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Saddle clamp assemblyA saddle clamp assembly is presented. The assembly is comprised of a hollow cylindrical body centered about a longitudinal axis and being diametrically split into semicircular top and bottom sections. Each section has a pair of connection flanges, at opposite ends, that project radially outward. A pair of bolts are retained on the top section flanges and are threadable into nuts retained on the bottom section flanges. A base member is anchored to a central underside portion of the bottom clamp body section and has a pair of connection tabs positioned beneath the bottom clamp body section connection flanges on opposite sides of the clamp axis. A pair of bolts are retained on the base member connection tabs and are threadable into a pair of nuts retainable on a support structure. The connection tab and connection flanges on each side of the clamp body are axially offset in a manner permitting downward installation/removable tool access to the lower bolts past the connection flanges. An elongated retention tether is used to connect the top clamp body section to the balance of the clamp assembly. This prevents loss of the top clamp body section when it is removed from the bottom clamp body section.
Document ID
19950008891
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Belrose, Charles R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 17, 2013
Publication Date
January 25, 1994
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-977468
Patent Number: NASA-CASE-MFS-28701-1
Patent Number: US-PATENT-5,281,042
Accession Number
95N15305
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MFS-28701-1|US-PATENT-5,281,042
Patent Application
US-PATENT-APPL-SN-977468
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