Aircraft nacelle incorporating a hood closure device that is independent of the locking mechanism
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United States of America Patent
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Nov 25, 2014
Issued Date -
N/A
app pub date -
Dec 8, 2010
filing date -
Dec 9, 2009
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aircraft nacelle includes, on its outside surface, at least one opening that is blocked by at least one movable part (16) that is kept in closed position by at least one locking mechanism that connects the movable part (16) to another part of the nacelle (16′), characterized in that it includes an anchoring point (32) on one of the two parts (16′) that are to be connected, and a detachable link (34) that is connected to a traction element (36) that is integral with the other part (16) that is to be connected.
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