Folding articulating wing mechanism

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

Reexamination Certificate

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Reexamination Certificate

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07732741

ABSTRACT:
A locking mechanism for securing an articulated folding wing assembly in a fully extended position by means of a tapered locking plunger urged by a coiled compression spring to contact a complementary mating surface formed on the wing assembly. The spring urged locking plunger is released from a retracted position by rotation of the wing assembly from the folded position to the extended position. A folding mechanism for rotating the wing assembly through a compound angle from the folded position to a rigid and positively locked fully extended position is provided wherein the extended wing may be rotated about its longitudinal axis to provide directional control to the vehicle.

REFERENCES:
patent: 3125956 (1964-03-01), Kongelbeck
patent: 4106727 (1978-08-01), Ortell
patent: 4351499 (1982-09-01), Maudal
patent: 4586680 (1986-05-01), DiTommaso
patent: 4592525 (1986-06-01), Madderra
patent: 4664339 (1987-05-01), Crossfield
patent: 4667899 (1987-05-01), Wedertz
patent: 4858851 (1989-08-01), Mancini
patent: 4869442 (1989-09-01), Miller
patent: 5240203 (1993-08-01), Myers
patent: 5820072 (1998-10-01), Na et al.
patent: 6260797 (2001-07-01), Palmer
patent: 6905093 (2005-06-01), Dryer et al.

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