Turbochargers of this invention comprise a turbine housing and a turbine wheel rotatably disposed therein. A center housing is connected to the turbine housing, and a compressor housing is attached to the center housing. A compressor is rotatably disposed within the compressor housing, and comprises
Turbochargers of this invention comprise a turbine housing and a turbine wheel rotatably disposed therein. A center housing is connected to the turbine housing, and a compressor housing is attached to the center housing. A compressor is rotatably disposed within the compressor housing, and comprises two impellers placed in back-to-back orientation. A movable member is disposed within the compressor housing to downstream of the compressor to control the flow of air within the compressor housing. The position of the movable member can be operated to control the amount of pressurized air that is produced by one of the compressor impellers to provide enhanced compressor operating efficiency throughout the operating range and mass flow requirements of the engine.
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What is claimed is: 1. A compressor for a turbocharger comprising: a compressor wheel that comprises first and second compressor faces oriented back-to-back and a bore for mounting the compressor wheel to a shaft along a rotational axis of the compressor wheel; and a compressor housing that compris
What is claimed is: 1. A compressor for a turbocharger comprising: a compressor wheel that comprises first and second compressor faces oriented back-to-back and a bore for mounting the compressor wheel to a shaft along a rotational axis of the compressor wheel; and a compressor housing that comprises a first passage to the first compressor face wherein a wall portion of the first passage comprises an annular, contoured surface to direct inlet air in a more axial direction toward an inducer portion of the first compressor face, a second passage to an inducer portion of the second compressor face, a bifurcated air inlet oriented to receive inlet air radially relative to the rotational axis of the compressor wheel and to supply inlet air!in substantially the same condition, to the first passage and to the second passage, and a volute to receive pressurized air that is directed radially from an exducer portion of the first compressor face and an exducer portion of the second compressor face to the volute via a common passage disposed intermediate the exdueer portions and the volute wherein an outside surface of the volute and the wall portion of the first passage form, in part, a first section that projects radially inward and extends circularly within the compressor housing and wherein another outside surface of the volute and a wall portion of the second passage form, in part, a second section that projects radially inward and extends circularly within the compressor housing. 2. The compressor of claim 1 wherein the bore of the compressor wheel comprises a partial bore. 3. The compressor of claim 1 wherein the wall portion of the second passage comprises an annular, contoured surface to direct inlet air in a more axial direction toward the second compressor lace. 4. The compressor of claim 3 wherein the wall portion of the second passage comprises an opposing annular, plate-like surface for mounting the compressor housing to a center housing of a turbocharger. 5. The compressor of claim 1 further comprising a backing plate for mounting the compressor housing to a center housing of a turbocharger. 6. The compressor of claim 5 wherein a portion of the backing plate defines, in part, the second passage. 7. The compressor of claim 6 wherein the portion of the backing plate that defines, in part, the second passage comprises an annular, contoured surface to direct inlet air in a more axial direction toward the second compressor face. 8. A turbocharger comprising the compressor of claim 1. 9. A compressor for a turbocharger comprising: a compressor wheel that comprises first and second compressor faces oriented back-to-back and a bore for mounting the compressor wheel to a shaft along a rotational axis of the compressor wheel; and a multi-component compressor housing that comprises a first passage to an inducer portion of the first compressor face wherein an attachable component forms part of the first passage, covers an axial end of the compressor wheel and comprises an annular, contoured surface to direct inlet air in a more axial direction toward the inducer portion of the first compressor face and forms, in part, a first section that projects radially inward and extends circularly within the compressor housing, a second passage to an inducer portion of the second compressor face, a bifurcated air inlet oriented to receive inlet air and to supply inlet air to the first passage and to the second passage, and a volute to receive pressurized air that is directed radially from an exducer portion of the first compressor face and an exducer portion of the second compressor face to the volute via a common passage disposed intermediate the exducer portions and the volute wherein an outside surface of the volute and a wall portion of the second passage form, in part, a second section that projects radially inward and extends circularly within the compressor housing. 10. The compressor of claim 9 wherein the bore of the compressor wheel comprises a partial bore. 11. The compressor of claim 9 wherein a component of the compressor housing comprises an annular, plate-like surface for mounting the compressor housing to a center housing of a turbocharger. 12. The compressor of claim 11 wherein the attachable component attaches to the component that comprises the annular, plate-like surface. 13. A turbocharger comprising the compressor of claim 9. 14. A compressor for a turbocharger comprising: a compressor wheel that comprises first and second compressor faces oriented back-to-back and a bore for mounting the compressor wheel to a shaft along a rotational axis of the compressor wheel; and a multi-component compressor housing that comprises a first component that substantially defines a first passage to an inducer portion of the first compressor face, a second component that attaches to the first component and substantially defines a second passage to an inducer portion of the second compressor face, a bifurcated air inlet oriented to receive inlet air and to supply inlet air to the first passage and to the second passage, and a volute to receive pressurized air that is directed radially from an exducer portion of the first compressor face and an exducer portion of the second compressor face to the volute via a common passage disposed intermediate the exducer portions and the volute wherein an outside surface of the volute and a wall portion of the first component form, in part, a first section that projects radially inward and extends circularly within the compressor housing and wherein another outside surface of the volute and a wall portion of the second component form, in part, a second section that projects radially inward and extends circularly within the compressor housing. 15. The compressor of claim 14 wherein the bore of the compressor wheel comprises a partial bore. 16. A turbocharger comprising the compressor of claim 14.
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이 특허에 인용된 특허 (12)
Plunkett Francis P. (Syracuse NY), Diffuser throttle ring control.
Hiereth Hermann (Esslingen DEX) Erdmann Wolfgang (Stuttgart DEX) Sumser Siegfried (Stuttgart DEX), Exhaust gas turbocharger for a supercharged internal combustion engine.
Bates Bradford (Ann Arbor MI) Belaire Richard C. (Whitmore Lake MI) Stephan Craig H. (Ann Arbor MI), Power turbine flywheel assembly for a dual shaft turbine engine.
Kindl, Helmut Matthias; Smiljanovski, Vanco; Kemmerling, Joerg; Sommerhoff, Franz Arnd; Kuske, Andreas, Turbocharger arrangement having compressor wheels arranged in parallel and a method for operating a turbocharger arrangement.
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