JPS643003U - - Google Patents

Info

Publication number
JPS643003U
JPS643003U JP9595287U JP9595287U JPS643003U JP S643003 U JPS643003 U JP S643003U JP 9595287 U JP9595287 U JP 9595287U JP 9595287 U JP9595287 U JP 9595287U JP S643003 U JPS643003 U JP S643003U
Authority
JP
Japan
Prior art keywords
circumference
steam turbine
stator
blade
blades
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
JP9595287U
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 JP9595287U priority Critical patent/JPS643003U/ja
Publication of JPS643003U publication Critical patent/JPS643003U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案の第1の実施例を示す構造図、
第2図は第1図の部分矢視図、第3図は従来静翼
の構造断面図、第4図は第1図のA―A断面図、
第5図は水滴径の頻度分布の説明図、第6図は第
2の実施例を示す構造図、第7図は従来の典型的
なタービンの断面構造図、第8図は第7図の部分
矢視図、第9図は第8図のB―B断面図である。 1,1′…静翼、16…段差。
FIG. 1 is a structural diagram showing a first embodiment of the present invention;
Fig. 2 is a partial view in the direction of the arrows in Fig. 1, Fig. 3 is a structural sectional view of a conventional stationary blade, Fig. 4 is a sectional view taken along line AA in Fig. 1,
Fig. 5 is an explanatory diagram of the frequency distribution of water droplet diameters, Fig. 6 is a structural diagram showing the second embodiment, Fig. 7 is a cross-sectional structural diagram of a typical conventional turbine, and Fig. 8 is the same as Fig. 7. 9 is a sectional view taken along line BB in FIG. 8. 1, 1'... Stator blade, 16... Step.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 静翼を円周上に複数枚支持するダイヤフラム及
び支持リングと、動翼を円周上に複数枚支持する
デイスクロータとからなる蒸気タービン装置に使
用される静翼々型において、該翼型の前縁と後縁
との間の翼表面の一部に段差部を形成したことを
特徴とする蒸気タービン静翼。
In a stator blade type used in a steam turbine device, which is composed of a diaphragm and a support ring that support a plurality of stator blades on the circumference, and a disc rotor that supports a plurality of rotor blades on the circumference, the front of the airfoil is A steam turbine stationary blade characterized by forming a stepped portion in a part of the blade surface between an edge and a trailing edge.
JP9595287U 1987-06-24 1987-06-24 Pending JPS643003U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9595287U JPS643003U (en) 1987-06-24 1987-06-24

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9595287U JPS643003U (en) 1987-06-24 1987-06-24

Publications (1)

Publication Number Publication Date
JPS643003U true JPS643003U (en) 1989-01-10

Family

ID=31320730

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9595287U Pending JPS643003U (en) 1987-06-24 1987-06-24

Country Status (1)

Country Link
JP (1) JPS643003U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013231394A (en) * 2012-04-27 2013-11-14 Toshiba Corp Steam turbine blade and steam turbine
JP2015183535A (en) * 2014-03-20 2015-10-22 株式会社東芝 Steam turbine and method for forming nozzle coating on steam turbine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013231394A (en) * 2012-04-27 2013-11-14 Toshiba Corp Steam turbine blade and steam turbine
JP2015183535A (en) * 2014-03-20 2015-10-22 株式会社東芝 Steam turbine and method for forming nozzle coating on steam turbine

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