Allison Engine Company: Difference between revisions
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| successor = [[Rolls-Royce North America|Rolls-Royce Corporation]] |
| successor = [[Rolls-Royce North America|Rolls-Royce Corporation]] |
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| founder = [[James A. Allison|James Allison]] |
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The '''Allison Engine Company''' was a U.S. [[aircraft engine]] manufacturer. |
The '''Allison Engine Company''' was a U.S. [[aircraft engine]] manufacturer. In 1929, shortly after the death of [[James A. Allison|James Allison]], the company was purchased by the [[Fisher Body|Fisher brothers]]. Fisher sold the company to [[General Motors Corporation|General Motors]], who owned it for most of its history. The company was acquired by [[Rolls-Royce plc]] in 1995 to become a subsidiary, [[Rolls-Royce North America|Rolls-Royce Corporation]].<ref>John Leonard's articles in various issues of the Allison Branch newsletters</ref> |
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==History== |
==History== |
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===Early work=== |
===Early work=== |
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Originally known as the Indianapolis Speedway Team Company, it changed its name numerous times to the Allison Speedway Team Company, the Allison Experimental Company and last as the Allison Engineering Company before becoming a division of [[General Motors Corporation|General Motors]]. |
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Allison started as an engine and car "hot rodding" company servicing the [[Indianapolis Motor Speedway]] in [[Indianapolis]]. Its only regular production line item was steel-backed lead bushings, used as bearings in various aircraft engines. It also built various drive shafts, extensions and gear chains for high power engines, on demand. Another, smaller, business was the conversion of older [[Liberty engine]]s to more powerful models, both for aircraft and marine use. |
Allison started as an engine and car "hot rodding" company servicing the [[Indianapolis Motor Speedway]] in [[Indianapolis]]. Its only regular production line item was steel-backed lead bushings, used as bearings in various aircraft engines. It also built various drive shafts, extensions and gear chains for high power engines, on demand. Another, smaller, business was the conversion of older [[Liberty engine]]s to more powerful models, both for aircraft and marine use. |
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The first Allison was Manufacturer Serial No. 1, AAC S/N 25-521, an X-4520, a 12-cylinder air-cooled 4-bank “X” configured engine designed by the Army Air Corps and built by the Allison Engineering Company in 1925. |
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In the late 1920s the [[United States Army]] funded the development of a series of high-power engines, as part of its [[hyper engine]] series, which it intended to produce on [[Continental Motors Company|Continental Motors]]' production lines. Allison's manager, [[N.H. Gilman]], decided to experiment with his own high-power cylinder design. The result was presented to the Army in 1928, which turned down the development proposal. |
In the late 1920s the [[United States Army]] funded the development of a series of high-power engines, as part of its [[hyper engine]] series, which it intended to produce on [[Continental Motors Company|Continental Motors]]' production lines. Allison's manager, [[N.H. Gilman]], decided to experiment with his own high-power cylinder design. The result was presented to the Army in 1928, which turned down the development proposal. |
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Revision as of 03:06, 11 May 2011
 | This article needs additional citations for verification. (December 2010) |
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| Industrie | Aircraft enginess |
|---|---|
| Gründer | James Allison |
| Fate | Acquired |
| Successor | Rolls-Royce Corporation |
| Parent | General Motors Corporation |
The Allison Engine Company was a U.S. aircraft engine manufacturer. In 1929, shortly after the death of James Allison, the company was purchased by the Fisher brothers. Fisher sold the company to General Motors, who owned it for most of its history. The company was acquired by Rolls-Royce plc in 1995 to become a subsidiary, Rolls-Royce Corporation.[1]
History
Early work
Originally known as the Indianapolis Speedway Team Company, it changed its name numerous times to the Allison Speedway Team Company, the Allison Experimental Company and last as the Allison Engineering Company before becoming a division of General Motors.
Allison started as an engine and car "hot rodding" company servicing the Indianapolis Motor Speedway in Indianapolis. Its only regular production line item was steel-backed lead bushings, used as bearings in various aircraft engines. It also built various drive shafts, extensions and gear chains for high power engines, on demand. Another, smaller, business was the conversion of older Liberty engines to more powerful models, both for aircraft and marine use.
The first Allison was Manufacturer Serial No. 1, AAC S/N 25-521, an X-4520, a 12-cylinder air-cooled 4-bank “X” configured engine designed by the Army Air Corps and built by the Allison Engineering Company in 1925.
In the late 1920s the United States Army funded the development of a series of high-power engines, as part of its hyper engine series, which it intended to produce on Continental Motors' production lines. Allison's manager, N.H. Gilman, decided to experiment with his own high-power cylinder design. The result was presented to the Army in 1928, which turned down the development proposal.
In 1929, shortly after the death of James Allison, the company was purchased by the Fisher brothers, who instructed it to use the cylinder design for a six cylinder engine for a "family aircraft". Before work on this design had progressed very far, Fisher sold the company to General Motors, which ended development due to financial pressures of the Great Depression. Nevertheless Gilman pressed ahead with the cylinder design, building a "paper project" V-12 engine. The Army was once again uninterested, but instead suggested Allison try selling it to the United States Navy. The Navy agreed to fund development of A and B models to a very limited degree for its airships, until the crash of the USS Macon in 1935, when the Navy's need for a 1,000 hp (750 kW) engine disappeared.
