发明名称 |
AIRCRAFT LANDING GEAR |
摘要 |
In some embodiments, an aircraft may include a retractable or extendable landing gear. The landing gear may include a wheel connected to an axle, a strut configured to resist longitudinal compression, and a linear actuator that is partially disposed within an opening of the strut. |
申请公布号 |
US2016207611(A1) |
申请公布日期 |
2016.07.21 |
申请号 |
US201514599705 |
申请日期 |
2015.01.19 |
申请人 |
Bell Helicopter Textron Inc. |
发明人 |
Fenny Carlos A.;Ross Brent C.;Kell Kevin;Baines Andrew |
分类号 |
B64C25/20 |
主分类号 |
B64C25/20 |
代理机构 |
|
代理人 |
|
主权项 |
1. A landing gear for an aircraft, the landing gear comprising:
a wheel in mechanical communication with an axle forming a wheel assembly; a strut coupled to the wheel assembly and configured to resist longitudinal compression along a first axis, the strut comprising:
a piston having an opening therein; anda housing associated with the piston; and a linear actuator comprising:
an elongated shaft at least partially disposed within the opening of the piston; anda motor operable to reposition the strut by moving the elongated shaft. |
地址 |
Fort Worth TX US |