JPS61147301U - - Google Patents

Info

Publication number
JPS61147301U
JPS61147301U JP3027685U JP3027685U JPS61147301U JP S61147301 U JPS61147301 U JP S61147301U JP 3027685 U JP3027685 U JP 3027685U JP 3027685 U JP3027685 U JP 3027685U JP S61147301 U JPS61147301 U JP S61147301U
Authority
JP
Japan
Prior art keywords
shroud
cooling air
air hole
blade
cooling
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
JP3027685U
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 JP3027685U priority Critical patent/JPS61147301U/ja
Publication of JPS61147301U publication Critical patent/JPS61147301U/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に係るシユラウド翼
の冷却装置の断面図、第2図は従来のガスタービ
ン装置における動翼とシユラウドを示す斜視図で
ある。 図面中、1,4は動翼、2,5はシユラウド、
3,11はタービンデイスク、6はタービン輪環
、7はタービン輪環保持部材、8,9は冷却空気
孔、10は障壁部品、白ぬきの矢印は作動流体の
流れる方向を示すものである。
FIG. 1 is a sectional view of a shroud blade cooling device according to an embodiment of the present invention, and FIG. 2 is a perspective view showing a rotor blade and a shroud in a conventional gas turbine device. In the drawing, 1 and 4 are rotor blades, 2 and 5 are shrouds,
3 and 11 are turbine disks, 6 is a turbine ring, 7 is a turbine ring holding member, 8 and 9 are cooling air holes, 10 is a barrier component, and the white arrow indicates the flow direction of the working fluid.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] タービン動翼の外周部に取り付けられたシユラ
ウドに対向する部分におけるケーシングに冷却空
気孔を設けて、該冷却空気孔から導入された冷却
空気を前記シユラウドに吹き付けるようにしたこ
とを特徴とするシユラウド翼の冷却装置。
A shroud blade characterized in that a cooling air hole is provided in a portion of the casing opposite to a shroud attached to an outer peripheral portion of a turbine rotor blade, and cooling air introduced from the cooling air hole is blown onto the shroud. cooling system.
JP3027685U 1985-03-05 1985-03-05 Pending JPS61147301U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3027685U JPS61147301U (en) 1985-03-05 1985-03-05

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3027685U JPS61147301U (en) 1985-03-05 1985-03-05

Publications (1)

Publication Number Publication Date
JPS61147301U true JPS61147301U (en) 1986-09-11

Family

ID=30529831

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3027685U Pending JPS61147301U (en) 1985-03-05 1985-03-05

Country Status (1)

Country Link
JP (1) JPS61147301U (en)

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