Lock for a translating sleeve of a nacelle
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United States of America Patent
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Aug 18, 2015
Grant Date -
May 1, 2014
app pub date -
Oct 31, 2012
filing date -
Oct 31, 2012
priority date (Note) -
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status (Latency Note)
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Abstract
A locking system for a cascade thrust reverser on a bypass turbofan is disclosed. The locking system includes a translating sleeve configured to move between a stowed position and a deployed position. A lock member is mounted to a beam and has a locking portion which contacts a roller on the translating sleeve to retract the locking portion when the translating sleeve moves to the stowed position.
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