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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Bibliographic Details
Main Authors MILLER BRANDON WAYNE, ADIBHATLA SRIDHAR, GANSLER MICHAEL THOMAS
Format Patent
LanguageChinese
English
Published 25.12.2018
Subjects
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