JPS6279938U - - Google Patents
Info
- Publication number
- JPS6279938U JPS6279938U JP17098285U JP17098285U JPS6279938U JP S6279938 U JPS6279938 U JP S6279938U JP 17098285 U JP17098285 U JP 17098285U JP 17098285 U JP17098285 U JP 17098285U JP S6279938 U JPS6279938 U JP S6279938U
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- partition wall
- end surface
- nozzle blade
- variable capacity
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000005192 partition Methods 0.000 claims description 5
- 230000002093 peripheral effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
Description
第１図は本考案の一実施例を示す可変容量ラジ
アルタービンの部分断面図、第２図はその一部拡
大図、第３図は従来例の部分断面図、第４図はそ
の一部拡大図である。
１０……タービン翼車、１１……回転軸、２０
……軸受台、２１……断熱板、３０……タービン
車室、３１……第１導入路、３２……第２導入路
、３３……仕切壁、４０……ノズル翼、４１……
ノズル支持板、３３１……仕切壁ノズル端面、４
０１……ノズル翼端面。
Fig. 1 is a partial sectional view of a variable capacity radial turbine showing an embodiment of the present invention, Fig. 2 is a partially enlarged view, Fig. 3 is a partial sectional view of a conventional example, and Fig. 4 is a partially enlarged view. It is a diagram. 10... Turbine impeller, 11... Rotating shaft, 20
... Bearing stand, 21 ... Heat insulation plate, 30 ... Turbine casing, 31 ... First introduction path, 32 ... Second introduction path, 33 ... Partition wall, 40 ... Nozzle blade, 41 ...
Nozzle support plate, 331...Partition wall nozzle end surface, 4
01... Nozzle blade end surface.
Claims (1)
、かつ、一方の導入路の内側にノズル翼を配置し
た可変容量あるいは混流を可能としたラジアルタ
ービンであつて、ノズル翼の一端をノズル支持板
と一体とし、他端を開放形としてノズル翼端面を
形成し、該ノズル翼端面と上記仕切壁の内周側側
壁の一部に設けた仕切壁ノズル端面とをタービン
翼車の回転軸とほぼ直角な二つの平面にて対面す
るごとくした可変容量ラジアルタービン。 A radial turbine that enables variable capacity or mixed flow, with two introduction passages separated by a partition wall and a nozzle blade placed inside one of the introduction passages, with one end of the nozzle blade supported by the nozzle. A nozzle blade end surface is formed integrally with the plate and the other end is open, and the nozzle blade end surface and a partition wall nozzle end surface provided on a part of the inner peripheral side wall of the partition wall are connected to the rotation axis of the turbine wheel. A variable capacity radial turbine with two nearly perpendicular planes facing each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17098285U JPS6279938U (en) | 1985-11-08 | 1985-11-08 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17098285U JPS6279938U (en) | 1985-11-08 | 1985-11-08 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6279938U true JPS6279938U (en) | 1987-05-22 |
Family
ID=31106196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP17098285U Pending JPS6279938U (en) | 1985-11-08 | 1985-11-08 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6279938U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2123861A2 (en) | 2008-05-20 | 2009-11-25 | Mitsubishi Heavy Industries, Ltd. | Mixed flow turbine for a turbocharger |
| JP2012102745A (en) * | 2012-01-23 | 2012-05-31 | Mitsubishi Heavy Ind Ltd | Diagonal flow turbine |
| WO2012132523A1 (en) * | 2011-03-31 | 2012-10-04 | 三菱重工業株式会社 | Turbocharger |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59101505A (en) * | 1982-12-01 | 1984-06-12 | Mitsubishi Heavy Ind Ltd | Double flow radial turbine |
| JPS60212623A (en) * | 1984-04-09 | 1985-10-24 | Hitachi Ltd | Exhaust turbo-supercharger |
-
1985
- 1985-11-08 JP JP17098285U patent/JPS6279938U/ja active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59101505A (en) * | 1982-12-01 | 1984-06-12 | Mitsubishi Heavy Ind Ltd | Double flow radial turbine |
| JPS60212623A (en) * | 1984-04-09 | 1985-10-24 | Hitachi Ltd | Exhaust turbo-supercharger |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2123861A2 (en) | 2008-05-20 | 2009-11-25 | Mitsubishi Heavy Industries, Ltd. | Mixed flow turbine for a turbocharger |
| WO2012132523A1 (en) * | 2011-03-31 | 2012-10-04 | 三菱重工業株式会社 | Turbocharger |
| JP2012215129A (en) * | 2011-03-31 | 2012-11-08 | Mitsubishi Heavy Ind Ltd | Turbocharger |
| KR101529411B1 (en) * | 2011-03-31 | 2015-06-16 | 미츠비시 쥬고교 가부시키가이샤 | Turbocharger |
| JP2012102745A (en) * | 2012-01-23 | 2012-05-31 | Mitsubishi Heavy Ind Ltd | Diagonal flow turbine |