FIELD: turbojet engines.
SUBSTANCE: proposed turbojet engine thrust reverser contains two doors 10a, 10b made for displacement between positions corresponding to open and closed positions of reverser by means of at least one control power cylinder 12, two electric 14a, 14b, each being coupled with at least on control power cylinder of each door. Each electric motor is controlled by electronic control unit 18a, 18b connected with fully-responsible electronic control computer 20. Two means for automatic control of each door travel by position setting orders are provided. Said automatic control means provide synchronous displacement of doors with due account of possible changes of forces acting onto thrust reverser and possible difference in force acting on each door.
EFFECT: improved reliability and safety of thrust reverser.
10 cl, 2 dwg
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|---|---|---|---|
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