초록 ▼

A gas turbine engine arrangement comprises a core engine, a power turbine and a propulsor. The core engine comprises at least one compressor and at least one turbine arranged to drive the at least one compressor and the core engine is arranged in a casing. The power turbine is positioned downstream

A gas turbine engine arrangement comprises a core engine, a power turbine and a propulsor. The core engine comprises at least one compressor and at least one turbine arranged to drive the at least one compressor and the core engine is arranged in a casing. The power turbine is positioned downstream of the at least one turbine and the power turbine is arranged to drive the propulsor. An electrical machine is arranged upstream of the at least one compressor. The electrical machine comprises a stator and a rotor and the electrical machine comprises a motor/generator. A first clutch selectively connects the rotor of the electrical machine to the power turbine and a second clutch selectively connects the rotor of the electrical machine to the at least one compressor of the core engine.

대표청구항 ▼

1. A method of operating a gas turbine engine that includes a core engine arranged in a casing that has a propulsor, a compressor and a first turbine arranged to drive said compressor, a power turbine positioned downstream of the first turbine and being arranged to drive the propulsor, an electrical

1. A method of operating a gas turbine engine that includes a core engine arranged in a casing that has a propulsor, a compressor and a first turbine arranged to drive said compressor, a power turbine positioned downstream of the first turbine and being arranged to drive the propulsor, an electrical machine configured upstream of the compressor having a stator and a rotor, a motor/generator, a first clutch to selectively connect the rotor of the electrical machine to the power turbine and a second clutch to selectively connect the rotor of the electrical machine to the compressor of the core engine, the method comprising the steps of: in a first mode of operation,disconnecting the rotor of the electrical machine from the power turbine using the first clutch,connecting the rotor of the electrical machine to the at least one compressor using the second clutch; andoperating the electrical machine as an electrical motor such that the electrical machine starts the gas turbine engine,in a second mode of operation,disconnecting the rotor of the electrical machine from the at least one compressor using the second clutch,connecting the rotor of the electrical machine to the power turbine using the first clutch; andoperating the electrical machine as an electrical generator such that the power turbine drives the rotor of the electrical machine to generate electricity; andin a third mode of operation,connecting the power turbine and the rotor of the electrical machine using the first clutch;connecting the rotor of the electrical machine and the at least one compressor using the second clutch such that the power turbine drives the at least one compressor. 2. A method as claimed in claim 1 comprising the steps of operating in the third mode to transfer power from the power turbine to the at least one compressor to improve the stability of the core engine. 3. A method as claimed in claim 1 comprising the steps of operating in the third mode to transfer power from the power turbine to the at least one compressor such that the power turbine restarts the gas turbine engine during windmilling of the gas turbine engine.