Bearing housing of an exhaust-gas turbocharger
09850912 · 2017-12-26
Assignee
Inventors
Cpc classification
F02C6/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/403
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B39/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B39/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B39/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C6/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A bearing housing (1) of an exhaust-gas turbocharger 2, having an oil guide to at least one bearing point (5) in the bearing housing (1). The oil guide is formed by at least one of bores and cutouts in the bearing housing (1). There is formed in the oil guide a siphon (10) which is integrated into the bearing housing (1).
Claims
1. A bearing housing (1) of an exhaust-gas turbocharger (2), having an oil guide within the bearing housing through which oil flows from an oil supply inlet to at least one bearing point (5) in the bearing housing (1), wherein the oil guide is formed by at least one of bores and cutouts in the bearing housing (1), and wherein there is formed in the oil guide, when the bearing housing is in the installed orientation, a flow path including a first segment (6) through which oil flows downward, followed by a second segment through which oil flows upward, followed by a third segment (14) through which oil flows downward to said at least one bearing point (5) in the bearing housing (1), wherein an oil collecting reservoir is formed between the first segment (6) and second segment (7) in which oil collects after engine shut-down, which reservoir is integrated into the bearing housing (1).
2. The bearing housing as claimed in claim 1, wherein the first segment (6), second segment (7) and third segment (14) of the oil guide are straight bores, respectively, and wherein the second segment (7) is closed off at one end by means of a plug (9).
3. The bearing housing as claimed in claim 2, wherein the plug (9) is a heating element (15).
4. The bearing housing (1) as claimed in claim 1, wherein said at least one bearing point (5) comprises first and second axially separated bearing points, and wherein an oil passage (8) is provided in said oil guide for axially distributing oil to said first and second axially separated bearing points.
5. An exhaust-gas turbocharger (2) having at least one bearing housing (1), having an oil guide through which oil flows from an oil supply inlet to at least one bearing point (5) in the bearing housing (1), wherein the oil guide is formed by at least one of bores and cutouts in the bearing housing (1), and wherein there is formed in the oil guide, when the bearing housing is in the installed orientation, a flow path including a first segment (6) through which oil flows downward, followed by a second segment (7) through which oil flows upward, followed by a third segment (14) through which oil flows downward to said at least one bearing point (5) in the bearing housing (1), wherein an oil collecting reservoir is formed between the first segment (6) and second segment (7) in which oil collects after engine shut-down, which reservoir is integrated into the bearing housing (1), and wherein the at least one bearing point (5) is for mounting a shaft (4) which connects a turbine wheel (11) to a compressor wheel (12) of the exhaust-gas turbocharger (2).
6. The exhaust-gas turbocharger (2) as claimed in claim 5, wherein the first segment (6), second segment (7) and third segment (14) of the oil guide are straight bores, respectively, and wherein the second segment (7) is closed off at one end by means of a plug (9).
7. The bearing housing as claimed in claim 6, wherein the plug (9) is a heating element (15).
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)
(7) The exhaust-gas turbocharger 2 has a bearing housing 1 which connects a turbine housing to a compressor housing. A turbine wheel 11 is arranged in the turbine housing. A compressor wheel 12 is arranged in the compressor housing. The turbine wheel 11 is connected to the compressor wheel 12 via a shaft 4. The shaft 4 extends along a central axis 3.
(8)
(9) The oil guide comprises a first duct 6, a second duct 7 and a third duct 8. The individual ducts 6, 7, 8 are formed as bores in the bearing housing 1.
(10) The first duct 6 leads from the outside into the bearing housing 1. The oil is supplied via the first duct 6. The first duct 6 is arranged perpendicular to the central axis 3 but runs off-center and thus eccentrically with respect to the central axis 3.
(11) The second duct 7 intersects a lower end of the first duct 6. The first duct 6 and the second duct 7 are formed at an angle α greater than 90° relative to one another. An inner end of the second duct 7 opens into the third duct 8. Via said third duct 8, the oil is distributed to the individual bearing points 5. Said third duct 8 is situated higher than the point of intersection between the first duct 6 and the second duct 7. In this way, a part of the first duct 6 and a part of the second duct 7 form a siphon 10 within the bearing housing 1. The maximum fill level of said siphon 10 is denoted by the line 13 in
(12) An outer end of the second duct 7 is closed off by means of a closure plug 9 which thus forms the base of the siphon 10.
(13)
(14)
(15) In addition to the above written description of the invention, reference is hereby explicitly made, for disclosure supplementary thereto, to the diagrammatic illustration of the invention in
LIST OF REFERENCE SYMBOLS
(16) 1 Bearing housing 2 Exhaust-gas turbocharger 3 Central axis 4 Shaft 5 Bearing point 6 First duct 7 Second duct 8 Third duct 9 Closure plug 10 Siphon 11 Turbine wheel 12 Compressor wheel 13 Fill limit 14 Branch duct 15 Heating element α Angle, in particular between 100° and 170°, in particular between 110° and 160°.