JPS648505U - - Google Patents
Info
- Publication number
- JPS648505U JPS648505U JP10264187U JP10264187U JPS648505U JP S648505 U JPS648505 U JP S648505U JP 10264187 U JP10264187 U JP 10264187U JP 10264187 U JP10264187 U JP 10264187U JP S648505 U JPS648505 U JP S648505U
- Authority
- JP
- Japan
- Prior art keywords
- trailing edge
- blade
- cooling
- cooling air
- gas 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
- 238000001816 cooling Methods 0.000 claims description 11
- 238000007664 blowing Methods 0.000 description 1
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10264187U JPS648505U (it) | 1987-07-06 | 1987-07-06 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10264187U JPS648505U (it) | 1987-07-06 | 1987-07-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS648505U true JPS648505U (it) | 1989-01-18 |
Family
ID=31332734
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10264187U Pending JPS648505U (it) | 1987-07-06 | 1987-07-06 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS648505U (it) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005049970A1 (ja) * | 2003-11-21 | 2005-06-02 | Mitsubishi Heavy Industries, Ltd. | ガスタービンエンジンのタービン冷却翼 |
-
1987
- 1987-07-06 JP JP10264187U patent/JPS648505U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005049970A1 (ja) * | 2003-11-21 | 2005-06-02 | Mitsubishi Heavy Industries, Ltd. | ガスタービンエンジンのタービン冷却翼 |
| US7300251B2 (en) | 2003-11-21 | 2007-11-27 | Mitsubishi Heavy Industries, Ltd. | Turbine cooling vane of gas turbine engine |