JPS62114105U - - Google Patents
Info
- Publication number
- JPS62114105U JPS62114105U JP68186U JP68186U JPS62114105U JP S62114105 U JPS62114105 U JP S62114105U JP 68186 U JP68186 U JP 68186U JP 68186 U JP68186 U JP 68186U JP S62114105 U JPS62114105 U JP S62114105U
- Authority
- JP
- Japan
- Prior art keywords
- blade
- leading edge
- wall surface
- axial flow
- airfoil
- 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
- 238000010586 diagram Methods 0.000 description 6
- 230000006866 deterioration Effects 0.000 description 1
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP68186U JPS62114105U (en:Method) | 1986-01-09 | 1986-01-09 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP68186U JPS62114105U (en:Method) | 1986-01-09 | 1986-01-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62114105U true JPS62114105U (en:Method) | 1987-07-20 |
Family
ID=30777873
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP68186U Pending JPS62114105U (en:Method) | 1986-01-09 | 1986-01-09 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62114105U (en:Method) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09184451A (ja) * | 1995-11-17 | 1997-07-15 | United Technol Corp <Utc> | ターボ機械ブレード |
| US8317466B2 (en) | 2007-01-12 | 2012-11-27 | Mitsubishi Heavy Industries, Ltd. | Blade structure of gas turbine |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5688903A (en) * | 1979-12-20 | 1981-07-18 | Toshiba Corp | Turbine nozzle blade |
| JPS5820903A (ja) * | 1981-07-29 | 1983-02-07 | Hitachi Ltd | タ−ビン静翼 |
-
1986
- 1986-01-09 JP JP68186U patent/JPS62114105U/ja active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5688903A (en) * | 1979-12-20 | 1981-07-18 | Toshiba Corp | Turbine nozzle blade |
| JPS5820903A (ja) * | 1981-07-29 | 1983-02-07 | Hitachi Ltd | タ−ビン静翼 |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09184451A (ja) * | 1995-11-17 | 1997-07-15 | United Technol Corp <Utc> | ターボ機械ブレード |
| US8317466B2 (en) | 2007-01-12 | 2012-11-27 | Mitsubishi Heavy Industries, Ltd. | Blade structure of gas turbine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4826400A (en) | Curvilinear turbine airfoil | |
| JP5300874B2 (ja) | 非軸対称プラットフォームならびに外輪上の陥没および突起を備えるブレード | |
| GB2264755A (en) | Stator blade construction | |
| GB2164098A (en) | Improvements in or relating to aerofoil section members for turbine engines | |
| CA1157779A (en) | Compression section for an axial flow rotary machine | |
| JPH10274001A (ja) | ガスタービンエンジン内の翼の冷却通路の乱流促進構造 | |
| DE60044228D1 (de) | Kompressorrotor- Konfiguration | |
| JPS61114005U (en:Method) | ||
| JP2673156B2 (ja) | ファンブレード | |
| US11236627B2 (en) | Turbomachine stator element | |
| GB2046849A (en) | Turbomachine strut | |
| JPS6133968B2 (en:Method) | ||
| CN110131043A (zh) | 发动机系统和方法 | |
| JPS62114105U (en:Method) | ||
| JPH10306702A (ja) | ガスタービン翼 | |
| CN114502843A (zh) | 包括气动翼片的可变节距定子桨叶 | |
| JPH0692723B2 (ja) | 軸流流体機械 | |
| JPH07332007A (ja) | タービン静翼 | |
| JP3626899B2 (ja) | タービン翼間の端壁構造 | |
| JP3402176B2 (ja) | ターボ機械用動翼 | |
| JPH0689651B2 (ja) | 軸流流体機械 | |
| JPH04287802A (ja) | 蒸気タービンノズル | |
| JP4090613B2 (ja) | 軸流タービン | |
| JPS6241802U (en:Method) | ||
| JP2583241Y2 (ja) | タービンノズル |