JPS5996301U - Connection structure of turbine rotor blades - Google Patents

Connection structure of turbine rotor blades

Info

Publication number
JPS5996301U
JPS5996301U JP19218782U JP19218782U JPS5996301U JP S5996301 U JPS5996301 U JP S5996301U JP 19218782 U JP19218782 U JP 19218782U JP 19218782 U JP19218782 U JP 19218782U JP S5996301 U JPS5996301 U JP S5996301U
Authority
JP
Japan
Prior art keywords
connection structure
turbine rotor
rotor blades
length
wire
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
Application number
JP19218782U
Other languages
Japanese (ja)
Inventor
松浦 俊博
Original Assignee
株式会社東芝
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 株式会社東芝 filed Critical 株式会社東芝
Priority to JP19218782U priority Critical patent/JPS5996301U/en
Publication of JPS5996301U publication Critical patent/JPS5996301U/en
Pending legal-status Critical Current

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

【図面の簡単な説明】[Brief explanation of drawings]

第1図はタービン動翼のルーズタイワイヤ構造を示す斜
視図、第2図は第1図の■−■線に沿った断面図、第、
3図は第2図の■−■線に沿った断面図、第4図は従来
の真円形状のワイヤ穴の場合の応力分布を示した図、第
5図は本考案に依るタービン動翼の連結構造の一実施例
を示すもので、  ・第3図に示す従来の連結構造に対
応する図、第6図は本考案に依るタービン動翼の連結構
造に用いられるワイヤ穴の場合の第4図に対応する図、
第7図は本考案に係るもので、ワイヤ穴にタイワイヤを
挿通した状態を示す斜視図、第8図は本考案の他の実施
例に係るもので、ワイヤ穴形状の変形例を示した図であ
る。     。 1・・・動翼、2・・・タイワイヤ、3・・・ワイヤ穴
、4・・・接触部、5・・・隙間、a・・・長軸の長さ
、b・・・短軸の長さ。
Fig. 1 is a perspective view showing the loose tie wire structure of the turbine rotor blade, Fig. 2 is a sectional view taken along the line ■-■ in Fig. 1,
Figure 3 is a cross-sectional view taken along the line ■-■ in Figure 2, Figure 4 is a diagram showing the stress distribution in the case of a conventional perfectly circular wire hole, and Figure 5 is a turbine rotor blade according to the present invention. This figure shows an example of a connection structure, as shown in FIG. 3, which corresponds to the conventional connection structure, and FIG. A diagram corresponding to Figure 4,
Fig. 7 is a perspective view of the present invention, showing a state in which a tie wire is inserted into a wire hole, and Fig. 8 is a perspective view of another embodiment of the present invention, showing a modified example of the shape of the wire hole. It is. . DESCRIPTION OF SYMBOLS 1... Moving blade, 2... Tie wire, 3... Wire hole, 4... Contact part, 5... Gap, a... Length of major axis, b... Short axis length.

Claims (1)

【実用新案登録請求の範囲】 1 隣接する動翼を連結するために動翼に形成されるタ
イワイヤ挿通用のワイヤ穴が楕円あるいは長円形状を有
することを特徴とするタービン動翼の連結構造。 2 ワイヤ穴はその長軸が翼の長さ方向に一致するよう
に動翼に形成される、実用新案登録請求゛の範囲第1項
記載のタービン動翼の連結構造。 3 ワイヤ穴の短軸の長さがワイヤの直径の約1゜05
倍であり、長軸の長さが短軸の長さの1.2〜1.4倍
であることを特徴とする、実用新案登録請求の範囲第1
項または第2項記載のタービン動翼の連結構造。
[Claims for Utility Model Registration] 1. A connection structure for turbine rotor blades, characterized in that a wire hole for passing a tie wire formed in a rotor blade for connecting adjacent rotor blades has an elliptical or oval shape. 2. The turbine rotor blade connection structure according to claim 1, wherein the wire hole is formed in the rotor blade so that its long axis coincides with the length direction of the blade. 3 The length of the short axis of the wire hole is approximately 1°05 of the diameter of the wire.
Utility model registration claim 1, characterized in that the length of the major axis is 1.2 to 1.4 times the length of the minor axis.
A connection structure for turbine rotor blades according to item 1 or 2.
JP19218782U 1982-12-21 1982-12-21 Connection structure of turbine rotor blades Pending JPS5996301U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19218782U JPS5996301U (en) 1982-12-21 1982-12-21 Connection structure of turbine rotor blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19218782U JPS5996301U (en) 1982-12-21 1982-12-21 Connection structure of turbine rotor blades

Publications (1)

Publication Number Publication Date
JPS5996301U true JPS5996301U (en) 1984-06-29

Family

ID=30413665

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19218782U Pending JPS5996301U (en) 1982-12-21 1982-12-21 Connection structure of turbine rotor blades

Country Status (1)

Country Link
JP (1) JPS5996301U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019057655A1 (en) * 2017-09-20 2019-03-28 Sulzer Turbo Services Venlo B.V. Assembly of vane units

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019057655A1 (en) * 2017-09-20 2019-03-28 Sulzer Turbo Services Venlo B.V. Assembly of vane units
US11428106B2 (en) 2017-09-20 2022-08-30 Sulzer Management Ag Assembly of vane units

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