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Thermal-stress-free fasteners for joining orthotropic materialsHot structures fabricated from orthotropic materials are an attractive design option for future high speed vehicles. Joining subassemblies of these materials with standard cylindrical fasteners can lead to loose joints or highly stressed joints due to thermal stress. A method has been developed to eliminate thermal stresses and maintain a tight joint by shaping the fastener and mating hole. This method allows both materials (fastener and structure), with different coefficients of thermal expansion (CTEs) in each of the three material directions, to expand freely with temperature yet remain in contact. For the assumptions made in the analysis, the joint will remain snug, yet free of thermal stress at any temperature. Finite element analysis was used to verify several thermal-stress-free fasteners and to show that conical fasteners, which are thermal-stress-free for isotropic materials, can reduce thermal stresses for transversely isotropic materials compared to a cylindrical fastener. Equations for thermal-stress-free shapes are presented and typical fastener shapes are shown.
Document ID
19870018635
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blosser, M. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1987
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:100489
NASA-TM-100489
Report Number: NAS 1.15:100489
Report Number: NASA-TM-100489
Accession Number
87N28068
Funding Number(s)
PROJECT: RTOP 506-53-33-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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