JPH0317201U - - Google Patents

Info

Publication number
JPH0317201U
JPH0317201U JP7639189U JP7639189U JPH0317201U JP H0317201 U JPH0317201 U JP H0317201U JP 7639189 U JP7639189 U JP 7639189U JP 7639189 U JP7639189 U JP 7639189U JP H0317201 U JPH0317201 U JP H0317201U
Authority
JP
Japan
Prior art keywords
partition plate
diameter
rotor blade
plate
inlet side
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
JP7639189U
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 JP7639189U priority Critical patent/JPH0317201U/ja
Publication of JPH0317201U publication Critical patent/JPH0317201U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案によるタービン仕切板の一実施
例を示す要部構造断面図、第2図は従来のタービ
ン仕切板を示す要部構造断面図である。 1…仕切板、1a…ノズル、2…動翼、10…
空隙部、11…調整板、12…中間板、Fi…動
翼入口流体、Fo…動翼出口流体、Fl…チツプ
リーケツジ、Fr,F′r…ルートリーケツジ、
Fc,F′c…仕切板リーケツジ、F′i…漏出
流体、S…渦流、S′…固定渦、Sl…ゼロ流線
FIG. 1 is a sectional view of the main part structure of an embodiment of the turbine partition plate according to the present invention, and FIG. 2 is a sectional view of the main part structure of a conventional turbine partition plate. 1... Partition plate, 1a... Nozzle, 2... Moving blade, 10...
Gap portion, 11... Adjustment plate, 12... Intermediate plate, Fi... Moving blade inlet fluid, Fo... Moving blade outlet fluid, Fl... Chipply cage, Fr, F'r... Routley cage,
Fc, F'c...partition plate leakage, F'i...leakage fluid, S...vortex, S'...fixed vortex, Sl...zero streamline.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 軸流タービンの仕切板において、動翼間に設置
する仕切板の流体入口側チツプ部分に、その前段
落に配置した動翼の外周径より大きく、かつ当該
仕切板のノズルの外周径より小さい径を有する環
状の調整板を取付けると共に、仕切板の流体入口
側根本部分に、その前段落に配置した動翼ルート
径より大きい外径を有し、かつ動翼と仕切板との
空隙部を分割するよう断面略楔形に形成した環状
の中間板を取付けたことを特徴とするタービン仕
切板。
In the partition plate of an axial flow turbine, a tip on the fluid inlet side of the partition plate installed between the rotor blades has a diameter that is larger than the outer circumferential diameter of the rotor blade placed in the preceding paragraph and smaller than the outer circumferential diameter of the nozzle of the partition plate. At the same time, install an annular adjustment plate having an outer diameter larger than the rotor blade root diameter placed in the previous paragraph at the root part of the fluid inlet side of the partition plate, and divide the gap between the rotor blade and the partition plate. A turbine partition plate characterized in that an annular intermediate plate having a substantially wedge-shaped cross section is attached.
JP7639189U 1989-06-30 1989-06-30 Pending JPH0317201U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7639189U JPH0317201U (en) 1989-06-30 1989-06-30

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7639189U JPH0317201U (en) 1989-06-30 1989-06-30

Publications (1)

Publication Number Publication Date
JPH0317201U true JPH0317201U (en) 1991-02-20

Family

ID=31617819

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7639189U Pending JPH0317201U (en) 1989-06-30 1989-06-30

Country Status (1)

Country Link
JP (1) JPH0317201U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006075047A (en) * 2004-09-08 2006-03-23 Mkv Platech Co Ltd Agricultural film
JP2014020307A (en) * 2012-07-19 2014-02-03 Mitsubishi Heavy Ind Ltd Gas turbine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006075047A (en) * 2004-09-08 2006-03-23 Mkv Platech Co Ltd Agricultural film
JP2014020307A (en) * 2012-07-19 2014-02-03 Mitsubishi Heavy Ind Ltd Gas turbine

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