Deployable wing mechanism

Details Deployable wing mechanism Deployable wing mechanism

1979-12-11

1982-06-29

Reeves, Robert B.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

B64C 340

Patent

active

043369146

ABSTRACT:
A deployable wing assembly using an inner wing segment and an outer wing segment. The inner wing segment is hinged longitudinally to the body of a missile, or the like, and with the outer wing segment hinged by a pin perpendicular to the surface of the wing segments at the junction, and including deploying and locking arrangements for both sections.

REFERENCES:
patent: 1485163 (1924-02-01), Braun
patent: 2572421 (1951-10-01), Abel
patent: 2924175 (1960-02-01), Jasse
patent: 3165281 (1965-01-01), Gohlke
patent: 3643599 (1972-02-01), Hubich
patent: 3790104 (1974-02-01), Jones
patent: 4022403 (1977-05-01), Chiquet

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