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Composite Stress Rupture: A New Reliability Model Based on Strength Decay

Authors :
Reeder, James R
Publication Year :
2012
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2012.

Abstract

A model is proposed to estimate reliability for stress rupture of composite overwrap pressure vessels (COPVs) and similar composite structures. This new reliability model is generated by assuming a strength degradation (or decay) over time. The model suggests that most of the strength decay occurs late in life. The strength decay model will be shown to predict a response similar to that predicted by a traditional reliability model for stress rupture based on tests at a single stress level. In addition, the model predicts that even though there is strength decay due to proof loading, a significant overall increase in reliability is gained by eliminating any weak vessels, which would fail early. The model predicts that there should be significant periods of safe life following proof loading, because time is required for the strength to decay from the proof stress level to the subsequent loading level. Suggestions for testing the strength decay reliability model have been made. If the strength decay reliability model predictions are shown through testing to be accurate, COPVs may be designed to carry a higher level of stress than is currently allowed, which will enable the production of lighter structures

Subjects

Subjects :
Composite Materials

Details

Language :
English
Database :
NASA Technical Reports
Notes :
WBS 869021-03-07.02.01
Publication Type :
Report
Accession number :
edsnas.20120008181
Document Type :
Report