Pivoting door thrust reverser for a turbofan gas turbine engine
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United States of America Patent
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May 8, 2012
Grant Date -
May 21, 2009
app pub date -
Nov 16, 2007
filing date -
Nov 16, 2007
priority date (Note) -
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status (Latency Note)
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Abstract
A pivot arrangement for a thrust reverser door of a gas turbine engine, the pivot fitting having a base and a shaft projecting from a main side of the base. The shaft receives a preferably curved pivot arm of the door to provide a low profile arrangement which improves performance when the doors are stowed.
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