发明名称 Constant-Velocity Joint with Torque-Combining Differential
摘要 A constant-velocity drive system for an aircraft rotor has a gimbal mechanism and a differential torque-combining mechanism. The gimbal mechanism has gimbals driven in rotation by a rotor mast about a mast axis, the gimbals providing for gimballing relative to the mast about gimbal axes generally perpendicular to the mast axis. The differential torque-combining mechanism is connected to the gimbal mechanism and configured to be driven in rotation about the mast axis by the gimbal mechanism. The differential mechanism is capable of gimballing relative to the mast about the gimbal axes, the differential torque-combining mechanism having an output component attached to a yoke of the rotor for driving the yoke in rotation with the differential torque-combining mechanism.
申请公布号 US2011315816(A1) 申请公布日期 2011.12.29
申请号 US201113227917 申请日期 2011.09.08
申请人 STAMPS FRANK B.;TISDALE PATRICK R.;BELL HELICOPTER TEXTRON INC. 发明人 STAMPS FRANK B.;TISDALE PATRICK R.
分类号 B64D35/00;B64C27/12 主分类号 B64D35/00
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