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 |