FIELD: aircraft industry; turbojet engines; thrust reversers.
SUBSTANCE: proposed thrust reverser for turbojet engine has two flaps made for travel between open and closed positions of thrust reverser, each flap being controlled by electronic control unit 18a, 18b connected with computing fully reliable control device 20 and two locks 36a, 36b providing locking of flap to which it is connected. Each lock is made for operation by commands from two electronic control units 18a, 18b sent simultaneously.
EFFECT: improved safety owing to synchronization of control of primary locks.
5 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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| ELECTRICAL CONTROL SYSTEM FOR TURBOJET ENGINE THRUST REVERSER | 1997 |
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| HAND-HELD MACHINE | 2008 |
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| TECHNOLOGICAL MACHINE | 2012 |
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