JPS61103503U - - Google Patents
Info
- Publication number
- JPS61103503U JPS61103503U JP18805684U JP18805684U JPS61103503U JP S61103503 U JPS61103503 U JP S61103503U JP 18805684 U JP18805684 U JP 18805684U JP 18805684 U JP18805684 U JP 18805684U JP S61103503 U JPS61103503 U JP S61103503U
- Authority
- JP
- Japan
- Prior art keywords
- turbine rotor
- face
- integral covers
- blade
- gap
- 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 1
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18805684U JPS61103503U (lt) | 1984-12-13 | 1984-12-13 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18805684U JPS61103503U (lt) | 1984-12-13 | 1984-12-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS61103503U true JPS61103503U (lt) | 1986-07-01 |
Family
ID=30745527
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP18805684U Pending JPS61103503U (lt) | 1984-12-13 | 1984-12-13 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS61103503U (lt) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1999013200A1 (fr) * | 1997-09-05 | 1999-03-18 | Hitachi, Ltd. | Turbine a vapeur |
JP2017500486A (ja) * | 2013-12-18 | 2017-01-05 | サフラン エアークラフト エンジンズ | ターボマシン用インペラのためのブレードと、このブレードをモデリングする方法 |
-
1984
- 1984-12-13 JP JP18805684U patent/JPS61103503U/ja active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1999013200A1 (fr) * | 1997-09-05 | 1999-03-18 | Hitachi, Ltd. | Turbine a vapeur |
JP2017500486A (ja) * | 2013-12-18 | 2017-01-05 | サフラン エアークラフト エンジンズ | ターボマシン用インペラのためのブレードと、このブレードをモデリングする方法 |
US10626728B2 (en) | 2013-12-18 | 2020-04-21 | Safran Aircraft Engines | Blade for a turbomachine impeller and method for modelling the same |