JPS58165202U - turbine stationary blade - Google Patents
turbine stationary bladeInfo
- Publication number
- JPS58165202U JPS58165202U JP6309582U JP6309582U JPS58165202U JP S58165202 U JPS58165202 U JP S58165202U JP 6309582 U JP6309582 U JP 6309582U JP 6309582 U JP6309582 U JP 6309582U JP S58165202 U JPS58165202 U JP S58165202U
- Authority
- JP
- Japan
- Prior art keywords
- turbine stationary
- stationary blade
- rear end
- divided
- turbine
- 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
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図はガスタービンのロータ部近傍断面図、第２図は
従来例の静翼配置図、第３図はその分割部静翼の平面図
、第４図は本考案の一実施例の静翼配置図、第５図はそ
の分割静翼の平面図である。Fig. 1 is a cross-sectional view of the rotor of a gas turbine, Fig. 2 is a stator vane arrangement of a conventional example, Fig. 3 is a plan view of the divided stator blade, and Fig. 4 is a stator vane of an embodiment of the present invention. FIG. 5 is a plan view of the divided stator blade.
Claims (1)
伴って分割される上記静翼を、その後端部近傍で分割す
ると共にその分割後端部を除去したことを特徴とするタ
ービン静翼。The stator vane, which is divided into upper and lower halves of the vehicle compartment in which a plurality of stator vanes are planted on the inner circumferential surface, is divided near its rear end, and the rear end of the division is removed. Turbine stationary blades.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6309582U JPS58165202U (en) | 1982-04-28 | 1982-04-28 | turbine stationary blade |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6309582U JPS58165202U (en) | 1982-04-28 | 1982-04-28 | turbine stationary blade |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS58165202U true JPS58165202U (en) | 1983-11-02 |
Family
ID=30073214
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6309582U Pending JPS58165202U (en) | 1982-04-28 | 1982-04-28 | turbine stationary blade |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58165202U (en) |
-
1982
- 1982-04-28 JP JP6309582U patent/JPS58165202U/en active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS583997U (en) | Aeration device | |
| JPS58165203U (en) | turbine stator blade | |
| JPS5870497U (en) | Cooling fan for internal combustion engine | |
| JPS5921001U (en) | steam turbine blade shroud | |
| JPS58114900U (en) | spiral pump | |
| JPS59135305U (en) | Steam turbine rotor blade shroud ring | |
| JPS5975501U (en) | Moving blade fixing device | |
| JPS601998U (en) | centrifugal fan impeller | |
| JPS5892873U (en) | Radial fan of rotating electric machine | |
| JPS58142302U (en) | axial flow turbomachinery | |
| JPS59144198U (en) | Centrifugal blower airfoil impeller | |
| JPS58113804U (en) | Multi-stage steam turbine with uncontrolled extraction | |
| JPS59168501U (en) | Gas turbine stator blade segment | |
| JPS58156117U (en) | automotive cooling fan | |
| JPS6098703U (en) | labyrinth device | |
| JPS6139402U (en) | Turbo gear wheel turbine wheel structure | |
| JPS6098702U (en) | turbine moving blade | |
| JPS60158000U (en) | ceiling fan | |
| JPS58124601U (en) | Axial flow turbomachinery blade cover | |
| JPS5975502U (en) | Moving blade fixing device | |
| JPS59131903U (en) | axial flow turbine | |
| JPS595798U (en) | impeller | |
| JPS6063183U (en) | washing machine rotor blade | |
| JPS6125503U (en) | Gas turbine with ceramic rotor blades | |
| JPS59107902U (en) | Gas turbine stator blade mounting structure |