发明名称 Constant velocity joint with control mechanism
摘要 According to one embodiment, a constant velocity (CV) joint includes a first yoke, a second yoke, and a control mechanism. The first yoke is configured to be rotatably coupled to an input device about a first axis and configured to receive the input device through a first opening. The second yoke is rotatably coupled to the first yoke about a second axis and rotatably coupled to an output device about a third axis. The control mechanism is adapted to constrain the first yoke and the second yoke so as to achieve a substantially CV characteristic between the input device and the output device.
申请公布号 US9399513(B2) 申请公布日期 2016.07.26
申请号 US201213673475 申请日期 2012.11.09
申请人 Bell Helicopter Textron Inc. 发明人 Sutton Drew A.;Foskey Christopher;Smith Dudley;Stamps Frank B.
分类号 B64C27/37;F16D3/30;B64C27/41;F16D3/33;B64C27/32 主分类号 B64C27/37
代理机构 Bell Helicopter Textron Inc 代理人 Bell Helicopter Textron Inc
主权项 1. A rotorcraft, comprising: a body; a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source; a hub; a rotor blade coupled to the hub; and a constant velocity (CV) joint coupled between the drive shaft and the hub, the CV joint comprising: a first yoke rotatably coupled to the drive shaft about a first axis and configured to receive the drive shaft through a first opening;a second yoke rotatably coupled to the first yoke about a second axis and rotatably coupled to the hub about a third axis; anda control mechanism adapted to constrain the first yoke and the second yoke so as to achieve a substantially CV characteristic between the drive shaft and the hub, the control mechanism comprising a positioning portion adapted to position the first and second yokes such that the second axis substantially resides on a bisector of an angle between the drive shaft and the hub.
地址 Fort Worth TX US