Releasable locking mechanisms

Joints and connections – Structurally installed in diverse art device

Reexamination Certificate

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Details

C403S002000, C403S021000, C411S433000

Reexamination Certificate

active

06939073

ABSTRACT:
In the aerospace field spacecraft components are held together by separation systems until a specific time when they must be separated or deployed. Customarily a threaded joining bolt engages one of the components to be joined, and a threaded nut is placed on that bolt against the other component so they can be drawn together by a releasable locking assembly. The releasable locking assembly herein includes a plunger having one end coupled to one end of a plunger bolt. The other end is flanged to abut and compress a coil spring when the plunger is advanced toward the interface plane between the two components. When the plunger is so advanced toward the interface plane, the end of the plunger bolt can be connected to the joining bolt. Thus during retraction the joining bolt is drawn to one side of the interface plane by the force of the expanding spring.

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Johnston, A.S., Ahmed, R., Garrison, J.C., Gaines, J.L., Waggoner, J.D., “X-38 Bolt Retrctor Subsystems Separation Demonstration,” NASA Technical Memorandum 2002-212047, NASA Center for AeroSpace Information (MSFC, Alabama), (Sep. 3, 2002).

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