Bearing chamber with mapped thermal heat exchange fins
US-2024151155-A1 · May 9, 2024 · US
US8926274B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8926274-B2 |
| Application number | US-99937009-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 26, 2009 |
| Priority date | Jul 2, 2008 |
| Publication date | Jan 6, 2015 |
| Grant date | Jan 6, 2015 |
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Official abstract text for this publication.
The invention relates to a bearing housing body group ( 1 ) of an exhaust-gas turbocharger, having a housing ( 2 ) for a bearing arrangement of a rotor shaft ( 3 ); having a turbine wheel ( 4 ) on one end ( 5 ) of the rotor shaft ( 3 ); having a compressor wheel ( 6 ) on the opposite end ( 7 ) of the rotor shaft ( 3 ); and having a compressor-wheel-side housing cover ( 8 ) which can be fixed by means of a fastening device ( 9 ) in a compressor-wheel-side housing opening ( 10 ), wherein the fastening device ( 9 ) is designed as a bayonet connection.
Opening claim text (preview).
The invention claimed is: 1. A bearing housing body group ( 1 ) of an exhaust-gas turbocharger comprising: a housing ( 2 ) for a bearing arrangement of a rotor shaft ( 3 ); a turbine wheel ( 4 ) on one end ( 5 ) of the rotor shaft ( 3 ); a compressor wheel ( 6 ) on an opposite end ( 7 ) of the rotor shaft ( 3 ); and a compressor-wheel-side housing cover ( 8 ) fixed by means of a fastening device ( 9 ) in a compressor-wheel-side housing opening ( 10 ), wherein the compressor-wheel-side housing cover ( 8 ) is located substantially entirely within the housing ( 2 ), wherein the compressor-wheel-side housing cover ( 8 ) is substantially flush with an axially outermost face of the housing ( 2 ), and wherein the fastening device ( 9 ) is a bayonet connection. 2. The bearing housing body group according to claim 1 , wherein the bayonet connection ( 9 ) has a web arrangement ( 11 ) on the housing cover ( 8 ) and a groove arrangement ( 12 ) in the housing opening ( 10 ). 3. The bearing housing body group according to claim 2 , wherein the web arrangement ( 11 ) has three webs which are arranged uniformly on the periphery of a web ring ( 21 ) of the housing cover ( 8 ) and which can be inserted into an annular groove arrangement ( 12 ) of the housing opening ( 10 ). 4. The bearing housing body group according to claim 3 , wherein the annular groove arrangement ( 12 ) includes three insertion recesses ( 13 , 14 ). 5. The bearing housing body group according to claim 1 , wherein the housing cover ( 8 ) has a holding groove ( 15 , 16 ) for holding an O-ring ( 17 ). 6. The bearing housing body group according to claim 5 , wherein the holding groove ( 15 ) is formed so as to be open at one of its two end sides. 7. The bearing housing body group according to claim 5 , wherein the holding groove ( 16 ) is formed so as to be closed at both end sides. 8. A bearing housing body group ( 1 ) of an exhaust-gas turbocharger comprising: a housing ( 2 ) for a bearing arrangement of a rotor shaft ( 3 ); a turbine wheel ( 4 ) on one end ( 5 ) of the rotor shaft ( 3 ); a compressor wheel ( 6 ) on an opposite end ( 7 ) of the rotor shaft ( 3 ); and a compressor-wheel-side housing cover ( 8 ) fixed by means of a fastening device ( 9 ) in a compressor-wheel-side housing opening ( 10 ), wherein the fastening device ( 9 ) is a bayonet connection, wherein the bayonet connection ( 9 ) has a web arrangement ( 11 ) on the housing cover ( 8 ) and an annular groove arrangement ( 12 ) in the housing opening ( 10 ), wherein the annular groove arrangement ( 12 ) includes part ring grooves ( 24 ), wherein an end of each part ring groove ( 24 ) includes a recess ( 25 ) having a contact surface ( 26 ) and a latching edge ( 27 ). 9. A bearing housing body group ( 1 ) of an exhaust-gas turbocharger comprising: a housing ( 2 ) for a bearing arrangement of a rotor shaft ( 3 ); a turbine wheel ( 4 ) on one end ( 5 ) of the rotor shaft ( 3 ); a compressor wheel ( 6 ) on an opposite end ( 7 ) of the rotor shaft ( 3 ); and a compressor-wheel-side housing cover ( 8 ) fixed by means of a fastening device ( 9 ) in a compressor-wheel-side housing opening ( 10 ), wherein the fastening device ( 9 ) is a bayonet connection, wherein a spring plate ( 18 ) for fixing an axial bearing ( 19 ) of the rotor shaft ( 3 ) is arranged between and directly operatively engages the axial bearing ( 19 ) and the housing cover ( 8 ).
Bearing supports · CPC title
in turbochargers · CPC title
Engines characterised by provision of pumps driven at least for part of the time by exhaust · CPC title
with a bayonet coupling · CPC title
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