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Toggle releaseThe invention relates to a pyrotechnic actuated release mechanism which is mechanically two fault tolerant for effecting release. It is particularly well suited for releasably connecting structures to be used in the space environment or in other aerospace applications. The device comprises a fastener plate and fastener body, each attachable to either one of a pair of structures to be joined. The fastener plate and the body are fastenable by a toggle supported at one end on the fastener plate and mounted for universal pivotal movement thereon. At its other end, which is received in a central opening in the fastener body and adapted for limited pivotal movement therein, the toggle is restrained by three retractable latching pins. Each pin is individually retractable by combustion of a pyrotechnic charge. While retraction of all three pins releases the toggle, the fastener is mechanically two fault tolerant since the failure of any single or pair of the latch pins to retract results in an asymmetrical loading on the toggle and its pivotal movement to effect a release. An annular bolt is mounted on the fastener plate as a support for the socket mounting of the toggle whereby its selective axial movement provides a means for pre-loading the toggle.
Document ID
19880015585
Acquisition Source
Legacy CDMS
Document Type
Other - Patent Application
Authors
Graves, Thomas Joseph
(NASA Lyndon B. Johnson Space Center Houston, TX., United States)
Yang, Robert Alexander
(NASA Lyndon B. Johnson Space Center Houston, TX., United States)
Brown, Christopher William
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
September 5, 2013
Publication Date
February 11, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.71:MSC-21354-1
Accession Number
88N24969
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MSC-21354-1
Patent Application
US-PATENT-APPL-SN-154712
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