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Variable length strut with longitudinal compliance and locking capabilityA variable length strut device is illustrated for connecting two associated structures which includes an outer load bearing shell, a drive assembly, a length varying compliance assembly positioned by drive assembly, and a strut rod locking assembly. The load bearing shell includes a connecting part adapted for connection to a first associated structure. A strut connection rod has a connecting part adapted for connection to a second associated structure and a distal end having a piston driver slidably carried in a housing of compliance assembly. Two compliance pistons act in opposing directions on the piston driver to provide longitudinal compliance in a compliance mode of operation. Locking assembly includes locking balls which are urged in a locking ring as locking bolt is urged to the left by fluid pressure. Microswitches sense the displacement of pistons away from the internal ring to bring the pistons to a neutral position wherein the pistons are in contact with the internal ring when it is desired to do so as affected by a control source.
Document ID
19850026088
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Belew, R. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
August 20, 1985
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: NASA-CASE-MFS-25907-1
Patent Application Number: US-PATENT-APPL-SN-510137
Patent Number: US-PATENT-4,536,114
Accession Number
85N34401
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MFS-25907-1|US-PATENT-4,536,114
Patent Application
US-PATENT-APPL-SN-510137
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