JPH02118102U - - Google Patents
Info
- Publication number
- JPH02118102U JPH02118102U JP2606889U JP2606889U JPH02118102U JP H02118102 U JPH02118102 U JP H02118102U JP 2606889 U JP2606889 U JP 2606889U JP 2606889 U JP2606889 U JP 2606889U JP H02118102 U JPH02118102 U JP H02118102U
- Authority
- JP
- Japan
- Prior art keywords
- blade
- height direction
- direction position
- blades
- same
- 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 4
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2606889U JPH02118102U (cs) | 1989-03-09 | 1989-03-09 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2606889U JPH02118102U (cs) | 1989-03-09 | 1989-03-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH02118102U true JPH02118102U (cs) | 1990-09-21 |
Family
ID=31247357
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2606889U Pending JPH02118102U (cs) | 1989-03-09 | 1989-03-09 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH02118102U (cs) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2015519501A (ja) * | 2012-04-16 | 2015-07-09 | シーメンス アクティエンゲゼルシャフト | 軸流流体機械のための静翼リングおよび静翼リングの設計法 |
JP2015520321A (ja) * | 2012-06-14 | 2015-07-16 | ジエ・アヴィオ・エッセ・エッレ・エッレ | フラッタリング防止手段を備えたガスタービンのための翼列 |
-
1989
- 1989-03-09 JP JP2606889U patent/JPH02118102U/ja active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2015519501A (ja) * | 2012-04-16 | 2015-07-09 | シーメンス アクティエンゲゼルシャフト | 軸流流体機械のための静翼リングおよび静翼リングの設計法 |
US9951648B2 (en) | 2012-04-16 | 2018-04-24 | Siemens Aktiengesellschaft | Guide blade ring for an axial turbomachine and method for designing the guide blade ring |
JP2015520321A (ja) * | 2012-06-14 | 2015-07-16 | ジエ・アヴィオ・エッセ・エッレ・エッレ | フラッタリング防止手段を備えたガスタービンのための翼列 |