JPS58180303U - gas turbine air cooling blade - Google Patents

gas turbine air cooling blade

Info

Publication number
JPS58180303U
JPS58180303U JP7778282U JP7778282U JPS58180303U JP S58180303 U JPS58180303 U JP S58180303U JP 7778282 U JP7778282 U JP 7778282U JP 7778282 U JP7778282 U JP 7778282U JP S58180303 U JPS58180303 U JP S58180303U
Authority
JP
Japan
Prior art keywords
gas turbine
air cooling
blade
turbine air
thin
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
JP7778282U
Other languages
Japanese (ja)
Inventor
山田 義郎
寺西 光夫
Original Assignee
株式会社日立製作所
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 株式会社日立製作所 filed Critical 株式会社日立製作所
Priority to JP7778282U priority Critical patent/JPS58180303U/en
Publication of JPS58180303U publication Critical patent/JPS58180303U/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) [Summary] 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 drawings]

第1図は従来技術を示す動翼の斜視図、第2図は他の従
来技術を示す動翼の斜視図、第3図は本考案の実施例を
示す斜視図、第4図は第3図の断面図である。 1・・・動翼、2・・・動翼ダブティル部、3・・・冷
却孔、4・・・インサート、4a・・・インサート冷却
孔、4b・・・インサート固定板、5・・・空気導入孔
、A・・・冷却空気。
FIG. 1 is a perspective view of a rotor blade showing a prior art, FIG. 2 is a perspective view of a rotor blade showing another prior art, FIG. 3 is a perspective view showing an embodiment of the present invention, and FIG. 4 is a perspective view of a rotor blade showing another prior art. FIG. DESCRIPTION OF SYMBOLS 1... Moving blade, 2... Moving blade dovetail part, 3... Cooling hole, 4... Insert, 4a... Insert cooling hole, 4b... Insert fixing plate, 5... Air Inlet hole, A...Cooling air.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ガスタービン動翼の高さ方向番こ、貫通した空間をもち
、二つの部材に分割可能な中空翼と、この中空翼の内壁
に対して所定の間隔を保ち、空冷用の複数の小孔を設け
た薄肉筒と、この薄肉筒を前記空間に組込み、分割可能
な前記中空翼を接合して前記薄肉筒を固定する機構とか
らなることを特徴とするガスタービン空冷翼。
The height direction of the gas turbine rotor blade is a hollow blade that has a through space and can be divided into two parts, and a plurality of small holes for air cooling that are maintained at a predetermined distance from the inner wall of this hollow blade. A gas turbine air-cooled blade comprising: a thin-walled tube; and a mechanism for assembling the thin-walled tube into the space, joining the splittable hollow blade, and fixing the thin-walled tube.
JP7778282U 1982-05-28 1982-05-28 gas turbine air cooling blade Pending JPS58180303U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7778282U JPS58180303U (en) 1982-05-28 1982-05-28 gas turbine air cooling blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7778282U JPS58180303U (en) 1982-05-28 1982-05-28 gas turbine air cooling blade

Publications (1)

Publication Number Publication Date
JPS58180303U true JPS58180303U (en) 1983-12-02

Family

ID=30087032

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7778282U Pending JPS58180303U (en) 1982-05-28 1982-05-28 gas turbine air cooling blade

Country Status (1)

Country Link
JP (1) JPS58180303U (en)

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