both to be adjusted with a single lever. There are four production variants of the engine: the civil AE 2100A, and the military variants which include the AE 2100D2/D2A, AE 2100D3, AE 2100J and AE 2100P.
221:
The engine's C variant was certified on
December 20, 1993. It powered the N-250 prototype's first flight on August 10, 1995, but the N-250 aircraft program was postponed indefinitely in the late 1990s due to the
2535:
2178:
524:
2548:
214:. Testing ended in June 1994 after 47 flight hours. The engine powered the initial flight of the C-130J aircraft on April 5, 1996. By April 1997, the D3 variant had received
3508:
2528:
309:
with two stages drives the propeller through an inner shaft and a gearbox. The engine has replaceable steel blades and vanes, which are more reliable but heavier than
879:
1690:
1887:
180:
turboprop, in a US$ 500 million deal. In July 1990, Industri
Pesawat Terbang Nusantara (IPTN) of Indonesia picked the GMA 2100 as the engine for the twin-engine
1924:
320:
are rated at 6,000 shaft horsepower (4,500 kilowatts), but was derated to 4,200, 4,590, and 3,600 shp (3,130, 3,420, and 2,680 kW) for the
344:
civil-certified version of the C-130J. The gearbox has a reduction ratio of about 14 and a mean time before unscheduled removal (MTBUR) of over 35,000 hours.
2521:
1017:
278:. This core is capable of powering turboprops of up to 10,000 shp (7,500 kW). The AE 2100 is a two-shaft design, and it was the first to use dual
1892:
2171:
1711:
1761:
Kaiser, Sascha; Donnerhack, Stefan; Lundbladh, Anders; Seitz, Arne (27–29 July 2015). "A composite cycle engine concept with hecto-pressure ratio".
305:
has 16 air-blast fuel injection nozzles. The turbine that drives the compressor has two stages, with the first stage using single-crystal blades. A
244:. In October 2015, Alenia announced plans to use a 5,100-horsepower (3,800-kilowatt) uprated version of the AE 2100 as the baseline engine by 2017.
2492:
2147:
1778:
1737:
1610:
1497:
769:
407:
325:
199:
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1572:
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1182:
899:
2134:
3503:
2498:
662:
529:
858:
1697:
737:
215:
102:
957:
499:), with the required power increase from 6,000 to 10,000 shp (4,500 to 7,500 kW) estimated to cost USD$ 600 million.
3120:
1541:
508:
3113:
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784:
1897:
1410:
3182:
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1910:
1468:
3429:
2408:
1111:
2502:
444:, a twin-turboprop airliner seating up to 86 passengers and requiring about 5,000 hp (3,700 kW) of power.
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2485:
2423:
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1933:
647:
223:
156:. The engine was originally known as the GMA 2100, when Allison was a division of former corporate parent
149:
82:
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827:
389:
98:
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Moxon, Julian; Winn, Allan; Elliott, Simon; Barrie, Douglas (11 December 1991). "Quiet revolution".
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302:
268:
1380:
1206:
Premo, David J. (November 1991). "Allison flies solo into the new commuter aircraft market".
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294:
264:
192:
132:
1306:
Sweetman, Bill (October 1994). "New power for regionals". Finance, markets & industry.
3157:
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1936:
1902:
1639:
1526:
697:
559:
256:
230:
211:
86:
1436:
Woolley, David (November 1991). "Powering up the next generation of turboprop aircraft".
195:
began on August 23, 1990, and finished after over 50 hours of flight and ground testing.
811:
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1962:
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470:
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337:
185:
157:
110:
1279:"From Rotol Airscrews to Dowty Propellers: 80 years of aviation propulsion excellence"
844:
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72:
1972:
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2110:
2038:
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2004:
1952:
1618:
1505:
1278:
1188:
891:
513:
496:
218:(FAA) type certification. 2,000 of the D3 variants have been delivered as of 2018.
41:
1244:
Coniglio, Sergio (February 2010). "Military aircraft propulsion: Jets vs. props".
