Released control release mechanism in particular for use in...

Details Released control release mechanism in particular for use in... Released control release mechanism in particular for use in...

2006-05-02

2006-05-02

Lazo, Thomas E. (Department: 3745)

Expansible chamber devices

Plural unitarily mounted cylinders or frame therefor

Coaxial cylinders

C244S137400

Reexamination Certificate

active

07036423

ABSTRACT:
The invention concerns a device forming a mechanism, in particular for use in the space industry, characterised in that it comprises in combination: two structural elements (100, 200) capable of relative displacement, locking means (300) adapted to prevent initially the relative displacement between the two structural elements (100, 200), and means (400) for controlled locking of the locking means (300) designed to prevent initially the release thereof, then when activated, successively, in a first phase, a sliding action in controlled amplitude of the locking means (300), for limited release between the two structural elements (100, 200), then in a second phase, complete release of the locking means (300) and hence of the structural elements (100, 200).

REFERENCES:
patent: 3186163 (1965-06-01), Dixon
patent: 3242666 (1966-03-01), Peterson
patent: 4158322 (1979-06-01), Hardesty
patent: 4263839 (1981-04-01), Akkerman et al.
patent: 4682804 (1987-07-01), Palmer et al.
patent: 5395149 (1995-03-01), Herman et al.
patent: 0657326 (1995-06-01), None
patent: 1558534 (1969-02-01), None
patent: WO8607427 (1986-12-01), None

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