JPS62133902U - - Google Patents
Info
- Publication number
- JPS62133902U JPS62133902U JP2183086U JP2183086U JPS62133902U JP S62133902 U JPS62133902 U JP S62133902U JP 2183086 U JP2183086 U JP 2183086U JP 2183086 U JP2183086 U JP 2183086U JP S62133902 U JPS62133902 U JP S62133902U
- Authority
- JP
- Japan
- Prior art keywords
- annular groove
- annular
- circumferential surface
- rotating shaft
- axial flow
- 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
- 239000012530 fluid Substances 0.000 claims description 2
Description
第1図は本考案に係る一実施例を示す縦断面図
、第2図は第1図の要部拡大図である。第3図は
従来例を示す縦断面図、第4図は第3図の動翼部
分の横断面図である。
1……ノズル、2……動翼、3……動翼先端か
らの漏れ流体、5……動翼シユラウド、8……溝
、9……T字型フイン。
FIG. 1 is a longitudinal sectional view showing an embodiment of the present invention, and FIG. 2 is an enlarged view of the main part of FIG. 1. FIG. 3 is a longitudinal cross-sectional view showing a conventional example, and FIG. 4 is a cross-sectional view of the rotor blade portion of FIG. 3. 1... Nozzle, 2... Moving blade, 3... Leakage fluid from the tip of moving blade, 5... Moving blade shroud, 8... Groove, 9... T-shaped fin.
Claims (1)
転軸に固定された動翼を複数個配置し、上記ノズ
ルを通して上記動翼に作動流体を供給して上記回
転軸を回転させる軸流ターボ機械において、上記
動翼の先端に取付けられたシユラウドの外周面に
上記回転軸を同軸心とした環状溝を刻設すると共
に、上記シユラウドの環状溝が対向する上記ケー
シングの内周面に一端が固着され、かつ他端が上
記環状溝に微小な間隙を有して挿入される円環状
フインを突設したことを特徴とする軸流ターボ機
械。 In an axial flow turbomachine, a plurality of rotor blades fixed to a rotating shaft are arranged opposite to a nozzle integrated in a casing, and a working fluid is supplied to the rotor blades through the nozzles to rotate the rotary shaft. An annular groove coaxial with the rotating shaft is carved on the outer circumferential surface of the shroud attached to the tip of the rotor blade, and one end is fixed to the inner circumferential surface of the casing facing the annular groove of the shroud. An axial flow turbomachine characterized in that an annular fin is protruded from the annular groove, and the other end of the annular fin is inserted into the annular groove with a small gap therebetween.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2183086U JPS62133902U (en) | 1986-02-18 | 1986-02-18 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2183086U JPS62133902U (en) | 1986-02-18 | 1986-02-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS62133902U true JPS62133902U (en) | 1987-08-24 |
Family
ID=30818636
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2183086U Pending JPS62133902U (en) | 1986-02-18 | 1986-02-18 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS62133902U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2017106375A (en) * | 2015-12-09 | 2017-06-15 | 三菱日立パワーシステムズ株式会社 | Seal structure, turbomachine and manufacturing method of seal fin |
-
1986
- 1986-02-18 JP JP2183086U patent/JPS62133902U/ja active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2017106375A (en) * | 2015-12-09 | 2017-06-15 | 三菱日立パワーシステムズ株式会社 | Seal structure, turbomachine and manufacturing method of seal fin |
WO2017098959A1 (en) * | 2015-12-09 | 2017-06-15 | 三菱日立パワーシステムズ株式会社 | Seal fin, seal structure, turbomachine, and method for producing seal fin |
CN108291451A (en) * | 2015-12-09 | 2018-07-17 | 三菱日立电力系统株式会社 | Seal fin, sealing structure, turbomachinery and the manufacturing method for sealing fin |
CN108291451B (en) * | 2015-12-09 | 2020-04-10 | 三菱日立电力系统株式会社 | Sealing fin, sealing structure, turbo machine, and method for manufacturing sealing fin |
US11105213B2 (en) | 2015-12-09 | 2021-08-31 | Mitsubishi Power, Ltd. | Seal fin, seal structure, turbo machine, and method for manufacturing seal fin |