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As integrated electric starter/generator (ES/G) is becoming popular in gas-turbine engines for aerospace applications, we show how this ES/G, such a two-role device, could be used as an actuator during flight to impose extra shaft torque. The imposed extra shaft torque is shown to enhance engine transient operations.

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This page is a summary of: Active Energy Management for Enhanced Engine Transient Operations, Journal of Propulsion and Power, September 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b39242.
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