Detachable connecting arrangement for fitting launchable external loads to an aircraft
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United States of America Patent
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Aug 8, 2017
Grant Date -
Jan 9, 2014
app pub date -
Jul 15, 2011
filing date -
Jul 21, 2010
priority date (Note) -
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Abstract
A detachable connecting arrangement for fitting launchable external loads to an aircraft, having a hook-like connecting element fitted to the external load and a holding element fitted to the aircraft for the hook-like connecting element. The hook-like connecting element includes a lower supporting surface and an upper supporting surface. The holding element has a first opposing supporting surface that interacts with the lower supporting surface, and a second, upper opposing supporting surface that interacts with the upper supporting surface. The lower supporting surface and the first opposing supporting surface are designed to support mass forces of the external load directed away from the aircraft, and the upper supporting surface and the upper opposing supporting surface are designed to support mass forces of the external load directed towards the aircraft.
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