Control device for a turbojet engine thrust reverser, blocking the reverser
AssigneeAircelle
InventorsJean-Philippe JORET, Pascal SOULIER, Vincent TADDEI
Life of this patent
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Abstract
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.
Claims10
A control device for a thrust reverser of a turbojet engine nacelle comprising movable portions actuated by actuators, which deploy so as to reverse a thrust, the control device comprising:
- 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 configured to inhibit, when activated, a deployment of the movable portions,
- wherein the control device comprises a means which inhibits a disengagement of the first blocking control when a mechanical control is activated.
Dependencies are inferred from the claim text.