Turbine housing for turbocharger
US-8961122-B2 · Feb 24, 2015 · US
US9850777B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9850777-B2 |
| Application number | US-201414164800-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 27, 2014 |
| Priority date | Jan 29, 2013 |
| Publication date | Dec 26, 2017 |
| Grant date | Dec 26, 2017 |
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Official abstract text for this publication.
Embodiments of the present invention may include a turbocharger having a turbine, a turbine housing, a variable valve, a first plate, a second plate and a heat shield member. The turbine housing accommodates the turbine and has a flow path. The variable valve rotates about each pivot member provided thereon, thereby adjusting the flow velocity of fluid guided from the flow path to the turbine. The first plate supports one end of each pivot member, and defines the flow path. The second plate supports the other end of each pivot member or the variable valves, and defines the flow path. The heat shield member covers a wall surface of the turbine housing, and defines the flow path.
Opening claim text (preview).
This invention claims: 1. A turbocharger comprising: a turbine configured to be rotated by using energy caused by a fluid flowing into the turbocharger; a turbine housing configured to accommodate the turbine, the turbine housing having a flow path for guiding the fluid to the turbine; a plurality of variable valves configured to rotate about each pivot member provided thereon, thereby adjusting flow velocity of the fluid guided from the flow path to the turbine; a first plate configured to support a first end of each pivot member of the variable valves; a second plate arranged so that the variable valves are between the second plate and the first plate, the first plate and the second plate being configured to define the flow path; a heat shield member configured to cover a wall surface of the turbine housing, wherein a gap is formed between the wall surface and the heat shield member, the heat shield member being configured to define the flow path, wherein the flow path is configured such that the fluid flowing into the turbocharger is guided between the first plate, the second plate, and the heat shield member, and to the turbine; a rotation shaft of the turbine; a bearing configured to rotatably support the rotation shaft; and a bearing housing configured to accommodate the rotation shaft and the bearing, the bearing housing being connected to the turbine housing, wherein the hearing housing is closer to the first plate than the second plate, and the second plate contacts with an inner wall of the turbine housing, and the heat shield member comprises a first end portion and a second end portion, wherein the first end portion is held between the turbine housing and the bearing housing or the second end portion is held between the turbine housing and the second plate. 2. The turbocharger of claim 1 , wherein the first end portion of the heat shield member is held between the turbine housing and the bearing housing, and the second end portion of the heat shield member is held between the turbine housing and the second plate. 3. The turbocharger of claim 1 , wherein the turbine housing comprises a discharge port to which the fluid is guided after rotating the turbine. 4. The turbocharger of claim 3 further comprising a discharge port heat shield member configured to cover at least a part of an inner wall of the discharge port. 5. The turbocharger of claim 4 , wherein the discharge port heat shield member is of a tubular configuration. 6. The turbocharger of claim 3 further comprising a connection pipe connected to the discharge port, wherein the connection pipe comprises a discharge port heat shield member accommodated in the discharge port so that the discharge port heat shield member covers at least a part of an inner wall of the discharge port. 7. The turbocharger of claim 6 , wherein the discharge port heat shield member is of a tubular configuration.
Casings modified therefor (double casings F01D25/26) · CPC title
for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line (F01D17/167 takes precedence) · CPC title
by means of valves, e.g. for steam turbines (valves in general F16K) · CPC title
Thermally insulated casings · CPC title
in turbochargers · CPC title
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