Controllable exhaust gas turbocharger with a double-fluted turbine housing
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-017/14
F02B-037/18
F02B-037/22
F02D-023/00
출원번호
US-0069155
(2002-08-20)
우선권정보
DE-0024228 (1999-05-27)
국제출원번호
PCT/US00/14295
(2000-05-24)
국제공개번호
WO00/73630
(2000-12-07)
발명자
/ 주소
Engels, Berthold
Forster, Arno
Lingenauber, Robert
Jaisle, Jens-Wolf
출원인 / 주소
BorgWarner, Inc.
대리인 / 주소
Pendorf & Cutliff
인용정보
피인용 횟수 :
26인용 특허 :
10
초록▼
An exhaust gas-driven turbocharger (1) exhibits an adjustable radial turbine (2) which powers a compressor (3) by way of a common shaft (4), whereby a turbine housing (5) designed with a multiplicity of scrolls surround the turbine wheel (6) and exhibits at least two afflux ports (7a, 7b) annularly
An exhaust gas-driven turbocharger (1) exhibits an adjustable radial turbine (2) which powers a compressor (3) by way of a common shaft (4), whereby a turbine housing (5) designed with a multiplicity of scrolls surround the turbine wheel (6) and exhibits at least two afflux ports (7a, 7b) annularly encompassing the turbine wheel (6), whose outlets (8a, 8b) at least partly surround the wheel approach (9) of the turbine wheel (6) and which are at an axial distance from one another. An annular, axially displaceable coupler (15) is provided for opening and closing the outlet (8a, 8b) of at least one afflux port (7a, 7b), so that the boost pressure of the turbine can be influenced thereby.
대표청구항▼
An exhaust gas-driven turbocharger (1) exhibits an adjustable radial turbine (2) which powers a compressor (3) by way of a common shaft (4), whereby a turbine housing (5) designed with a multiplicity of scrolls surround the turbine wheel (6) and exhibits at least two afflux ports (7a, 7b) annularly
An exhaust gas-driven turbocharger (1) exhibits an adjustable radial turbine (2) which powers a compressor (3) by way of a common shaft (4), whereby a turbine housing (5) designed with a multiplicity of scrolls surround the turbine wheel (6) and exhibits at least two afflux ports (7a, 7b) annularly encompassing the turbine wheel (6), whose outlets (8a, 8b) at least partly surround the wheel approach (9) of the turbine wheel (6) and which are at an axial distance from one another. An annular, axially displaceable coupler (15) is provided for opening and closing the outlet (8a, 8b) of at least one afflux port (7a, 7b), so that the boost pressure of the turbine can be influenced thereby. ring to a central processing unit, the mechanism comprises: a fixing member, moveably mounted on the absorbing member, comprising a head at a distance from the absorbing member and a neck with a diameter smaller than the diameter of the head; an elastic member, moveably mounted to the neck of the fixing member; and a disassociating flake, moveably mounted to the neck of the fixing member, comprising a body passed through by the neck of the fixing member, a forcing portion corresponding to the central processing unit mounted on a side of the body with a different angle, and a pulled portion mounted on the other side of the body, when disassociating the absorbing member from the surface of the central processing unit, the pulled portion being pulled to press the elastic member, the disassociating flake rotating around the fixing member in the meanwhile, so the forcing member moving relative to the central processing unit to press the surface of the central processing unit for completely disassociating, then the elastic member moving the disassociating flake back to its original place by elasticity. 11. The radiation apparatus of claim 10, wherein the elastic member, a leaf spring, comprises a pressing end and a forcing end, the neck of the fixing member passing through the elastic member between the pressing end and the forcing end, after the pulled portion being pulled, the pressing end and the pulled portion moving at the same time, the forcing end and the body rotating together, and the forcing end pressing the body for disassociating the absorbing member. 12. The radiation apparatus of claim 11, wherein the elastic member comprises a hole for the neck of the fixing member to pass through. 13. The radiation apparatus of claim 10 further comprises a sleeve moveably mounted to the neck of the fixing member passing through the disassociating flake, and the sleeve and the head of the fixing member clipping the elastic member. 14. The radiation apparatus of claim 13, wherein the absorbing member comprises a screw hole, the neck of the fixing member comprising an outer screw thread, the sleeve comprising an inner screw thread corresponding to the outer screw thread for combining the fixing member and the sleeve. 15. The radiation apparatus of claim 10, wherein the disassociating flake further comprises a hollow for the neck of the fixing member to pass through. 16. The radiation apparatus of claim 10, wherein the fixing member is a screw.
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이 특허에 인용된 특허 (10)
Moser Peter (Boppelsen CHX), Controllable exhaust gas turbocharger.
Ferrari, Sebastian; Massart, Eduardo; Lombard, Alain; Mitka, Jerome, Method of controlling a turbocharger having a variable-geometry mechanism and a waste gate.
Kindl, Helmut Matthias; Schorn, Norbert Andreas; Smiljanovski, Vanco; Sommerhoff, Franz Arnd; Kuske, Andreas; Kemmerling, Joerg, System and method for variable tongue spacing in a multi-channel turbine in a charged internal combustion engine.
Hittle, Craig Phillip; Kilkenny, Jonathan P.; Pierpont, David Andrew; Roozenboom, Stephan Donald, Turbocharger having balance valve, wastegate, and common actuator.
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