Free turbine turbogenerator comprising a reversible electrical machine coupled to the free turbine
AssigneeSafran Helicopter Engines
InventorsLoïs Pierre Denis Vive, Thomas Drouin, Olivier Bedrine
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AssigneeSafran Helicopter Engines
InventorsLoïs Pierre Denis Vive, Thomas Drouin, Olivier Bedrine
Estimating the term…
Disclosed is a turbogenerator, in particular for an electrically-driven rotary wing aircraft, comprising a gas generator equipped with a first shaft, at least one reversible electrical machine, and a free turbine provided with a second shaft and caused to rotate by a gas flow generated by the gas generator. The second shaft is coupled to the at least one electrical machine during all phases of operation of the turbomachine, and the turbomachine further comprises a single mechanical coupling means for coupling the first mechanical shaft to the second mechanical shaft when the electrical machine is operating in motor mode and mechanically uncoupling the first mechanical shaft from the second mechanical shaft when the electrical machine is operating in generator mode.
A turbomachine of a free turbine turbogenerator type, comprising a gas generator equipped with a first mechanical shaft, at least one reversible electrical machine and a free turbine provided with a second mechanical shaft and caused to rotate by a gas flow generated by the gas generator,
A turbomachine of a free turbine turbogenerator type, comprising a gas generator equipped with a first mechanical shaft, at least one reversible electrical machine and a free turbine provided with a second mechanical shaft and caused to rotate by a gas flow generated by the gas generator,
Dependencies are inferred from the claim text.