Pivot bearing arrangement for the control surface of a missile

Details Pivot bearing arrangement for the control surface of a missile Pivot bearing arrangement for the control surface of a missile

1985-10-29

1987-04-28

Kyle, Deborah L.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244 329, 277 27, F42B 1332, F42B 15053, F42B 15027, F16J 1516

Patent

active

046607862

ABSTRACT:
A pivot or bearing arrangement for the pivotable control surface of a guidable missile, especially a projectile which can be fired through the intermediary of the gas pressure generated by a propellant charge. The pivot bearing includes a control surface support guided by a radial ball bearing, including a circular shoulder which axially contacts against a sealing ring which lies on a shoulder of the supportive tail end structure of the projectile and which is constituted of a resiliently deformable or compressible material.

REFERENCES:
patent: 3024027 (1962-03-01), Kubiak
patent: 3037826 (1962-06-01), Zeller
patent: 3135203 (1964-06-01), Halsted et al.
patent: 3650496 (1972-03-01), Svensson
patent: 3743333 (1973-07-01), Kosinski
patent: 3843075 (1974-10-01), Webster et al.

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