Cumulative damage model for structural analysis of filed polymeric materials

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United States of America Patent

PATENT NO 6301970
SERIAL NO

09366763

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Abstract

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A method of predicting fatigue failure in a filled polymeric material is provided. The method involves the calculation of stress at the region of highest stress using an equation which includes as parameters, regression coefficients of the stress vs. modulus obtained from a finite element analysis. Once the regression coefficients are obtained, there is no further need to perform a finite element analysis. The calculated stresses are numerically integrated in a damage equation using a Monte Carlo method, using a cumulative model to estimate when failure will occur. The method has been tested in the case of temperature stress loading of a solid propellant rocket motor.

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Patent Owner(s)

Patent OwnerAddress
NAVY UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THECHIEF OF NAVAL RESEARCH OFFICE OF COUNSEL BALLSTON TOWER ONE 800 NORTH QUINCY STREET ARLINGTON VA 22217

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Biggs, Gary L Silver Spring, MD 3 46
Nestor, III John J Silver Spring, MD 1 27

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