Drive system for the retraction/extension of variable diameter rotor systems
AssigneeSikorsky Aircraft Corporation
InventorYuriy Gmirya
Life of this patent
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AssigneeSikorsky Aircraft Corporation
InventorYuriy Gmirya
Estimating the term…
A drive system for a variable diameter rotor (VDR) system includes a plurality of rotor blade assemblies with inner and outer rotor blade segments. The outer blade segment being telescopically mounted to the inner blade segment. The VDR retraction/extension system includes a drive housing mounted at the root of each blade. The housing supports a spool assembly, a harmonic gear set and an electric motor. The spool assembly includes a pair of counter rotating spools each of which drive a respective cable which extends through the interior of the inboard rotor blade section and around a pulley mounted to the outboard rotor blade section. In operation, the electric motor drives the harmonic gear set which rotates the counter rotating spools. Rotation of the spools causes the cables to be wound onto or off their respective spool consequently effecting retraction/extension of the pulley and the attached outboard rotor blade section relative the inboard rotor blade section. As each blade drive system is independently driven by a separate electrical motor, each independent VDR blade assembly is independently positionable.
A retraction/extension system for an rotor blade assembly, said rotor blade assembly having an outboard blade section telescopically mounted to an inboard blade section, said retraction/extension system comprising:
A retraction/extension system for a variable diameter rotor blade system having a rotor hub and a multiple of rotor blade assemblies, each of said rotor blade assemblies having an outboard blade section telescopically mounted to an inboard blade section, said retraction/extension system for each of said multiple of rotor blade assemblies comprising:
Dependencies are inferred from the claim text.