Suspending loads from a helicopter
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United States of America Patent
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-
May 23, 1995
Grant Date -
N/A
app pub date -
May 14, 1993
filing date -
May 15, 1992
priority date (Note) -
In Force
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Abstract
An arrangement and method for suspending a load from a rotary winged aircraft such as a helicopter by two releasable connections, wherein the load is adapted to be detached from the rotary winged aircraft upon both connections being released. Further safety features are also claimed.
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