发明名称 Torque compensation for propeller pitch change mechanism
摘要 A propeller assembly has a plurality of propeller blades, and a pitch change mechanism including at least one motor. A drive input drives the plurality of propeller blades to rotate about a central drive axis. The pitch change mechanism is operable upon driving of the motor to move the propeller blades relative to the drive input. The drive input includes a drive input gear transmission to change a pitch angle of the blades when the blades are moved relative to the drive input by the pitch change mechanism. Further, a method of operating a propeller assembly to change a pitch angle is disclosed and claimed.
申请公布号 US8496436(B2) 申请公布日期 2013.07.30
申请号 US20100685034 申请日期 2010.01.11
申请人 PERKINSON ROBERT H.;HAMILTON SUNDSTRAND CORPORATION 发明人 PERKINSON ROBERT H.
分类号 B64C11/34 主分类号 B64C11/34
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