Aeronautics and astronautics – Spacecraft – With deployable appendage
Reexamination Certificate
2007-06-27
2010-12-14
Ellis, Christopher P (Department: 3644)
Aeronautics and astronautics
Spacecraft
With deployable appendage
C244S158100, C074S470000
Reexamination Certificate
active
07850124
ABSTRACT:
A rotary positioning device of a movable element for space equipment comprising a part attached to a fixed portion of the equipment and a handle actuating the movable portion of the equipment, said handle being rigidly connected to a first race of a ball or roller antifriction bearing and said fixed part being connected to the second race of said antifriction bearing, wherein a link between said fixed part and the second race is an elastic link in rotation about the axis of said antifriction bearing and wherein a stop is rigidly attached to one of the races in order to interact with an element rigidly attached to the other race, so that the relative rotation of the two races of said antifriction bearing is limited angularly.
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Baudasse Yannick
Brossier Jérôme
Ellis Christopher P
Lowe Hauptman & Ham & Berner, LLP
Thales
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