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Damage Tolerance and Reliability of Turbine Engine ComponentsA formal method is described to quantify structural damage tolerance and reliability in the presence of multitude of uncertainties in turbine engine components. The method is based at the materials behaviour level where primitive variables with their respective scatters are used to describe the behavior. Computational simulation is then used to propagate those uncertainties to the structural scale where damage tolerance and reliability are usually specified. Several sample cases are described to illustrate the effectiveness, versatility, and maturity of the method. Typical results from these methods demonstrate that the methods are mature and that they can be used for future strategic projections and planning to assure better, cheaper, faster, products for competitive advantages in world markets. These results also indicate that the methods are suitable for predicting remaining life in aging or deteriorating structures.
Document ID
19990070407
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 19, 2013
Publication Date
March 1, 1999
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Public Use Permitted.
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