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Compression Springs at Elevated TemperaturesThe behavior of compression springs is affected by increased temperatures. The most significant factors affecting springs are a loss of load and length (relaxation), and a change in the modulus of rigidity. Relaxation will reduce preset loads or change the location of supported components whereas a change in the modulus of rigidity will alter the spring rate. Both factors must be taken into account when designing compression springs. Curves and equations are presented (for music wire, 18-8 stainless steel, 17-7 PH, and Inconel-X) which can aid in the design of compression springs for use at elevated temperatures.
Document ID
19660027420
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
M J Siegel
(University of Southern California Los Angeles, California, United States)
Date Acquired
August 3, 2013
Publication Date
May 19, 1966
Publication Information
Publication: Proceedings of the First Aerospace Mechanisms Symposium
Publisher: U. S. Department of Commerce
Subject Category
Structural Mechanics
Meeting Information
Meeting: 1st Aerospace Mechanisms Symposium
Location: Santa Clara, CA
Country: US
Start Date: May 19, 1966
End Date: May 20, 1966
Sponsors: Lockheed Martin (United States), Jet Propulsion Lab
Accession Number
66N36710
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Spring
Temperature effect
Compression
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