Bearing housing of an exhaust-gas turbocharger
09739172 · 2017-08-22
Assignee
Inventors
Cpc classification
F01D25/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C6/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B23P15/00
PERFORMING OPERATIONS; TRANSPORTING
B23P17/00
PERFORMING OPERATIONS; TRANSPORTING
F05D2240/54
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/162
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T29/49988
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
F16C17/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2360/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C35/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2230/51
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B23P17/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A bearing housing (1) of an exhaust-gas turbocharger, having a compressor-side housing flange (2), a central housing section (3) which is integrally connected to the housing flange (2) and in which a first partial section (4) of an oil chamber (5) is arranged; and a turbine-side housing section (6) which has a turbine-side housing flange (7) and in which a second partial section (8) of the oil chamber (5) is formed. The central housing section (3) and the turbine-side housing section (6) are formed in one piece. A bearing housing (9) which forms a separate component is inserted into the central housing section (3) and into the turbine-side housing section (6), with these delimiting the oil chamber (5).
Claims
1. A bearing housing (1) of an exhaust-gas turbocharger, with a compressor-side housing flange (2), a turbine-side housing flange (7), and a central housing section (3) which is integrally connected to the compressor-side housing flange (2) and turbine-side housing flange (7), and in which an oil inlet bore (20) having a single inlet opening and a single outlet opening is arranged; wherein a bearing sleeve (9), having an outer circumferential surface, an inner cylindrical bore, and oil inflow ducts (11, 12), each oil inflow duct having a single inlet opening and a single outlet opening, as a separate component is inserted into the central housing section (3) and fixed against rotation an axially extending oil supply channel (4) in communication with the oil inlet bore (20) outlet opening and the oil inflow duct (11, 12) inflow openings, and an oil collection chamber (5), are defined between the bearing sleeve (9) outer circumferential surface and the central housing section (3), said oil supply channel (4) and said oil collection chamber (5) being separated at the outer circumferential surface of the bearing sleeve (9) by a barrier, and axially spaced journal bearings are inserted in the inner cylindrical bore of the bearing sleeve (9), wherein the oil inlet bore (20), oil supply channel (4) and oil inflow ducts (11, 12) are in communication with the journal bearings, and wherein the bearing housing extends axially between a compressor end and a turbine end, and wherein the bearing sleeve (9) extends axially in the direction of the turbine beyond the turbine end of the bearing housing (1).
2. The bearing housing (1) as claimed in claim 1, wherein the bearing sleeve (9) is substantially cylindrical and of constant diameter to the extent housed in the bearing housing (1).
3. A bearing housing (1) of an exhaust-gas turbocharger, with a compressor-side housing flange (2), a turbine-side housing flange (7), and a central housing section (3) which is integrally connected to the compressor-side housing flange (2) and turbine-side housing flange (7), and in which an oil inlet bore (20) having a single inlet opening and a single outlet opening is arranged; wherein a bearing sleeve (9), having an outer circumferential surface, an inner cylindrical bore, and oil inflow ducts (11, 12), each oil inflow duct having a single inlet opening and a single outlet opening, as a separate component is inserted into the central housing section (3) and fixed against rotation an axially extending oil supply channel (4) in communication with the oil inlet bore (20) outlet opening and the oil inflow duct (11, 12) inflow openings, and an oil collection chamber (5), are defined between the bearing sleeve (9) outer circumferential surface and the central housing section (3), said oil supply channel (4) and said oil collection chamber (5) being separated at the outer circumferential surface of the bearing sleeve (9) by a barrier, and axially spaced journal bearings are inserted in the inner cylindrical bore of the bearing sleeve (9), wherein the oil inlet bore (20), oil supply channel (4) and oil inflow ducts (11, 12) are in communication with the journal bearings, and a water chamber (10) is provided which is separate from the oil chamber (5) and which is delimited by the central housing section (3) and the bearing sleeve (9).
4. The bearing housing (1) as claimed in claim 3, wherein the water chamber (10) is of semi-circular design.
5. The bearing housing (1) as claimed in claim 3, wherein the water chamber (10) is provided with two water ports (13, 14).
6. The bearing housing (1) as claimed in claim 3, wherein the water chamber (10) has only one water port (13).
7. A bearing housing (1) of an exhaust-gas turbocharger, with a compressor-side housing flange (2), a turbine-side housing flange (7), and a central housing section (3) which is integrally connected to the compressor-side housing flange (2) and turbine-side housing flange (7), and in which an oil inlet bore (20) having a single inlet opening and a single outlet opening is arranged; wherein a bearing sleeve (9), having an outer circumferential surface, an inner cylindrical bore, and oil inflow ducts (11, 12), each oil inflow duct having a single inlet opening and a single outlet opening, as a separate component is inserted into the central housing section (3) and fixed against rotation an axially extending oil supply channel (4) in communication with the oil inlet bore (20) outlet opening and the oil inflow duct (11, 12) inflow openings, and an oil collection chamber (5), are defined between the bearing sleeve (9) outer circumferential surface and the central housing section (3), said oil supply channel (4) and said oil collection chamber (5) being separated at the outer circumferential surface of the bearing sleeve (9) by a barrier, and axially spaced journal bearings are inserted in the inner cylindrical bore of the bearing sleeve (9), wherein the oil inlet bore (20), oil supply channel (4) and oil inflow ducts (11, 12) are in communication with the journal bearings, and a heat decoupling chamber (25) is provided which, at its end pointing toward the shaft (16), is closed off by the bearing sleeve (9).
Description
(1) Further details, advantages and features of the invention will emerge from the following description of exemplary embodiments on the basis of the drawing, in which:
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(15) The central housing section 3 and the turbine-side housing section 6 are formed in one piece, and the bearing sleeve 9, which forms a separate component, is inserted in the central housing section 3 and turbine-side housing section 6. The advantage of said arrangement is that the bearing sleeve 9 and the two housing sections 3 and 6 together delimit the oil chamber 5.
(16) It can also be seen from
(17) In an alternative embodiment, the bearing sleeve 9 may be divided into two sleeve parts which, in the assembled state, are inserted in alignment one behind the other in the central housing section 3 and the turbine-side housing section 6.
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(22) The method according to the invention which can be carried out with the core 23 has the following method steps:
(23) casting a single-piece bearing housing shell;
(24) separately manufacturing the bearing sleeve 9; and
(25) inserting the bearing sleeve 9 into the bearing housing shell.
(26) The advantage of the method according to the invention is that, during the casting process, a single-piece bearing housing shell with a water chamber 10 and an oil chamber 5 is produced. As can be seen from
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(30) Here,
(31) To supplement the above written disclosure, reference is explicitly made to the diagrammatic illustration of the invention in
LIST OF REFERENCE SYMBOLS
(32) 1 Bearing housing 2 Compressor-side housing flange 3 Central housing section 4 First partial section 5 Oil chamber 5.sub.ÖK Oil core 6 Turbine-side housing section 7 Turbine-side housing flange 8 Second partial section 9 Bearing sleeve 10 Water chamber 10.sub.WK Water core 11, 12 Oil inlet ducts 13, 14 Water ports 13.sub.AK Water port core 14.sub.AK Water port core 15 Compressor wheel 16 Shaft 17 Bearing arrangement 18 Turbine-side bearing arrangement 19 Turbine wheel 20 Oil inlet 21 Oil outlet 22 Axial bearing 23 Combined oil/water core 23′ Alternative core 24 Adapter port 25 Heat decoupling chamber K Core LG Bearing housing ÖK Oil core ÖR Oil chamber WAK Water core WR Water chamber WA.sub.1-WA.sub.4 Water ports