Invention Grant
US08356768B2 Multiple drive-path transmission with torque-splitting differential mechanism 有权
具有转矩分离差动机构的多驱动路径传输

Multiple drive-path transmission with torque-splitting differential mechanism
Abstract:
A transmission for a rotary-wing aircraft has a differential torque-splitting mechanism associated with an input shaft. The differential has a drive disk coaxial with the shaft and integral in rotation with the shaft, a first driven member coaxial with the shaft and generally adjacent the drive disk, and a second driven member coaxial with the shaft and generally adjacent the drive disk. At least one pin engages each of the drive disk, the first driven member, and the second driven member. The first driven member is configured to drive a first transfer gear, and the second driven member is configured to drive a second transfer gear for supplying torque to a bull gear associated with a rotor mast.
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