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Mounting Systems for Structural Members, Fastening Assemblies Thereof, and Vibration Isolation Systems Including the SameMounting systems for structural members, fastening assemblies thereof, and vibration isolation systems including the same are provided. Mounting systems comprise a pair of mounting brackets, each clamped against a fastening assembly forming a mounting assembly. Fastening assemblies comprise a spherical rod end comprising a spherical member having a through opening and an integrally threaded shaft, first and second seating members on opposite sides of the spherical member and each having a through opening that is substantially coaxial with the spherical member through opening, and a partially threaded fastener that threadably engages each mounting bracket forming the mounting assembly. Structural members have axial end portions, each releasably coupled to a mounting bracket by the integrally threaded shaft. Axial end portions are threaded in opposite directions for permitting structural member rotation to adjust a length thereof to a substantially zero strain position. Structural members may be vibration isolator struts in vibration isolation systems.
Document ID
20160011046
Acquisition Source
Goddard Space Flight Center
Document Type
Other - Patent
Authors
Young, Ken
Hindle, Timothy
Barber, Tim Daniel
Date Acquired
September 6, 2016
Publication Date
August 9, 2016
Subject Category
Structural Mechanics
Report/Patent Number
Patent Number: US-Patent-9,410,596
Patent Application Number: US-Patent-Appl-SN-13/289,815
Funding Number(s)
CONTRACT_GRANT: NNG09HR00C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,410,596
Patent Application
US-Patent-Appl-SN-13/289,815
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