发明名称 System for opening and closing the door of an aircraft landing gear compartment
摘要 A system for opening and closing a door for a landing gear compartment of an aircraft includes a connection between the landing gear and the door with a first system forming an actuator mounted on the landing gear and a second system forming an actuator mounted on the door. The two systems form actuators connected to each other by at least one fluid communication device such that actuating the first system causes the actuation of the second system.
申请公布号 US8888040(B2) 申请公布日期 2014.11.18
申请号 US200913002158 申请日期 2009.07.06
申请人 Airbus Operations SAS 发明人 Gleyse Gilbert
分类号 B64C25/10;B64C25/16;B64C25/22 主分类号 B64C25/10
代理机构 Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P. 代理人 Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
主权项 1. A system for opening and closing a door of a compartment for a landing gear of an aircraft, said system comprising: a connection mechanism between the landing gear and the door configured to ensure opening of the door when the landing gear comes out of said compartment and closing of the door when the landing gear goes back in said compartment, wherein the connection mechanism includes a first actuator mounted on the landing gear and a second actuator mounted on the door, the two actuators being connected to each other by at least one fluid communication device such that movement of the landing gear actuates the first actuator which causes fluid from the first actuator to actuate the second actuator, and wherein the first actuator, the second actuator and the fluid communication device together form at least one closed fluid circuit.
地址 Toulouse FR