发明名称 APPARATUS AND METHOD FOR CONTROLLING LANDING GEAR
摘要 A landing gear system includes landing gear (22), an uplock (26) that is releasably engageable with the landing gear (22), an uplock hydraulic actuator (16) operably connected to the uplock (26), a landing gear hydraulic actuator (14) operatively connected to the landing gear, and a controller (C) operatively connected to the uplock hydraulic actuator (16) and the landing gear hydraulic actuator. In response to receipt of a command to deploy the landing gear, the controller (C) actuates the uplock hydraulic actuator (16) and the landing gear hydraulic actuator (14) to the UP condition and then actuates the uplock hydraulic actuator (16) and the landing gear actuator (14) to the DOWN condition. An alternative embodiment incorporates a piloted check valve (42) upstream of the landing gear hydraulic actuator. The piloted check valve (42) delays operation of the landing gear hydraulic actuator (14) until release of the landing gear (22) by the uplock (26).
申请公布号 CA2914570(A1) 申请公布日期 2014.12.18
申请号 CA20142914570 申请日期 2014.06.12
申请人 BOMBARDIER INC.;LEARJET INC. 发明人 RIBAS, CLOVIS S.;BOUCHER, FREDERIC
分类号 B64C25/22;B64C25/26;F15B15/00 主分类号 B64C25/22
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