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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Main Authors | , , , |
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Format | Patent |
Language | English French German |
Published |
15.05.2024
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Subjects | |
Online Access | Get full text |
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