JPS6165201U - - Google Patents

Info

Publication number
JPS6165201U
JPS6165201U JP14928384U JP14928384U JPS6165201U JP S6165201 U JPS6165201 U JP S6165201U JP 14928384 U JP14928384 U JP 14928384U JP 14928384 U JP14928384 U JP 14928384U JP S6165201 U JPS6165201 U JP S6165201U
Authority
JP
Japan
Prior art keywords
stopper
turbine wheel
turbine
rotor blade
notch
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
JP14928384U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP14928384U priority Critical patent/JPS6165201U/ja
Publication of JPS6165201U publication Critical patent/JPS6165201U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案のタービン翼車の部分斜視図、
第2図は本考案の他の実施例における止め金の斜
視図、第3図は蒸気タービンの蒸気通路部を示す
断面図、第4図は従来のタービン翼車における動
翼の取付け作業説明図、第5図は従来のタービン
翼車の正面部分図である。 5…動翼、7…タービンロータ円板、8…ダブ
テール、10…切り欠き部、12…止め金、14
…止め金のソリツド部、16…放射方向の溝、1
7…板状部材、18…溝。
FIG. 1 is a partial perspective view of the turbine wheel of the present invention.
Fig. 2 is a perspective view of a stopper in another embodiment of the present invention, Fig. 3 is a sectional view showing the steam passage section of a steam turbine, and Fig. 4 is an explanatory diagram of the installation work of rotor blades in a conventional turbine wheel. , FIG. 5 is a partial front view of a conventional turbine wheel. 5... Moving blade, 7... Turbine rotor disk, 8... Dovetail, 10... Notch, 12... Stopper, 14
...Solid part of clasp, 16...Radial groove, 1
7...Plate member, 18...Groove.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] タービンロータ円板の動翼挿入用切り欠き部に
止め金を係止するようにしたタービン翼車におい
て、上記止め金のソリツド部における動翼との隣
接面に放射方向の溝を設けたことを特徴とする、
タービン翼車。
In a turbine wheel in which a stopper is secured to a notch for inserting a rotor blade in a turbine rotor disk, radial grooves are provided in the solid portion of the stopper on the surface adjacent to the rotor blade. Characterized by
Turbine wheel.
JP14928384U 1984-10-02 1984-10-02 Pending JPS6165201U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14928384U JPS6165201U (en) 1984-10-02 1984-10-02

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14928384U JPS6165201U (en) 1984-10-02 1984-10-02

Publications (1)

Publication Number Publication Date
JPS6165201U true JPS6165201U (en) 1986-05-02

Family

ID=30707469

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14928384U Pending JPS6165201U (en) 1984-10-02 1984-10-02

Country Status (1)

Country Link
JP (1) JPS6165201U (en)

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