System for controlling the cowl of a turbojet engine nacelle thrust reverser
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United States of America Patent
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Jan 27, 2015
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N/A
app pub date -
Nov 21, 2008
filing date -
Feb 13, 2008
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Abstract
A nacelle for a turbojet engine includes an air inlet forward section, a median section surrounding a fan of the turbojet engine, an aft section equipped with a thrust reverser system, a power control unit able to convert a high voltage electric supply into an electric supply towards an electromechanical actuator, and a drive unit for the power control unit which is distinct and separate from the latter and has a control input and a drive output to be connected to the power control unit. The thrust reverser system includes a mobile cowl which, under action of an electromechanical actuator, is able to move from a closed position to an open position in which the mobile cowl opens a passage in the nacelle.
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