Electric control system for a turbojet engine thrust reverser in

Details Electric control system for a turbojet engine thrust reverser in Electric control system for a turbojet engine thrust reverser in

1997-11-12

1999-10-05

Kim, Ted

Power plants

Reaction motor

Interrelated reaction motors

60230, 244110B, F02K 302, F02K 176

Patent

active

059606266

ABSTRACT:
An electric control system is disclosed for a turbojet engine thrust reverser having at least one movable component movable between a forward thrust position and a reverse thrust position, the control system having at least one electromechanical drive device mechanically connected to the moveable component such that actuation of the electromechanical drive device moves the component between the forward and reverse thrust positions, and an electronic control unit electrically connected to the electromechanical drive device and to a turbojet engine control system to transmit actuation signals to the electromechanical drive device to control the movement of the component between the forward and reverse thrust positions. The electronic control system preferably also has at least one electrically actuated locking device to hold the movable component in the forward thrust position.

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patent: 4437783 (1984-03-01), Halin et al.
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patent: 4754694 (1988-07-01), Martin
patent: 5404714 (1995-04-01), Davies
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patent: 5547130 (1996-08-01), Davies
patent: 5819527 (1998-10-01), Fournier
patent: 5826823 (1998-10-01), Lymons et al.

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