Exhaust-gas turbocharger
09732631 ยท 2017-08-15
Assignee
Inventors
Cpc classification
F02B37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C6/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T29/49398
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F01N2450/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/1805
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B67/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01D25/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C6/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An exhaust-gas turbocharger (1) having a turbine housing (2), and having an exhaust manifold (3) connected to the turbine housing (2). At least one adapter ring (4, 5) is arranged between the turbine housing (2) and the exhaust manifold (3).
Claims
1. An exhaust-gas turbocharger (1) including a turbine housing (2), wherein the turbine housing (2) is a double-walled sheet metal part comprising an outer wall and an inner wall, an exhaust manifold (3), wherein the exhaust manifold (3) is a double-walled sheet metal part comprising an outer wall and an inner wall, and a turbine-housing-side adapter ring (5) having first and second sides, the first side including a flange mating surface, the second side having an annularly encircling groove (8) into which a plug-in flange (9) of turbine housing outer wall engages, wherein the turbine-housing-side adapter ring (5) second side is welded to the turbine housing (2) outer wall, and an exhaust manifold-side adapter ring (4) having first and second sides, the first side including a flange mating surface complementary to the turbine-housing-side adapter ring (5) flange mating surface, wherein the manifold-side adapter ring (4) second side is provided with a plug-in region (6) which is engaged around by and welded to a receiving section (7) of the exhaust manifold (3) outer wall, wherein the turbine-housing-side adapter ring (5) flange mating surface is welded to the manifold-side adapter ring (4) flange mating surface.
2. A double-walled sheet metal manifold module including a double-walled turbine housing (2) comprising an internal turbine housing wall and an external turbine housing wall, a double-walled exhaust manifold (3) comprising an internal manifold wall and an external manifold wall, a turbine-housing-side adapter ring (5) having first and second sides, the first side welded to the turbine housing (2) external turbine housing wall, and a manifold-side adapter ring (4) having first and second sides, the first side welded to the exhaust manifold (3) external exhaust manifold wall and the second side welded to the turbine-housing-side adapter ring (5) second side.
3. A method for producing a double-walled sheet-metal manifold module, having the following method steps: (a) forming a double-walled turbine housing (2) comprising an outer wall and an inner wall, (b) forming a double-walled exhaust manifold (3) comprising an outer wall and an inner wall, (c) forming a manifold-side adapter ring (4) having first and second sides, the first side including a flange mating surface, the second side adapted to being welded to the exhaust manifold (3), (d) forming a turbine-housing-side adapter ring (5) having first and second sides, the first side including a flange mating surface complementary to the manifold-side adapter ring (4) flange mating surface, the second side adapted to being welded to the turbine housing (2), and (e1) welding the manifold-side adapter ring (4) second side to the manifold, aligning the turbine housing to the manifold, aligning the turbine housing adapter ring (5) relative to the turbine housing, welding the two adapter rings (4, 5) to one another at their first sides, and welding the turbine-housing-side adapter ring second side to the turbine housing, or (e2) welding the turbine-housing-side adapter ring (5) second side to the turbine housing, aligning the manifold to the turbine housing, aligning the manifold adapter ring (4) relative to the manifold, welding the two adapter rings (4, 5) to one another at their first sides, and welding the manifold-side adapter ring second side to the manifold.
Description
(1) Further details, advantages and features of the present invention will emerge from the following description of exemplary embodiments on the basis of the appended drawing, in which:
(2)
(3)
(4)
(5)
(6) The turbine housing 2 of the exhaust-gas turbocharger 1 is connected to an exhaust manifold 3, wherein the turbine housing 2 and the exhaust manifold 3 are preferably double-walled sheet-metal components.
(7) The exhaust manifold 3 has fastening flanges 12 to 15, by means of which it can be fastened, in the installed state of the exhaust-gas turbocharger 1, to an internal combustion engine not illustrated in
(8) The illustration of the exhaust manifold 3 in
(9) In the embodiment illustrated in the figures, the manifold-side adapter ring 4 is provided with a plug-in region 6 which is engaged around by a receiving region 7 of the exhaust manifold 3 in the assembled state according to
(10) The turbine-side adapter ring 5 has an annularly encircling groove 8 into which a plug-in flange 9 of the turbine housing 2 engages in the assembled state. The welding is carried out at the points denoted by the three arrows ST in
(11) As has likewise already been explained in the introduction, in each case one associated adapter ring is used both on the side of the exhaust manifold 3 and also on the side of the turbine housing 2. It is however also conceivable in principle for a single adapter ring to be used to realize the required position compensation.
(12) In addition to the written disclosure of the invention, reference is hereby explicitly made to the diagrammatic illustration thereof in
LIST OF REFERENCE SYMBOLS
(13) 1 Exhaust-gas turbocharger 2 Turbine housing 3 Exhaust manifold 4 Manifold-side adapter ring 5 Turbine-housing-side adapter ring 6 Plug-in region 7 Receiving region 8 Annular grooves 9 Plug-in flange 10 Internal pipe system 11 Plug-in connection 12-15 Flanges of the exhaust manifold 3 for mounting on the engine 16 Manifold outlet 17 Turbine housing inlet VS Connecting point (weld between turbine housing 2 and exhaust manifold 3) VB Connecting region ST Weld points