Spin actuated release mechanism
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorsStanley J. Herold, Donald E. Lagrange, John E. Laswell
Life of this patent
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Abstract
A release mechanism for use with an air-dropped store having a timed firing echanism which can be set for different time intervals. Action is initiated by a plurality of dynamic pressure sensing fins which, upon actuation, first unlock an inertia locking arm and then the fins impart a rotation to the store which rotation, in turn, causes the locking arm to pivot and initiate a timer. The timer, in turn, initiates separation of the release mechanism from the store.
Claims4
A release mechanism for use with an aircraft parachute flare comprising,
- a housing,
- a plurality of arms for removably attaching said housing to an aircraft parachute flare,
- means for actuating said arms for uncoupling said housing from said aircraft parachute flare,
- an ertia arm pivotally mounted in said housing for locking said means for actuating said arms,
- a pin attached to said inertia arm,
- an actuator slidably mounted to said housing and engageable with said pin attached to said inertia arm,
- spring means for disengaging said actuator from said pin attached to said inertia arm,
- a plurality of shafts slidably positioned in said housing engageable with said actuator for holding said actuator in a locking position with said pin attached to said inertia arm, and
- means for disengaging said plurality of shafts from said actuator and pivoting said inertia arm whereby said means for actuating said arms is unlocked.
Dependencies are inferred from the claim text.