Assessment of Current Turbine Engine High Cycle Fatigue Test Methods

Author:

Nichol K. L.1

Affiliation:

1. Experimental Design & Analysis Solutions, Inc., 318 Shadow Creek Drive, Brentwood, TN 37027

Abstract

Testing of turbine engine components to verify structural durability goals is performed in a variety of ways and at a variety of facilities. Further, methods used differ between engine companies and even among engine programs within the same company. A recent emphasis on reducing high cycle fatigue (HCF) failures of engine components has made it obvious that improvements and standardization of HCF test methods are needed. This paper presents findings from an assessment of current HCF test approaches and identifies weaknesses that form the basis for recommending improvements. Weaknesses identified included data processing, mode identification, and selection of instrumentation locations.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference12 articles.

1. Heiser, W. H., and May, R., 1996, “U.S. Air Force Engine Management…A Cradle-to Grave Process,” Global Gas Turb. News, 36, No. 2, p. 9.

2. Thompson, D. E., and Griffin, J. T., 1999, “The National Turbine Engine High Cycle Fatigue Program,” Global Gas Turb. News, 39, No. 1, pp. 14–17.

3. Purcell, T. E. , 1996, “Dynamic Stress Analysis of Gas Turbine Rotor Airfoils Using Thermoelastic Techniques,” Exp. Tech., May/June, pp. 9–13.

4. Tibbals, T. F., Bapty, T. A., and Abbot, B. A., 1994, “CADDMAS: A Real-Time Parallel System for Dynamic Data Analysis,” ASME Paper No. 94-GT-194.

5. Tibbals, T. F., Sensmeier, M. D., Nichol, K. L., Stoner, A., and Biegl, C., 1999, “Model Integrated Testing for Durability Assessment of Turbine Engines,” ITEA Conference Proceedings, University of Tennessee Space Institute, Tullahoma, TN, Oct.

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