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