| 发明名称 |
SHOCK ABSORBER ASSEMBLY FOR POWER DRIVE UNIT OF A VEHICLE |
| 摘要 |
A shock absorber assembly is configured to be operatively connected to a drive shaft of a power drive unit (PDU) of an aircraft. The shock absorber assembly may include a first hub, a second hub, and a bull gear having at least a portion sandwiched between the first and second hubs. The bull gear is configured to rotate independently of the first and second hubs a controlled distance in response to a mechanical malfunction of the PDU. |
| 申请公布号 |
US2016244151(A1) |
申请公布日期 |
2016.08.25 |
| 申请号 |
US201514630226 |
申请日期 |
2015.02.24 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
Jones Kelly Thomas |
| 分类号 |
B64C13/00;B64C3/48;B64C9/02;F16F15/129;F16F15/123 |
主分类号 |
B64C13/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A shock absorber assembly configured to be operatively connected to a drive shaft of a power drive unit (PDU) of an aircraft, the shock absorber assembly comprising:
a first hub; a second hub; and a bull gear having at least a portion sandwiched between the first and second hubs, wherein the bull gear is configured to rotate independently of the first and second hubs a controlled distance in response to a mechanical malfunction of the PDU. |
| 地址 |
Chicago IL US |
