POWER GENERATION DEVICE AND CORRESPONDING AIRCRAFT
A power generation device, comprising: a gas turbine engine (200) including a rotor shaft (204) and a first casing (208) around the rotor shaft (204); a transmission (212) connecting the rotor shaft (204) to a gearbox (210), the transmission (212) comprising a drive shaft (216) and a second casing (...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | A power generation device, comprising: a gas turbine engine (200) including a rotor shaft (204) and a first casing (208) around the rotor shaft (204); a transmission (212) connecting the rotor shaft (204) to a gearbox (210), the transmission (212) comprising a drive shaft (216) and a second casing (218) around the drive shaft (216); one or more permanent magnets (202) attached to the rotor shaft (204) and/or the drive shaft (216); one or more coils (206) attached to the first casing (208) and/or the second casing (218); an electrical device connected to the coils (206), the electrical device receives electrical energy generated by the coils (206) when the engine (200) is running so as to rotate the permanent magnets (202) on the shaft, and magnetic fields generated by the permanent magnets (202) interact with the coils (206); the electrical energy reduces transient and peak electrical power demands on the engine (200). |
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