JPS637202U - - Google Patents

Info

Publication number
JPS637202U
JPS637202U JP10094386U JP10094386U JPS637202U JP S637202 U JPS637202 U JP S637202U JP 10094386 U JP10094386 U JP 10094386U JP 10094386 U JP10094386 U JP 10094386U JP S637202 U JPS637202 U JP S637202U
Authority
JP
Japan
Prior art keywords
rotor blade
protrusion
platform
showing
engage
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
JP10094386U
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 JP10094386U priority Critical patent/JPS637202U/ja
Publication of JPS637202U publication Critical patent/JPS637202U/ja
Pending legal-status Critical Current

Links

Description

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

第1図から第3図は、本考案に係わる一実施例
を示す図である。第1図は本考案に係るタービン
動翼の一実施例を示す斜視図、第2図はデイスク
に埋込んだ状態を示す第1図の―線矢視図、
第3図のa,bは他実施例を示す図である。第4
図から第6図は従来のタービン動翼を示す図で第
4図は斜視図、第5図は第4図の―線矢視図
、第6図は動翼の作用を示す説明図である。 1……ブレード、2……プラツトホーム、3…
…翼根、4……デイスク、5……突出部、6……
溝部。
FIGS. 1 to 3 are diagrams showing one embodiment of the present invention. FIG. 1 is a perspective view showing an embodiment of a turbine rotor blade according to the present invention, FIG. 2 is a view taken along the line - - of FIG. 1 showing a state embedded in a disk,
3a and 3b are views showing other embodiments. Fourth
6 to 6 are views showing conventional turbine rotor blades, FIG. 4 is a perspective view, FIG. 5 is a view taken along the line arrow - in FIG. 4, and FIG. 6 is an explanatory view showing the action of the rotor blade. . 1...Blade, 2...Platform, 3...
...wing root, 4... disk, 5... protrusion, 6...
Groove.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 隣接する動翼のプラツトホーム対向面の一面に
突出部を形成すると共に、上記対向面の他面には
上記突出部に係合する切込み部を設けたことを特
徴とする動翼。
A rotor blade characterized in that a protrusion is formed on one surface of a platform-facing surface of an adjacent rotor blade, and a notch portion is provided on the other surface of the opposing surface to engage with the protrusion.
JP10094386U 1986-07-01 1986-07-01 Pending JPS637202U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10094386U JPS637202U (en) 1986-07-01 1986-07-01

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10094386U JPS637202U (en) 1986-07-01 1986-07-01

Publications (1)

Publication Number Publication Date
JPS637202U true JPS637202U (en) 1988-01-18

Family

ID=30971231

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10094386U Pending JPS637202U (en) 1986-07-01 1986-07-01

Country Status (1)

Country Link
JP (1) JPS637202U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011106449A (en) * 2009-11-12 2011-06-02 General Electric Co <Ge> Turbine rotating blade and rotor
JP2012072750A (en) * 2010-09-30 2012-04-12 Hitachi Ltd Turbine moving blade

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011106449A (en) * 2009-11-12 2011-06-02 General Electric Co <Ge> Turbine rotating blade and rotor
JP2012072750A (en) * 2010-09-30 2012-04-12 Hitachi Ltd Turbine moving blade

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