Hybrid-electric propulsion system, method of assessing engine, and assessment control system
The invention relates to a hybrid-electric propulsion system for an aircraft, a computer-implemented method of assessing a health of a gas turbine engine of the hybrid-electric propulsion system, andan assessment control system. The method includes receiving, by one or more computing devices, data i...
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Main Authors | , , |
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Format | Patent |
Language | Chinese English |
Published |
25.12.2018
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Subjects | |
Online Access | Get full text |
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