JPS6117101U - Turbine wheel blade structure - Google Patents
Turbine wheel blade structureInfo
- Publication number
- JPS6117101U JPS6117101U JP10007684U JP10007684U JPS6117101U JP S6117101 U JPS6117101 U JP S6117101U JP 10007684 U JP10007684 U JP 10007684U JP 10007684 U JP10007684 U JP 10007684U JP S6117101 U JPS6117101 U JP S6117101U
- Authority
- JP
- Japan
- Prior art keywords
- turbine wheel
- straight line
- root portion
- blade structure
- blade
- 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
Landscapes
- Supercharger (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は排気ターボチャージャの一部の側面断面図、第
２図は第１図の■一■線に沿ってみた断面図、第３図は
第１図および第２図の■一■線に沿ってみた断面図であ
る。
２・・・タービン翼車、３・・・翼、７・・・高圧作用
面、訃・・低圧作用面。Figure 1 is a side cross-sectional view of a part of the exhaust turbocharger, Figure 2 is a cross-sectional view taken along line 1 and 1 in Figure 1, and Figure 3 is line 1 and 2 in Figures 1 and 2. FIG. 2...Turbine impeller, 3...Blade, 7...High pressure working surface, butt...Low pressure working surface.
Claims (1)
をなす断面内において回転軸線を通る直線に沿って半径
方向外方に延びており、該翼の厚みが根元部から半径方
向外方に向けて徐々に薄くなるタービン翼車において、
上記根元部における翼の高圧作用面から上記直線に至る
肉厚を根元部における翼の抵圧作用面から上記直線に至
る肉厚よりも大きくしたタービン翼車の翼構造。The blades of the turbine wheel extend radially outward along a straight line passing through the rotational axis in a cross section perpendicular to the rotational axis of the turbine wheel, and the blades have a thickness extending radially outward from the root portion. In a turbine wheel that gradually becomes thinner toward
A blade structure of a turbine wheel, wherein the wall thickness from the high pressure acting surface of the blade at the root portion to the straight line is larger than the wall thickness from the resistance acting surface of the blade at the root portion to the straight line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10007684U JPS6117101U (en) | 1984-07-04 | 1984-07-04 | Turbine wheel blade structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10007684U JPS6117101U (en) | 1984-07-04 | 1984-07-04 | Turbine wheel blade structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6117101U true JPS6117101U (en) | 1986-01-31 |
Family
ID=30659544
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10007684U Pending JPS6117101U (en) | 1984-07-04 | 1984-07-04 | Turbine wheel blade structure |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6117101U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2016514798A (en) * | 2013-04-05 | 2016-05-23 | ボーグワーナー インコーポレーテッド | Turbine wheel of exhaust gas turbocharger |
-
1984
- 1984-07-04 JP JP10007684U patent/JPS6117101U/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2016514798A (en) * | 2013-04-05 | 2016-05-23 | ボーグワーナー インコーポレーテッド | Turbine wheel of exhaust gas turbocharger |
| US10001012B2 (en) | 2013-04-05 | 2018-06-19 | Borgwarner Inc. | Turbine wheel of an exhaust-gas turbocharger |
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