JPS5997207U - Turbine blade fixing device - Google Patents
Turbine blade fixing deviceInfo
- Publication number
- JPS5997207U JPS5997207U JP19290482U JP19290482U JPS5997207U JP S5997207 U JPS5997207 U JP S5997207U JP 19290482 U JP19290482 U JP 19290482U JP 19290482 U JP19290482 U JP 19290482U JP S5997207 U JPS5997207 U JP S5997207U
- Authority
- JP
- Japan
- Prior art keywords
- blades
- rotor
- fixing device
- turbine blade
- blade fixing
- 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
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第1図、および第2図は従来の羽根植込状態の説明図、
第3図は従来技術の不具合の一部を示す説明図、第4図
は本考案の一実施例を示す説明図、第5図は第4図のV
−V線に沿うところの断面図である。
1・・・植込部、2・・・ロータディスク、3・・・溝
部、4・・・羽根、6・・・シュラウド板、7・・・突
起部、訃・・ 。
結合片、9・・・ボルト、10・・・切欠き部、11・
・・テーパ面。
t −
−第4図 ・ 4、
と
第3図 −−′−
−l/−−−Figures 1 and 2 are explanatory diagrams of the conventional blade implanted state;
FIG. 3 is an explanatory diagram showing some of the defects in the prior art, FIG. 4 is an explanatory diagram showing an embodiment of the present invention, and FIG.
It is a sectional view taken along line -V. DESCRIPTION OF SYMBOLS 1... Implant part, 2... Rotor disk, 3... Groove part, 4... Vane, 6... Shroud plate, 7... Projection part, butt... Connecting piece, 9... Bolt, 10... Notch, 11.
...Tapered surface. t - -Figure 4 4, and Figure 3 --'- -l/---
Claims (1)
置にロタディスクの両側面に開口した切欠き部を設ける
11.一方、羽根の植込部には植込部底面両縁端に向け
て一定の角度で傾斜しているテーパ面を形成し、さらに
これらの羽根とロータディスクとは羽根の植込部をロー
タディスクの溝部に嵌合して一体化すると共に、前記切
欠き部のそれぞれに前記羽根テーパ面にそのi端を当接
することにより一羽根全体をロータディス々の半径方向
に移動せしめる−−対の結合片を締結部材を芥して嵌着
したことを特徴とするタービン羽根固定装置。10-Provide a notch that opens on both sides of the rota disc at a position facing downward from the groove of the rotor disc.11. On the other hand, the implanted part of the blade has a tapered surface that is inclined at a constant angle toward both edges of the bottom of the implanted part, and these blades and the rotor disk are connected to each other. A pair of connecting pieces are fitted into the grooves of the rotor discs to be integrated, and the i-ends of the blades are brought into contact with the tapered surfaces of the blades in each of the notches, thereby moving the entire blade in the radial direction of the rotor disks. A turbine blade fixing device characterized in that a fastening member is removed and fitted.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19290482U JPS5997207U (en) | 1982-12-22 | 1982-12-22 | Turbine blade fixing device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19290482U JPS5997207U (en) | 1982-12-22 | 1982-12-22 | Turbine blade fixing device |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5997207U true JPS5997207U (en) | 1984-07-02 |
Family
ID=30415019
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP19290482U Pending JPS5997207U (en) | 1982-12-22 | 1982-12-22 | Turbine blade fixing device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5997207U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010501765A (en) * | 2006-08-25 | 2010-01-21 | シーメンス アクチエンゲゼルシヤフト | Turbine blade fixing device |
WO2013058220A1 (en) * | 2011-10-20 | 2013-04-25 | 三菱重工業株式会社 | Rotor blade support structure |
-
1982
- 1982-12-22 JP JP19290482U patent/JPS5997207U/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010501765A (en) * | 2006-08-25 | 2010-01-21 | シーメンス アクチエンゲゼルシヤフト | Turbine blade fixing device |
WO2013058220A1 (en) * | 2011-10-20 | 2013-04-25 | 三菱重工業株式会社 | Rotor blade support structure |
JP2013087714A (en) * | 2011-10-20 | 2013-05-13 | Mitsubishi Heavy Ind Ltd | Rotor blade support structure |
US9677406B2 (en) | 2011-10-20 | 2017-06-13 | Mitsubishi Hitachi Power Systems, Ltd. | Rotor blade support structure |
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