1107:"New regional airplanes: Fresh designs promise answer to evolving market demands"
422:
A variant proposed in 1995 and paired with Dowty R394 propellers to retrofit the
3096:
3021:
2996:
2986:
2936:
2916:
2911:
2906:
2739:
2589:
2579:
2436:
2373:
2335:
2100:
2095:
2085:
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1999:
1994:
1989:
710:
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333:
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169:
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1820:
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1325:
1317:
1312:. Vol. 49, no. 583. Minneapolis, Minnesota, U.S.A. pp. 16–18.
1261:
1253:
1215:
1158:
1120:
1091:
1054:
995:
972:
934:
836:
803:
434:, at a price after engine/propeller trade-in of USD$ 11 million per aircraft.
271:, the AE 2100 shares the same high-pressure core as that engine, as does the
188:
with a 13 ft 6 in diameter (4.11 m) Dowty R373 propeller on a
3187:
3046:
3026:
2858:
2323:
2312:
2048:
599:
556:
364:
340:, R384 on the IPTN N-250, and R391 on the C-130J military transport and the
321:
173:
145:
106:
60:
1129:
3202:
2556:
2199:
2014:
1981:
1944:
1653:"FLA finds a new home". Finance, markets & industry: Business watch.
640:
310:
275:
177:
1770:
1115:. Vol. 33, no. 18 (published October 2001). pp. R10–R14.
2126:
795:
610:
317:
17:
1149:
Caires, Greg (20 June 1997). "Allison wins C-27J engine competition".
528:
A side view of the AE 2100J engine without its casing, on display at
441:
298:
1248:. Vol. 34, no. 2. Mönch Publishing Group. pp. 77–84.
1729:
336:
propellers, including the model R381 on the Saab 2000, R414 on the
282:(full authority digital engine control) to control both engine and
1609:(Report). JPRS Report. Vol. JPRS-EST-94-014-L. Translated by
1347:"IPTN rolls out with 188 orders; Gulfstream Air signs LOI for 4".
770:"Rolls-Royce reaches services contract with USAF for C-130J Fleet"
523:
507:
279:
251:
206:
on March 19, 1994, which was conducted by
Marshall Aerospace on a
50:
1717:
Improving the efficiency of engines for large nonfighter aircraft
1802:
The
History of North American Small Gas Turbine Aircraft Engines
1573:"Allison plans to build new hybrid AE2100 for Japan's amphibian"
1496:(Report). JPRS Report. Vol. JPRS-EST-94-017. Translated by
670:: 0.460 lb/(hp⋅h) (0.209 kg/(hp⋅h); 0.280 kg/kWh)
332:, respectively. The engine uses six-bladed, all-composite blade
2517:
2160:
1906:
1018:"Rolls-Royce delivers 2,000th AE 2100D3 engine for USAF C-130J"
1765:. AIAA/SAE/ASEE Joint Propulsion Conference (51st ed.).
1696:(Report) (32nd ed.). Department of Transportation (DOT)
831:. Vol. 138, no. 4225. 18 July 1990. pp. 18+.
1490:
France-Italian ATR consortium plans two new aircraft models
1351:. Vol. 12, no. 45. 14 November 1994. p. 3.
1603:
France: Proposed engine for FLA would use SNECMA M88 core
1411:"Lockheed Martin LM-100J starts taking (a similar) shape"
1659:. Vol. 49, no. 583. October 1994. p. 14.
1183:"Alenia Aermacchi outlines performance boost for C-27J"
772:(Press release). 20 September 2017 – via ASDNews.
469:
positioning to mitigate seawater ingestion; powers the
923:
Warwick, Graham (31 August 1994). "Hercules renewed".
884:
Department of
Defense appropriations for 1995, part 3
301:
for the first five stages have variable blades. The
3458:
3201:
2857:
2555:
2464:
2432:
2401:
2322:
2198:
2125:
2047:
2013:
1980:
1943:
958:"Lockheed Martin makes delayed C-130J first flight"
1858:"Allison plans flight tests of turboprop GMA 2100"
1856:
1799:Leyes II, Richard A.; William A. Fleming (1999).
