Wing lock and disconnect mechanisms for a RC aircraft
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United States of America Patent
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May 26, 2020
Grant Date -
Mar 1, 2018
app pub date -
Aug 31, 2017
filing date -
Sep 1, 2016
priority date (Note) -
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status (Latency Note)
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Abstract
A radio-controlled (RC) aircraft has a wing lock and disconnect mechanism. The RC aircraft has a structural member and a wing that disconnects from a fuselage. The RC aircraft has a lock mechanism, a wing structural member recess, a fuselage structural member recess, a lock recess, and an aperture. The lock mechanism couples to the wing and is adapted to fit within the lock recess of the fuselage. The wing structural member receives the structural member. The fuselage structural members recess corresponds to the wing structural member recess. The lock recess receives the lock mechanism. The wing disconnects from the fuselage by unlocking the lock mechanism. The structural member fits within the wing structural member recess and the fuselage structural member recess.
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