|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02B-033/44 F01D-017/16 F02C-006/12|
|미국특허분류(USC)||060/598; 060/605.2; 060/605.3; 415/112; 415/191; 415/178; 415/208.2; 415/229|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 48|
A bearing housing of a rotor shaft support assembly of a turbocharger core mounts to and closes a forward end of a cavity that both receives and discharges exhaust gases of an internal combustion engine. A turbine rotor operatively coupled to a rotor shaft and a compressor rotor of an associated turbocharger rotor assembly rotates within a turbine rotor shroud portion of an associated turbine nozzle cartridge assembly, wherein the rotor shaft is rotationally supported by at least one bearing within the bearing housing. The turbine nozzle cartridge assemb...
1. A turbocharger core adapted to cooperate with a cavity that provides for both receiving and discharging exhaust gases of an internal combustion engine, comprising: a. a turbocharger rotor assembly comprising: i. a turbine rotor;ii. a compressor rotor; andiii. a rotor shaft operatively coupling said turbine rotor to said compressor rotor, wherein said turbine rotor, said compressor rotor and said rotor shaft are operative about a common axis of rotation of said turbocharger rotor assembly;b. a rotor shaft support assembly comprising: i. a bearing housi...