1500:(FBIS) (published 28 July 1994). pp. 30–31.
1542:"Dassault aims Atlantic at European MPA tenders"
1239:
1237:
1235:
1233:
1834:. Vol. 140, no. 4297. pp. S10+.
1601:Casamayou, Jean-Pierre (30 May – 5 June 1994).
1390:. Vol. 150, no. 4538. pp. 113+.
1201:
1199:
929:. Vol. 146, no. 4436. pp. 130+.
880:United States House Committee on Appropriations
1763:51st AIAA/SAE/ASEE Joint Propulsion Conference
1613:(FBIS) (published 8 July 1994). pp. 6–7.
1607:Science & Technology: Europe/International
1494:Science & Technology: Europe/International
263:A derivative of the Allison AE 1107C-Liberty (
2529:
2172:
1918:
1867:. Vol. 132, no. 8. pp. 36–38.
1378:Doyle, Andrew; Norris, Guy (28 August 1996).
1045:"Allison AE 2100C certified for IPTN N-250".
198:The GMA 2100D3 became the powerplant for the
8:
1898:Lockheed Martin C-130J specification booklet
990:. Vol. 195. 10 April 1997. p. 63.
986:"C-130J engine receives FAA certification".
491:A variant proposed in 1994 for the European
172:A.B. selected the GMA 2100 to power its new
1805:. Washington, DC: Smithsonian Institution.
1469:"Falcon to begin C-130 re-engine programme"
1440:. Vol. 13, no. 11. pp. 12+.
1210:. Vol. 13, no. 11. pp. 19+.
825:"Allison wins regional powerplant battle".
440:A variant offered in 1994 for the proposed
2536:
2522:
2514:
2179:
2165:
2157:
1925:
1911:
1903:
1273:
1271:
540:FAA type certificate data sheet no. TE1CH.
229:In June 1997, the AE 2100 was selected by
866:The Dowty Aerospace Gloucester Newsletter
3509:Rolls-Royce aircraft gas turbine engines
1855:Kandebo, Stanley W. (19 February 1990).
1720:. National Academies Press. pp. 29–
868:. No. 18. February 1991. p. 7.
516:C-130J Hercules ready for inspection at
1888:AE 2100 product page at rolls-royce.com
761:
1635:
1624:
1522:
1511:
31:
1691:Type certificate data sheet no. TE1CH
1611:Foreign Broadcast Information Service
1498:Foreign Broadcast Information Service
1492:. West Europe: Corporate Strategies.
408:Lockheed Martin C-130J Super Hercules
326:Lockheed Martin C-130J Super Hercules
200:Lockheed Martin C-130J Super Hercules
7:
1864:Aviation Week & Space Technology
1105:Polek, Gregory (26 November 2007).
1078:"IPTN wins approval as N-250 flies"
1415:Aerospace & Defense Technology
1180:Perry, Dominic (19 October 2015).
679:2.76 shp/lb (4.54 kW/kg)
25:
1467:Staats, Alan (12 December 1995).
1026:(Press release). 22 February 2018
49:The Rolls-Royce AE 2100 D2A on a
2499:Rolls-Royce Limited aero engines
1971:
1409:Broge, Jean L. (21 April 2016).
738:Pratt & Whitney Canada PW150
690:
530:Marine Corps Air Station Iwakuni
40:
27:Turboprop aircraft engine family
1698:Federal Aviation Administration
1128:Polek, Gregory (October 2001).
216:Federal Aviation Administration
103:Lockheed Martin C-130J Hercules
2493:Joint development aero engines
1570:Lewis, Paul (20 August 1997).
1488:Burgner, Norbert (June 1994).
1349:Commuter Regional Airline News
1153:. Vol. 195. p. 499.
1076:Lewis, Paul (15 August 1995).