V-1710
By this point the Army had become more interested in the design, and asked Allison to continue with a new "C" model. They had few funds of their own to invest, and Allison supported much of the development out of their own pocket. The V-1710-C first flew on 14 December 1936 in the Consolidated A-11A testbed. The V-1710-C6 successfully completed the Army 150 hour Type Test on 23 April 1937, at 1,000 hp (750 kW), the first engine of any type to do so. By this point all of the other Army engine projects had been cancelled or withdrawn, leaving the V-1710 as the only modern design available. It was soon found as the primary powerplant of the new generation of United States Army Air Corps (USAAC) fighters, the P-38 Lightning, P-39 Airacobra and P-40 Warhawk.
The Army had been leaning heavily towards exhaust-driven turbochargers instead of the more common mechanically-driven superchargers, feeling that their added performance more than made up for the added complexity. Thus little effort was invested in equipping the V-1710 with a reasonable supercharger, and when placed in aircraft designs like the P-39 or P-40 which lacked the room for a turbo the engine suffered tremendously at higher altitudes. It was for this reason in particular that the V-1710 was later removed from the P-51 Mustang and replaced with the Rolls-Royce Merlin.
Post-war
With the need for the V-1710 winding down at the end of the war, Allison found itself with a massive production infrastructure that was no longer needed. For this reason, in 1947, the Army decided to take General Electric's versions of Frank Whittle's jet engines and give them to Allison to produce instead. The main production model was GE's 4,000 lbf (18 kN) I-40, produced as the Allison J33. By the time production ended in 1955, Allison had produced over 7,000 J33s.
Allison also took over GE's axial flow engine design, becoming the Allison J35. The J35 was the primary powerplant for the F-84 Thunderjet and F-89 Scorpion, as well as appearing on numerous prototype designs. The J35 also finished production in 1955, by which point over 14,000 had been delivered.
Allison also started the development of a series of turboprop engines for the U.S. Navy, starting with the T38 and a "twinned" version as the T40. The Navy was interested only in the T40,[citation needed] but the complexities of the driveshaft arrangement doomed the engine and the project was eventually cancelled. Allison tried again with the T56, basically an enlarged T38 with the power of the T40, and was eventually rewarded when this engine was selected to power the C-130 Hercules.
Over the years a family of engines, based on the T56 basic configuration has been developed, culminating in the T406/Allison AE1107 turboshaft for the V-22 Osprey, the Allison AE2100 turboprop, used on newer models of the C-130 and the Allison/Rolls-Royce AE 3007 turbofan which propels many commuter aircraft, such as the Embraer ERJ 135 family.
One of Allison's most successful projects is the Model 250 turboshaft/turboprop engine family, which was started by the company in the early 60s, when helicopters started to be powered by turbine, rather than reciprocating, engines.
Experiments
In the mid-1970s the Allison Division of General Motors Corporation in Detroit designed ceramic components into the Allison GT 404-4 truck engine. Allison continued to work with General Motors on development of ceramic-turbine powered engines until the early 1990s. During their work they were able to engineer fairly stable automobile engines that were capable of burning a variety of fuels including (but not limited to) gasoline, diesel, kerosene, alcohol, vegetable oil, and coal powder.
In the 1980s Allison collaborated with Pratt & Whitney on demonstrating the 578-DX propfan. Unlike the competing General Electric GE-36 UDF, the 578-DX was fairly conventional, having a reduction gearbox between the LP turbine and the propfan blades. Noise considerations, plus a significant reduction in the real cost of aviation fuel, brought the NASA funded program to a halt.
In 1995, Allison tested a prototype lift fan.[2] LiftFan nozzle was tested in 1997 at NASA's Lewis facility.[3]
Acquisition by Rolls-Royce
In 1992 GM tried to sell Allison to concentrate on repairing automobile market share.[4] Rolls-Royce attempted to buy the company in 1993, but GM opted for a management buyout instead for $370 million.
In 1995 authorities approved, with restrictions, that Rolls-Royce bought Allison.[5] for $525 million.[6]
Produkte
- Allison V-1710
- Allison V-3420
- Allison J33
- Allison J35
- Allison J71
- Allison J102
- Allison TF41
- Allison AE 3007
- Allison 250/T63
- Allison AE 2100
- Allison T38
- Allison T40
- Allison T56
- Allison T406
- Allison T701
- Pratt & Whitney/Allison 578-DX
- Allison KF-501
References
- Notes
- ^ John Leonard's articles in various issues of the Allison Branch newsletters
- ^ -as Allison begins JSF lift-fan tests Flight International, 21 May 1997. Retrieved: 19 September 2010.
- ^ Lam, David W. Lift Fan nozzle for JSF tested in NASA Lewis' Powered Lift Rig NASA, 15 April 1998. Retrieved: 18 September 2010.
- ^ Allison Gas Turbine Division - company history Funding Universe. Retrieved: 18 September 2010.
- ^ DoD is satisfied that deal between Allison Engine Co. and Rolls Royce does not endanger national security
- ^ Lazonick, William & Prencipe, Andrea. Sustaining the Innovation Process: The Case of Rolls-Royce plc page 18. Retrieved: 18 September 2010.
- Bibliography
- Whitney, Daniel. Vee's for Victory!: The Story of the Allison V-1710 Aircraft Engine 1929-1948. Atglen, Pennsylvania: Schiffer Publishing Ltd., 1998. ISBN 0-7643-0561-1.