Release mechanism for a forward and aft restrained load in...

Aeronautics and astronautics – Aircraft structure – Passenger or cargo loading or discharging

Reexamination Certificate

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Details

C244S118100

Reexamination Certificate

active

07861972

ABSTRACT:
An object is deployed from an aircraft using gravity extraction of the object with the aid of a small parachute. The object is restrained in the fore and aft directions on either side of the center of gravity by fore and aft loading chains which hold the object to a loading deck. The chains are attached to the object by pear shaped rings mounted to a load plate. The load plate is supported on a lower attachment plate mounted to the object and is attached by a pin to an upper attachment plate also mounted to the object. Pulling the pin causes the load plate to rotate about a hinge formed on the lower attachment plate followed by release of the load plate from the lower attachment plate and the object to be deployed.

REFERENCES:
patent: 3306234 (1967-02-01), Hansen et al.
patent: 4144821 (1979-03-01), Lang

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