1047:Commuter Regional Airline News
567:124.12 in (315.3 cm)
450:A variant offered in 1996 for
297:design, but the inlet and the
1:
2148:Joint development aeroengines
1246:Military Technology (MILTECH)
785:"G.M. engines for Saab plane"
658:36 lb/s (16.3 kg/s)
495:(which eventually became the
2547:gas turbine aircraft engine
798:. 12 July 1989. p. D4.
573:28.71 in (72.9 cm)
2433:Aero-derivative industrial
1134:Aviation International News
1112:Aviation International News
579:1,740 lb (790 kg)
512:The AE 2100D3 engines of a
176:, a 50-seat stretch of the
3525:
2503:Rolls-Royce Heritage Trust
1605:. West Europe: Aerospace.
1477:. Phoenix, Arizona, U.S.A.
1438:Commuter Air International
1208:Commuter Air International
504:Specifications (AE 2100D3)
289:The AE 2100 inherited the
2480:
2144:
1969:
1712:National Research Council
1582:. Singapore. p. 22.
663:Specific fuel consumption
456:Atlantic Third Generation
348:Variants and applications
154:Rolls-Royce North America
48:
39:
34:
1130:"New Regional Airplanes"
1023:Rolls-Royce Holdings plc
750:List of aircraft engines
460:maritime patrol aircraft
402:Lockheed C-130K Hercules
210:testbed leased from the
208:Lockheed C-130K Hercules
3504:1990s turboprop engines
1687:Rolls-Royce Corporation
1619:2027/nyp.33433016823886
1506:2027/nyp.33433016823886
892:2027/uc1.31210014044646
886:(Report). p. 491.
545:General characteristics
430:models E through H and
413:Lockheed Martin LM-100J
316:The AE 2100 engine and
3460:Adaptive cycle engines
2545:United States military
2402:Other fan-type engines
1934:Allison Engine Company
1086:. Bandung, Indonesia.
648:Overall pressure ratio
533:
521:
260:
224:Asian financial crisis
150:Allison Engine Company
83:Allison Engine Company
733:General Electric GE38
675:Power-to-weight ratio
633:Maximum power output:
527:
511:
493:Future Large Aircraft
259:with six-bladed props
255:
2188:Rolls-Royce Holdings
1831:Flight International
1689:(29 December 2017).
1579:Flight International
1548:Flight International
1474:Flight International
1387:Flight International
1083:Flight International
1049:. 21 February 1994.
964:Flight International
926:Flight International
828:Flight International
390:Alenia C-27J Spartan
202:. It made its first
99:Alenia C-27J Spartan
2491:Symbol ‡ indicates
2484:Symbol † indicates
1771:10.2514/6.2015-4028
716:Rolls-Royce AE 3007
705:Related development
482:Saab 2000 AEW&C
273:Rolls-Royce AE 3007
184:regional airliner.
142:Rolls-Royce AE 2100
2549:designation system
1634:Unknown parameter
1521:Unknown parameter
1381:"Developing power"
1287:. 21 December 2017
727:Comparable engines
534:
522:
359:Lockheed P-3 Orion
307:free power turbine
261:
242:tactical airlifter
190:Lockheed P-3 Orion
168:On July 11, 1989,
94:Major applications
3491:
3490:
2511:
2510:
2154:
2153:
1780:978-1-62410-321-6
1739:978-0-309-10399-2
967:. 16 April 1996.
518:Ramstein Air Base
452:Dassault Aviation
432:Lockheed L-100-30
303:annular combustor
269:turboshaft engine
138:
137:
16:(Redirected from
3516:
2538:
2531:
2524:
2515:
2181:
2174:
2167:
2158:
1975:
1937:aircraft engines
1927:
1920:
1913:
1904:
1876:
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1824:
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1375:
1369:
1368:
1344:
1338:
1337:
1303:
1297:
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1292:
1284:Dowty Propellers
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913:
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863:
859:"P3 flight test"
855:
849:
848:
822:
816:
815:
787:
780:
774:
773:
766:
721:Rolls-Royce T406
700:
695:
694:
693:
379:(prototype only)
295:axial compressor
265:Rolls-Royce T406
193:testbed aircraft
133:Rolls-Royce T406
129:
119:
95:
69:
44:
32:
21:
3524:
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2185:
2155:
2150:
2140:
2121:
2043:
2009:
1976:
1967:
1939:
1931:
1893:Rolls-royce.com
1884:
1879:
1861:. Cover story.
