PROPULSION UNIT FOR AN AIRCRAFT
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United States of America Patent
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Nov 12, 2015
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May 14, 2013
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An aircraft propulsion assembly including a turbojet nacelle, and the nacelle includes a stationary structure and a movable structure. The movable structure includes: a thrust reversal device including a cowl translatable along a substantially longitudinal axis of the nacelle between a retracted position, and a deployed position; and a secondary air flow exhaust nozzle including a device for electrically controlling and actuating the nozzle. In particular, the device for controlling and actuating the nozzle includes an electrical switch suitable for being closed during a direct jet operation of the nacelle and moreover suitable for being open during a reverse jet operation. The electrical switch includes a stationary connector and a movable connector.
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