Displacement mechanism

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

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Details

91 61, 91530, 92 2, 244 49, 244 52, 244 78, F42B 1332

Patent

active

043986820

ABSTRACT:
A displacement mechanism for effecting both rotary movement of a movable member (for example a fin) with respect to a fixed member (for example a flight vehicle body) from a first, inoperative position to a second, operative position about a longitudinal axis and axial movement of the movable member along that axis to effect subsequent locking in the second position, comprises a fluid operated vane motor to effect rotation and a fluid operated piston/cylinder arrangement to effect the axial movement. Preferably the vane motor and the piston/cylinder arrangement are closely integrated one with another.

REFERENCES:
patent: 1982656 (1934-12-01), Gilman
patent: 2459902 (1949-01-01), Tucker
patent: 3563495 (1971-02-01), Korn
patent: 3620132 (1971-11-01), Nitkiewicz
patent: 3695556 (1972-10-01), Gauzza
patent: 3766831 (1973-10-01), Yeakley
patent: 4005641 (1977-02-01), Nussbaumer
patent: 4138206 (1979-02-01), Zenevich et al.

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