Apparatus for deploying wing of guided missile

Details Apparatus for deploying wing of guided missile Apparatus for deploying wing of guided missile

2006-05-26

2009-12-08

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Missile stabilization or trajectory control

Externally mounted stabilizing appendage

Reexamination Certificate

active

07628354

ABSTRACT:
An apparatus for deploying a wing of a guided missile comprises a fixed wing fixedly coupled to a body of a guided missile, a rotary wing rotatably coupled to the fixed wing, and a deploying portion for rotating the rotary wing into an unfolded state from a folded state by providing a torsion force to the rotary wing. In the apparatus, a folded degree of the rotary wing can be maximized.

REFERENCES:
patent: 2867841 (1959-01-01), Baldauf
patent: 3273500 (1966-09-01), Kongelbeck
patent: 4460137 (1984-07-01), Andersson et al.
patent: 5820072 (1998-10-01), Na et al.
patent: 6092264 (2000-07-01), Banks
patent: 2007/0045466 (2007-03-01), Hellis

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