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Allison V-3420

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Image:Allison V-3420 Engine.jpg
Allison V-3420 Engine

The Allison V-3420 was a large experimental American piston aircraft engine, designed in 1937.

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[edit] History

In 1937, at the behest of the United States Army Air Corps, the Allison Engine Company agreed to design and build a large-displacement high power aircraft engine. The resulting V-3420 was essentially a pair of 12 cylinder Allison V-1710 engines mated to a common crankcase with a 30° angle between the inner cylinder banks. The crankshafts of the two V-1710 engines were geared together to drive a common propeller shaft. Most V-3420 parts were interchangeable with those for V-1710-E and -F engines.

The V-3420 had a power-to-weight ratio of 1.6 kW/kg or 1 hp/lb, excellent for its time. It was envisioned as a powerful yet compact engine for several advanced Air Force projects of the day, including the Douglas XB-19, the Boeing XB-39 Superfortress, the Lockheed XP-58 Chain Lightning, and the General Motors P-75 Eagle. None of these designs reached full-scale production, and only about 150 V-3420s were built.

[edit] Specifications (V-3420)

Template:Pistonspecs

[edit] References

[edit] Related contents

pl:Allison V-3420


This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "Allison V-3420".
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