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Allison V-1710

Aircraft Engines

The Allison V-1710 was an American liquid-cooled V12 aircraft engine designed and built by the Allison Division of General Motors, and the most common US-developed engine of its type in service in the Second World War. Development began in 1929 to meet an Army Air Corps need for a modern 1,000 horsepower engine, and in 1937 the V-1710-C6 became the first engine of any type to pass the Army 150 hour type test at that rating. Turbocharged versions gave the twin-engined Lockheed P-38 Lightning excellent high-altitude performance. The engine also powered the Bell P-39 and Curtiss P-40, and the early North American P-51 Mustang. Its modular design let one production line serve many propeller and supercharger arrangements.

Facts
Year
1931 2
Cylinder Count
12 1
Classification
Configuration
V-Configuration 1
Connections

Exemplifies

Aviation, Modes
Source Allison V-1710 (Wikipedia)

Of Make

Source List of GM engines (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source List of GM engines (Wikipedia)Aircraft engines, Piston
Quote, Aircraft engines, Piston
1931–1944 Allison V-1710
Sources
1. Allison V-1710 (Wikipedia)
  • Lead
    was an American V12 aircraft engine
  • Technical description
    The V-1710 has 12 cylinders
  • Exemplifies: Aviation, Lead and applications
    was an American V12 aircraft engine
  • Part Of: Lockheed P-38 Lightning, Applications
    powering the Lockheed P-38, Bell P-39 and Curtiss P-40
  • Part Of: Bell P-39 Airacobra, Applications
    powering the Lockheed P-38, Bell P-39 and Curtiss P-40
  • Part Of: North American P-51 Mustang, Applications
    which became the first generation of the famed P-51 Mustang
View the Source
2. List of GM engines (Wikipedia)
Aircraft engines, Piston
Quote, Aircraft engines, Piston
1931-1944 Allison V-1710
View the Source
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