JPS6363503U - - Google Patents

Info

Publication number
JPS6363503U
JPS6363503U JP15677286U JP15677286U JPS6363503U JP S6363503 U JPS6363503 U JP S6363503U JP 15677286 U JP15677286 U JP 15677286U JP 15677286 U JP15677286 U JP 15677286U JP S6363503 U JPS6363503 U JP S6363503U
Authority
JP
Japan
Prior art keywords
side wall
shape
root side
rotor blade
turbine
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
JP15677286U
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 JP15677286U priority Critical patent/JPS6363503U/ja
Publication of JPS6363503U publication Critical patent/JPS6363503U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案の一実施例の子午面形状図、第
2図は本考案と従来例の反動度分布の比較図、第
3図は従来例の子午面形状図、第4図は本考案の
動翼根元子午面形状の説明図、第5図は本考案の
適用による根元翼形状の変化を示す説明図である
。 1……静翼、2……動翼、4……静翼根元側壁
、4′……動翼根元側壁。
Fig. 1 is a meridional plane shape diagram of an embodiment of the present invention, Fig. 2 is a comparison diagram of the recoil degree distribution of the present invention and a conventional example, Fig. 3 is a meridional plane shape diagram of the conventional example, and Fig. 4 is a diagram of the present invention. FIG. 5 is an explanatory diagram of the meridional plane shape of the rotor blade root according to the invention. FIG. 5 is an explanatory diagram showing the change in the root blade shape by applying the invention. 1... Stationary blade, 2... Moving blade, 4... Stationary blade root side wall, 4'... Moving blade root side wall.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] タービンの回転する動翼の根元部側壁形状にお
いて、子午面形状に凸部を設けたことを特徴とす
るタービン動翼の根元側壁構造。
A root side wall structure of a turbine rotor blade, characterized in that a convex portion is provided in the shape of a meridian plane in the shape of the root side wall of the rotating rotor blade of the turbine.
JP15677286U 1986-10-15 1986-10-15 Pending JPS6363503U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15677286U JPS6363503U (en) 1986-10-15 1986-10-15

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15677286U JPS6363503U (en) 1986-10-15 1986-10-15

Publications (1)

Publication Number Publication Date
JPS6363503U true JPS6363503U (en) 1988-04-26

Family

ID=31078707

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15677286U Pending JPS6363503U (en) 1986-10-15 1986-10-15

Country Status (1)

Country Link
JP (1) JPS6363503U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001271602A (en) * 2000-03-27 2001-10-05 Honda Motor Co Ltd Gas turbine engine
WO2005042925A1 (en) * 2003-10-31 2005-05-12 Kabushiki Kaisha Toshiba Turbine cascade structure

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001271602A (en) * 2000-03-27 2001-10-05 Honda Motor Co Ltd Gas turbine engine
WO2001075276A1 (en) * 2000-03-27 2001-10-11 Honda Giken Kogyo Kabushiki Kaisha Gas turbine engine
US6837679B2 (en) 2000-03-27 2005-01-04 Honda Giken Kogyo Kabushiki Kaisha Gas turbine engine
WO2005042925A1 (en) * 2003-10-31 2005-05-12 Kabushiki Kaisha Toshiba Turbine cascade structure

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