| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide a sealing method corresponding to the improved condensation problem of an electromechanical actuator system used for an aircraft landing gear. <P>SOLUTION: An actuator system 100 includes a housing 130. The housing 130 includes a cavity defined by the housing and an opening defined in a wall of the housing. The housing encases an actuator within the cavity. The actuator system 100 also includes a cap 120 coupled to the housing to facilitate shielding the opening from a surrounding environment. <P>COPYRIGHT: (C)2010,JPO&INPIT</p> |
