|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 66|
A power generating apparatus for use with an aircraft gas turbine engine has a low pressure spool assembly which includes an electrical generator. The electrical generator includes a generator stator supported on a stationary structure of the engine and a generator rotor rotatable around the generator stator and mounted to the low pressure spool assembly.
1. A power generating apparatus comprising an aircraft gas turbine engine having a low pressure compressor assembly including a bladed propulsor rotatable in response to ram air passing through the engine, an electrical generator including a generator stator and a generator rotor, and a power conditioning apparatus, the power conditioning apparatus providing first and second electrical outputs, the first having a higher voltage than the second, the generator rotor connected to a rotor disc of the low pressure compressor assembly for rotation with the bla...