A hidden latch system for an interior structure of an aircraft is disclosed. The hidden latch system includes at least two engagement features coupled to an interior structure of an aircraft. Each of the at least two engagement features includes an engagement portion, an engagement rod, and a self-centering feature. The engagement portion is configured to engage and release the engagement rod, and the self-centering feature is configured to self-center the engagement rod in at least one direction. Further, the engagement portion is configured to release the engagement rod using a cable pull system.
Remotely-Activated Self-Centering Cable Latch
2017-03-02
Patent
Electronic Resource
English
NTRS | 1980
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