Rotary ball lock latching mechanism
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United States of America Patent
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Jan 29, 2019
Grant Date -
Jan 5, 2017
app pub date -
Jul 2, 2015
filing date -
Jul 2, 2015
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A latching mechanism is provided for engaging an aircraft surface panel to a support member. The aircraft panel is provided with a post extending from the lower surface, which extends through a panel support member into a post engagement mechanism. The post engagement mechanism defines a rotatable sleeve, which rotates for locking and unlocking engagement between the post and the post engagement mechanism. Locking engagement continues when power to the post engagement actuator is terminated. The post engagement mechanism may utilize various types of actuators, including mechanical, hydraulic, and pneumatic. The aircraft panel and the panel support member are translatable into and out of abutting engagement independent of the need for any contact with the aircraft panel upper surface.
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