SYSTEM AND METHOD FOR SECURING BATTERY IN AIRCRAFT
Number of patents in Portfolio can not be more than 2000
United States of America
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Issued Date -
Mar 3, 2022
app pub date -
Sep 1, 2020
filing date -
Sep 1, 2020
priority date (Note) -
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status (Latency Note)
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Abstract
A system for rapid securement and disengagement of a battery assembly-type power source element is provided herein. The system can include a battery assembly that includes a battery element having opposite, opposing surfaces and configured to provide power to at least a portion of a vehicle. On the surface of the battery assembly a pin element can be disposed. The system also includes a receiver assembly configured to mechanically couple the battery assembly. The receiver assembly can include an insertion opening having a size configured to receive the battery assembly and a hook assembly. The hook assembly can include a hook configured to mechanically couple to the pin element of the battery assembly and shaft configured to drive the hook such that a distance between the insertion opening and the battery assembly is changed.
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