Universal vtol power and rotor system module

Details Universal vtol power and rotor system module Universal vtol power and rotor system module

B - Operations, Transporting

64

C

B64C 27/14 (2006.01) B64C 27/08 (2006.01) B64C 27/82 (2006.01) B64C 39/02 (2006.01)

Patent

CA 2301350

A universal power drive and lifting rotor system module for single and multiple rotor type VTOL aircraft having a component support airframe module hawing a plurality of quick disconnect fasteners for detachably connecting components thereto. A train drive shaft is supported for rotation within the component support airframe and is adapted for detachable connection to an engine. A lifting rotor assembly and transmission are mounted on the component support airframe using quick disconnect fasteners. The rotor transmission has a power input shaft adapted for detachable connection to the main drive shaft for transferring power between the main drive shaft and the power input shaft.

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