JPS62176448U - - Google Patents
Info
- Publication number
- JPS62176448U JPS62176448U JP6426686U JP6426686U JPS62176448U JP S62176448 U JPS62176448 U JP S62176448U JP 6426686 U JP6426686 U JP 6426686U JP 6426686 U JP6426686 U JP 6426686U JP S62176448 U JPS62176448 U JP S62176448U
- Authority
- JP
- Japan
- Prior art keywords
- groove
- gas turbine
- collar
- fitted
- shaped
- 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
- 230000007704 transition Effects 0.000 claims 1
- 238000001816 cooling Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6426686U JPS62176448U (zh) | 1986-04-30 | 1986-04-30 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6426686U JPS62176448U (zh) | 1986-04-30 | 1986-04-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62176448U true JPS62176448U (zh) | 1987-11-09 |
Family
ID=30900269
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6426686U Pending JPS62176448U (zh) | 1986-04-30 | 1986-04-30 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62176448U (zh) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013164071A (ja) * | 2012-02-13 | 2013-08-22 | General Electric Co <Ge> | ターボ機械のための連絡管シールアセンブリ |
| US9097119B2 (en) | 2010-05-05 | 2015-08-04 | Alstom Technology Ltd. | Transitional region for a secondary combustion chamber of a gas turbine |
-
1986
- 1986-04-30 JP JP6426686U patent/JPS62176448U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9097119B2 (en) | 2010-05-05 | 2015-08-04 | Alstom Technology Ltd. | Transitional region for a secondary combustion chamber of a gas turbine |
| JP2013164071A (ja) * | 2012-02-13 | 2013-08-22 | General Electric Co <Ge> | ターボ機械のための連絡管シールアセンブリ |