JPS61147303U - - Google Patents
Info
- Publication number
- JPS61147303U JPS61147303U JP3027585U JP3027585U JPS61147303U JP S61147303 U JPS61147303 U JP S61147303U JP 3027585 U JP3027585 U JP 3027585U JP 3027585 U JP3027585 U JP 3027585U JP S61147303 U JPS61147303 U JP S61147303U
- Authority
- JP
- Japan
- Prior art keywords
- rotor blades
- gas turbine
- rotating shaft
- attached
- stator blade
- 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
- 238000007789 sealing Methods 0.000 claims description 3
Description
第１図は本考案の一実施例に係るガスタービン
装置の要部を表す縦断面図、第２図は従来のガス
タービン装置の要部を表す縦断面図である。
図面中、１は動翼、２は回転軸、３は静翼、４
はケーシング、６はシール部材、１０は支持部材
である。
FIG. 1 is a longitudinal cross-sectional view showing the main parts of a gas turbine apparatus according to an embodiment of the present invention, and FIG. 2 is a longitudinal cross-sectional view showing the main parts of a conventional gas turbine apparatus. In the drawing, 1 is a rotor blade, 2 is a rotating shaft, 3 is a stationary blade, 4
1 is a casing, 6 is a sealing member, and 10 is a supporting member.
Claims (1)
を収容したケーシングに取付けられると共に該動
翼の各段列間に配設された静翼とを備えたガスタ
ービン装置において、前記静翼の先端と前記回転
軸の周面との間をシールするシール部材を該静翼
内を貫通する支持部材を介して前記ケーシングに
取付けたことを特徴とするガスタービン装置。 A gas turbine apparatus comprising rotor blades arranged in multiple rows on a rotating shaft, and stationary blades attached to a casing housing the rotor blades and arranged between each row of the rotor blades, A gas turbine device, characterized in that a sealing member for sealing between a tip of a stator blade and a circumferential surface of the rotating shaft is attached to the casing via a support member passing through the inside of the stator blade.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3027585U JPS61147303U (en) | 1985-03-05 | 1985-03-05 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3027585U JPS61147303U (en) | 1985-03-05 | 1985-03-05 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS61147303U true JPS61147303U (en) | 1986-09-11 |
Family
ID=30529830
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3027585U Pending JPS61147303U (en) | 1985-03-05 | 1985-03-05 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61147303U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004332737A (en) * | 2003-05-06 | 2004-11-25 | General Electric Co <Ge> | Method and device for controlling rotor blade tip clearance in gas turbine engine |
-
1985
- 1985-03-05 JP JP3027585U patent/JPS61147303U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004332737A (en) * | 2003-05-06 | 2004-11-25 | General Electric Co <Ge> | Method and device for controlling rotor blade tip clearance in gas turbine engine |