SPEED LIMITING FOR POWER TURBINE GOVERNING AND PROTECTION IN A TURBOSHAFT ENGINE

A turboshaft engine for a helicopter, comprising: a gas generator (102; 202); a power turbine (104) disposed downstream of the gas generator (102; 202); and a controller (132; 232) in communication with the gas generator (102; 202) and the power turbine (104), the controller (132; 232) including a p...

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Bibliographic Details
Main Authors MEISNER, Richard P, CROWLEY, Timothy J, CAI, Chaohong, MA, David Lei
Format Patent
LanguageEnglish
French
German
Published 15.05.2024
Subjects
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