Lost-fluid hydraulic actuation system

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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Details

89 1811, 60415, F41F 3055

Patent

active

047579609

ABSTRACT:
Lost-fluid hydraulic actuation system.
This system makes it possible to control for a short time an element (168) in an autonomous working unit, particularly a rocket, with an onboard means (100) connected to the unit. Hydraulic fluid under pressure is introduced into the element (168) by a delivery pipe (141). A tank (130) supplies the hydraulic fluid used during the autonomous working, a helium bottle (110) puts the hydraulic fluid under pressure, and an evacuation pipe (171) evacuates the hydraulic fluid out of the autonomous unit after it has actuated the element (168).

REFERENCES:
patent: 2170890 (1939-08-01), Allen
patent: 2278181 (1942-03-01), Lieberherr
patent: 2290479 (1942-07-01), Mercier
patent: 2866385 (1958-12-01), Miller
patent: 3049877 (1962-08-01), Sherman
patent: 3163985 (1965-01-01), Bouyoucos
patent: 3443475 (1969-05-01), Berton
patent: 3692258 (1972-09-01), Parilla
patent: 3908933 (1975-09-01), Goss et al.
patent: 3911678 (1975-10-01), Shafer et al.

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