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Life extending control of gas turbine engines for aircraft propulsion

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2 Author(s)
Caplin, J. ; Dept. of Mech. Eng., Pennsylvania State Univ., University Park, PA, USA ; Ray, A.

This paper examines the incorporation of a damage prediction model into the control systems synthesis of an aircraft gas turbine engine, with the objective of extending the life of critical engine components while maintaining the required level of system performance. Turbine blades are used as an example, with the primary modes of damage being high-cycle fatigue and low-cycle thermomechanical fatigue

Published in:

Decision and Control, 1997., Proceedings of the 36th IEEE Conference on  (Volume:5 )

Date of Conference:

10-12 Dec 1997