发明名称 Control device for a turbojet engine thrust reverser, blocking the reverser
摘要 A control device for a thrust reverser of a turbojet engine nacelle, which includes movable portions actuated by actuators, includes: a first blocking control acting on a motor-actuated system; and a second blocking control acting, mechanically, on the movable portions. The second blocking control may inhibit, when activated, a deployment of the movable portions. The control device further includes a device inhibiting disengagement of the first blocking control when a mechanical control is activated.
申请公布号 US9593644(B2) 申请公布日期 2017.03.14
申请号 US201514975326 申请日期 2015.12.18
申请人 AIRCELLE 发明人 Joret Jean-Philippe;Soulier Pascal;Taddei Vincent
分类号 F02K1/76;F02K1/72;F02K1/62 主分类号 F02K1/76
代理机构 Burris Law, PLLC 代理人 Burris Law, PLLC
主权项 1. A control device for a thrust reverser of a turbojet engine nacelle comprising movable portions actuated by actuators, which movable portions deploy so as to reverse a thrust, the control device comprising: a first blocking control acting on a motor-actuated system, the first blocking control comprising an operating lever; and a second blocking control acting, mechanically, on the movable portions, the second blocking control configured to inhibit, when activated, a deployment of the movable portions, wherein the control device comprises a member which directly blocks displacement of the operating lever of the first blocking control when the second blocking control is activated, thereby blocking deployment of the thrust reverser of the turbojet engine nacelle.
地址 Gonfreville l'Orcher FR