Turbine housing of an exhaust-gas turbocharger
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F04D-029/42
F02C-006/12
F01D-025/24
F01D-009/02
F02B-037/02
출원번호
US-0455813
(2012-04-25)
등록번호
US-9097181
(2015-08-04)
우선권정보
DE-10 2011 050 506 (2011-05-19)
발명자
/ 주소
Grussmann, Elmar
출원인 / 주소
BENTELER AUTOMOBIL TECHNIK GMBH
대리인 / 주소
Henry M. Feiereisen LLC
인용정보
피인용 횟수 :
0인용 특허 :
2
초록▼
A turbine housing of an exhaust-gas turbocharger includes an outer housing, an inner housing, and a tubular fitting which is formfittingly connected to the inner housing and has a flange collar for attachment of a bearing case of a turbine wheel. The inner housing traverses the fitting and has an en
A turbine housing of an exhaust-gas turbocharger includes an outer housing, an inner housing, and a tubular fitting which is formfittingly connected to the inner housing and has a flange collar for attachment of a bearing case of a turbine wheel. The inner housing traverses the fitting and has an end portion which is bent radially outwards about the flange collar. A press ring is arranged upon the end portion for additional securement of the inner housing in place.
대표청구항▼
1. A turbine housing of an exhaust-gas turbocharger, comprising: an outer housing;an inner housing;a tubular fitting formfittingly connected to the inner housing and having a flange collar for attachment of a bearing case of a turbine wheel, said inner housing traversing the fitting and having an en
1. A turbine housing of an exhaust-gas turbocharger, comprising: an outer housing;an inner housing;a tubular fitting formfittingly connected to the inner housing and having a flange collar for attachment of a bearing case of a turbine wheel, said inner housing traversing the fitting and having an end portion bent radially outwards about the flange collar; anda press ring arranged upon the end portion for additional positional fixation of the inner housing upon the flange collar. 2. The turbine housing of claim 1, wherein the end portion of the inner housing has a C-shaped configuration. 3. The turbine housing of claim 1, wherein the flange collar has a bulged configuration pointing in a radial direction of a rotation axis of the turbine wheel. 4. The turbine housing of claim 1, wherein the inner housing has at least one region bearing upon the fitting in a radial direction. 5. The turbine housing of claim 1, wherein the end portion of the inner housing is arranged so as to point in an axial direction of a rotation axis of the turbine wheel away from the turbine housing. 6. The turbine housing of claim 1, wherein the press ring is constructed for contact upon at least one of member selected from the group consisting of the end portion of the inner housing and an inner surface area of the fitting. 7. The turbine housing of claim 6, wherein the press ring is constructed for frictional engagement upon the member. 8. The turbine housing of claim 1, wherein the press ring and the end portion define a braze gap. 9. The turbine housing of claim 8, wherein the braze gap provides for a material joint. 10. The turbine housing of claim 9, further comprising a solder for introduction in the braze gap to provide a solder joint as the material joint between the press ring and the fitting. 11. The turbine housing of claim 1, further comprising a formfitting connection between contacting surfaces of the press ring and the fitting. 12. The turbine housing of claim 11, wherein one of the contacting surfaces is an inner surface of the fitting. 13. The turbine housing of claim 11, wherein the formfitting connection is configured as a toothing between the contacting surfaces. 14. The turbine housing of claim 11, further comprising a solder for providing a solder joint between the contacting surfaces. 15. The turbine housing of claim 1, further comprising a formfitting connection between contacting surfaces of the flange collar and the end portion of the inner housing. 16. The turbine housing of claim 15, wherein the formfitting connection is configured as a toothing between the contacting surfaces. 17. The turbine housing of claim 15, further comprising a solder for providing a solder joint between the contacting surfaces. 18. The turbine housing of claim 1, further comprising a formfitting connection between contacting surfaces of the fitting on a turbine side thereof and the inner housing. 19. The turbine housing of claim 18, wherein the formfitting connection is configured as a toothing between the contacting surfaces. 20. The turbine housing of claim 19, wherein the toothing is a micro toothing. 21. The turbine housing of claim 18, further comprising a solder for providing a solder joint between the contacting surfaces. 22. The turbine housing of claim 1, wherein the press ring is made of steel. 23. The turbine housing of claim 1, wherein the press ring and the fitting are made of a same material. 24. The turbine housing of claim 1, wherein the press ring is made of a steel alloy including the following chemical constituents, expressed in weight-%: Carbon (C) ≦0.20Silicon (Si) ≦1.50 to 2.00Manganese (Mn) ≦2.00Phosphorus (P)≦0.045Sulfur (S) ≦0.015Chromium (Cr) 19.00 to 21.00Nickel (Ni) 11.00 to 13.00Nitrogen (N) ≦0.11,the remainder iron and incidental smelting-related impurities. 25. The turbine housing of claim 24, wherein the, the steel alloy has a yield strength Rp0.2 of 230 N/mm and a tensile strength of 550 N/mm2 to 750 N/mm2.
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이 특허에 인용된 특허 (2)
Grussmann,Elmar; Smatloch,Christian; Hinder,Axel; K?rner,Thomas; M?ller,Rainer, Casing arrangement for a turbocharger of an internal combustion engine.
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