High bandwidth control of turbofan/turboprop thrust response using embedded electric machines
Systems and methods for high bandwidth control of thrust response for turbofan or turboprop engines are provided. Such systems and methods include an engine control system that processes a rate command and a feedback signal from an engine to generate separate fuel and electric machine control signal...
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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
11.06.2024
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Subjects | |
Online Access | Get full text |
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Summary: | Systems and methods for high bandwidth control of thrust response for turbofan or turboprop engines are provided. Such systems and methods include an engine control system that processes a rate command and a feedback signal from an engine to generate separate fuel and electric machine control signals that respectively control fuel and electric machine dynamics of the engine to produce engine dynamics that result in desired thrust response. |
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Bibliography: | Application Number: US202217942525 |