JPS6112903U - gas turbine air cooling blade - Google Patents

gas turbine air cooling blade

Info

Publication number
JPS6112903U
JPS6112903U JP9603484U JP9603484U JPS6112903U JP S6112903 U JPS6112903 U JP S6112903U JP 9603484 U JP9603484 U JP 9603484U JP 9603484 U JP9603484 U JP 9603484U JP S6112903 U JPS6112903 U JP S6112903U
Authority
JP
Japan
Prior art keywords
gas turbine
turbine air
air cooling
cooling blade
blade
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
JP9603484U
Other languages
Japanese (ja)
Inventor
裕行 山尾
Original Assignee
三菱重工業株式会社
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 by 三菱重工業株式会社 filed Critical 三菱重工業株式会社
Priority to JP9603484U priority Critical patent/JPS6112903U/en
Publication of JPS6112903U publication Critical patent/JPS6112903U/en
Pending legal-status Critical Current

Links

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

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

第１図は空冷翼にインサートを挿入する状況を示す斜視
図、第２図は第１図のＡ−Ａ線に沿う断面図である。 １・・・・・・空冷翼、２・・・・・・インサート、８
・・・・・・細孔。FIG. 1 is a perspective view showing a state in which an insert is inserted into an air-cooled blade, and FIG. 2 is a sectional view taken along line A-A in FIG. 1. 1... Air cooling blade, 2... Insert, 8
······pore.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 中空の翼内部に細孔のあいたインサートを挿置して圧入
冷却空気をこれら細孔から吹出させてジェットを生成さ
せるようにしたガスタービン空冷翼において、前記イン
サートの材料として形状記憶合金を使用したガスタービ
ン空冷翼。In a gas turbine air-cooled blade in which an insert with pores is inserted inside a hollow blade and pressurized cooling air is blown out from these pores to generate a jet, a shape memory alloy is used as the material of the insert. Gas turbine air-cooled blades.
JP9603484U 1984-06-28 1984-06-28 gas turbine air cooling blade Pending JPS6112903U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9603484U JPS6112903U (en) 1984-06-28 1984-06-28 gas turbine air cooling blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9603484U JPS6112903U (en) 1984-06-28 1984-06-28 gas turbine air cooling blade

Publications (1)

Publication Number Publication Date
JPS6112903U true JPS6112903U (en) 1986-01-25

Family

ID=30655342

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9603484U Pending JPS6112903U (en) 1984-06-28 1984-06-28 gas turbine air cooling blade

Country Status (1)

Country Link
JP (1) JPS6112903U (en)

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