TWIN-DOOR THRUST REVERSER
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United States of America Patent
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app pub date -
Jul 11, 2014
filing date -
Jan 17, 2012
priority date (Note) -
Abandoned
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Abstract
A thrust reverser for aircraft turbojet engine nacelle includes at least one upstream door and a downstream door. The upstream and downstream doors move in concert between a direct jet position and a reverse jet position. In the direct jet position, two doors are closed, and in the reverse jet position the two doors are open and able to deflect a part of a cold air flow circulating inside the nacelle. The thrust reverser further includes a curved downstream edge of the upstream door to make adapted a part of cold air flow circulating between an upper camber of the upstream door and a lower camber of the downstream door.
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