Power plant for propeller aircraft

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/26 (2006.01) B64C 27/28 (2006.01) B64C 29/00 (2006.01) B64D 27/02 (2006.01) B64D 35/00 (2006.01)

Patent

CA 2314570

A power plant for propeller aircraft has two propulsion devices, each having a propeller, an engine for powering the propeller, and a gear transmission interposed between the engine and the propeller. The transmission has a power input shaft connected directly to the engine, and a power output shaft supporting the propeller and rotated with respect to the input shaft about a hinge axis perpendicular to the output shaft. The gear transmission also has a single gear fitted to the output shaft and having two opposed sets of teeth meshing with a pair of pinions. One of the pinions extends coaxially with the hinge axis, and is connected to the input shaft by a single pair of gears.

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