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Systems and methods for determining strength of cylindrical structures by internal pressure loading

Patent ·
OSTI ID:1207245
In one embodiment, an apparatus, includes: a mandrel; an expansion cylinder, comprising: opposite first and second ends; an inner circumferential surface extending between the ends and characterized by an inner diameter, the inner circumferential surface defining a hollow cavity; an outer circumferential surface extending between the ends and characterized by an outer diameter that is greater than the inner diameter; and a plurality of slots extending from the inner circumferential surface to the outer circumferential surface and latitudinally oriented between the ends; and one or more base plates configured to engage one of the ends of the expansion cylinder. In another embodiment, a method includes: arranging an expansion cylinder inside a test cylinder; arranging a mandrel inside the expansion cylinder; applying a force to the mandrel for exerting a radial force on the expansion cylinder; and detecting one or more indicia of structural failure of the test cylinder.
Research Organization:
Lawrence Livermore National Laboratory (LLNL), Livermore, CA (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
AC52-07NA27344
Assignee:
Lawrence Livermore National Security, LLC (Livermore, CA)
Patent Number(s):
9,097,602
Application Number:
13/748,443
OSTI ID:
1207245
Country of Publication:
United States
Language:
English

References (19)

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Experimental Failure Effect Analysis of Composite High-Speed Flywheel Rotors book January 2003
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Effect of winding tension and cure schedule on residual stresses in radially-thick fiber composite rings journal September 1991
Behavior of a Unidirectional Metal-Matrix Composite Under Thermomechanical Loading journal July 1996

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