1854:
1827:
1813:
1798:
1794:
1789:
1788:
1781:
1760:
1759:
1755:
1740:
1710:
1709:
1705:
1693:
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1680:
1652:
1651:
1647:
1633:
1623:
1600:
1599:
1595:
1569:
1568:
1564:
1551:. 21 May 1996.
1539:
1538:
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1510:
1487:
1486:
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1465:
1461:
1435:
1434:
1430:
1408:
1407:
1403:
1377:
1376:
1372:
1346:
1345:
1341:
1305:
1304:
1300:
1290:
1288:
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1276:
1269:
1243:
1242:
1231:
1205:
1204:
1197:
1179:
1178:
1174:
1148:
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744:Related lists
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2437:gas turbines
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2273:Trent series
2193:and aircraft
2191:aero engines
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1792:Bibliography
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2053:Turboshafts
1627:cite report
1514:cite report
711:Allison T56
635:4,637
627:Performance
590:Compressor:
577:Dry weight:
488:AE 2100SD-7
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291:Allison T56
204:test flight
170:Saab-Scania
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3498:Categories
3178:LHTEC T800
2859:Turboprops
2424:LiftSystem
2324:Turboprops
2307:Trent 7000
2297:Trent 1000
2049:Turboprops
910:1097431953
812:A175743161
756:References
619:, 2-stage
600:Combustors
584:Components
384:AE 2100D2A
377:IPTN N-250
330:IPTN N-250
3203:Turbofans
2557:Turbojets
2497:See also
2302:Trent XWB
2292:Trent 900
2287:Trent 800
2282:Trent 700
2277:Trent 500
2213:Advance 3
2208:Advance 2
2200:Turbofans
2015:Turbofans
1982:Turbojets
1945:V engines
1873:0005-2175
1848:A11714309
1840:0015-3710
1821:247550535
1748:934667552
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1665:1423-3215
1656:Interavia
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1446:0199-2686
1423:2472-2081
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1326:199793280
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1055:1040-5402
1004:A19305553
996:0889-0404
973:0015-3710
943:A16074135
935:0015-3710
837:0015-3710
804:0362-4331
592:14-stage
571:Diameter:
557:turboprop
537:Data from
520:, Germany
426:-powered
404:(testbed)
396:AE 2100D3
365:Saab 2000
361:(testbed)
322:Saab 2000
284:propeller
174:Saab 2000
146:turboprop
107:Saab 2000
61:Turboprop
3183:APW T800
3001:variants
2465:Aircraft
2340:variants
2090:variants
1714:(2007).
882:(1994).
845:A9247977
684:See also
615:2-stage
476:AE 2100P
465:AE 2100J
458:(ATL3G)
447:AE 2100H
437:AE 2100G
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371:AE 2100C
353:AE 2100A
311:titanium
276:turbofan
178:Saab 340
35:AE 2100
2999: (
2488:engines
2486:Allison
2346:AE 2100
2338: (
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2127:Propfan
2088: (
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2061:250/T63
2028:AR.168R
2023:AE 3007
1953:VG-1410
1291:30 July
796:Reuters
668:Takeoff
611:Turbine
605:Annular
565:Length:
532:in 2019
342:LM-100J
318:gearbox
122:2,300+
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248:Design
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2313:V2500
2257:RJ500
2252:RB401
2247:RB282
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2230:EJ200
2224:BR700
1694:(PDF)
862:(PDF)
594:axial
551:Type:
334:Dowty
182:N-250
144:is a
57:Type
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