JPS614178U - Cooling structure of combustor transition piece - Google Patents

Cooling structure of combustor transition piece

Info

Publication number
JPS614178U
JPS614178U JP8808684U JP8808684U JPS614178U JP S614178 U JPS614178 U JP S614178U JP 8808684 U JP8808684 U JP 8808684U JP 8808684 U JP8808684 U JP 8808684U JP S614178 U JPS614178 U JP S614178U
Authority
JP
Japan
Prior art keywords
transition piece
cooling structure
cooling
wall
combustor transition
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
JP8808684U
Other languages
Japanese (ja)
Inventor
重実 萬代
満 稲田
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 JP8808684U priority Critical patent/JPS614178U/en
Publication of JPS614178U publication Critical patent/JPS614178U/en
Pending legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)

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 the drawing]

第1図は本考案による尾簡の冷却構造を示す斜視図、第
2図は第1図における■一I線矢視の断面図、第3図は
従来のガスタービン燃焼器の尾筒構造や示す側面図であ
る。 、 1−2・・・・・・尾筒、2−1・・・・・・対流
冷却プレート、2−2・・・・・・フィルム冷却孔、2
−3・・・・・・燃焼ガス、2−4・・・・・・フイル
ム冷却幸気。
Fig. 1 is a perspective view showing the tail piece cooling structure according to the present invention, Fig. 2 is a sectional view taken along the line II in Fig. 1, and Fig. 3 shows the tail piece structure of a conventional gas turbine combustor. FIG. , 1-2... Transition piece, 2-1... Convection cooling plate, 2-2... Film cooling hole, 2
-3... Combustion gas, 2-4... Film cooling air.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃焼器尾簡の高温部に複数のフイルム冷却孔を穿設し、
同部分の尾筒外壁に間隙をもたせて対流・冷却プレート
を付設し、同冷却プレニトと尾筒外壁との間の間隙を流
れる空気を上記フイルム冷却孔より尾筒内壁に沿って流
入するよう構成した燃焼器尾筒の冷却構造。
Multiple film cooling holes are drilled in the high temperature part of the combustor tail.
A convection/cooling plate is attached to the outer wall of the transition tube in the same area with a gap, and the air flowing through the gap between the cooling prenit and the outer wall of the transition tube is configured to flow through the film cooling hole and along the inner wall of the transition tube. The cooling structure of the combustor transition piece.
JP8808684U 1984-06-15 1984-06-15 Cooling structure of combustor transition piece Pending JPS614178U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8808684U JPS614178U (en) 1984-06-15 1984-06-15 Cooling structure of combustor transition piece

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8808684U JPS614178U (en) 1984-06-15 1984-06-15 Cooling structure of combustor transition piece

Publications (1)

Publication Number Publication Date
JPS614178U true JPS614178U (en) 1986-01-11

Family

ID=30640895

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8808684U Pending JPS614178U (en) 1984-06-15 1984-06-15 Cooling structure of combustor transition piece

Country Status (1)

Country Link
JP (1) JPS614178U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6463714A (en) * 1987-09-02 1989-03-09 Noritz Corp Combustion control device for burner

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6463714A (en) * 1987-09-02 1989-03-09 Noritz Corp Combustion control device for burner

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