Aircraft latch Assembly with Lock Sensor(s)
Number of patents in Portfolio can not be more than 2000
United States of America
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N/A
Issued Date -
Jan 16, 2025
app pub date -
Jan 2, 2024
filing date -
Jan 2, 2024
priority date (Note) -
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status (Latency Note)
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Abstract
An assembly is provided for an aircraft. This assembly includes a keeper, a latch, a lock and an electric sensor. The latch includes a handle and a hook structure operatively coupled to the handle. The hook structure is engaged with the keeper when the handle is in a closed position. The hook structure is disengaged from the keeper when the handle is in an open position. The lock includes a lock element configured to move between a locked position and an unlocked position. The lock is configured to lock the handle in the closed position when the lock element is in the locked position. The lock is configured to unlock the handle from the closed position when the lock element is in the unlocked position. The electronic sensor is configured to provide a signal when the lock element is in one of the locked position or the unlocked position.
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