Method and apparatus for predicting failure in a system
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[0063] The following example describes the modeling and prediction of failure in an exemplary embodiment according to the present invention.
[0064] FIGS. 5(a)-5(f) illustrate a preferred embodiment of the invention applied to a single dynamic component, namely a composite helicopter rotor hub. Reference numerals refer to the elements as they were discussed with respect to FIGS. 1-4. In this example engineering analysis step 12 first incorporates a probabilistic approach using response surface FPM 88 techniques. Thereafter, the same example is used to demonstrate any difference that response surface ST 90, direct FPM 92, or direct ST 94 would have yielded.
[0065] A helicopter rotor hub is a structure to which the blades of the helicopter are attached. The rotor hub is a composite laminate structure, which means that it is manufactured by laying plies of composite sheets together and joining them (with an adhesive resin) to form an integral structure. Each composite sheet is called a ...
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