|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||290/52 ; 290/2 ; 417/406|
|발명자 / 주소|
|인용정보||피인용 횟수 : 42 인용 특허 : 1|
The invention provides a turbocharger (20), compressor (170) and turbine (172) rotors mounted on a shaft (160) supported by ball bearing assemblies (162, 164) such that the compressor rotor (172) and turbine rotor (170) are overhung to one side of the bearing assemblies with the turbine rotor separated from the bearing assemblies by the compressor rotor. The turbocharger (20) includes a turbine nozzle area (230) having a plurality of nozzle vanes (234) spaced circumferentially about the turbine rotor and in the nozzle area through which exhaust air from ...
A turbojet comprising: a housing having a flow channel communicating between a compressor inlet and a turbine exhaust, a radical flow compressor rotor fitted within said housing for receiving and compressing air from the compressor inlet and for directing compressed air along the flow channel, a fuel means for introducing fuel with said air flow channel to form an air fuel mixture within said air flow channel, ignition means within said air flow channel downstream of said compressor rotor for igniting the air fuel mixture to produce combustion gases, a t...