JPS60143272U - Gas turbine combustor transition piece - Google Patents

Gas turbine combustor transition piece

Info

Publication number
JPS60143272U
JPS60143272U JP3064084U JP3064084U JPS60143272U JP S60143272 U JPS60143272 U JP S60143272U JP 3064084 U JP3064084 U JP 3064084U JP 3064084 U JP3064084 U JP 3064084U JP S60143272 U JPS60143272 U JP S60143272U
Authority
JP
Japan
Prior art keywords
transition piece
gas turbine
turbine combustor
cooling air
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.)
Granted
Application number
JP3064084U
Other languages
Japanese (ja)
Other versions
JPH0233021Y2 (en
Inventor
重実 萬代
満 稲田
福江　一郎
邦明 青山
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 JP3064084U priority Critical patent/JPS60143272U/en
Publication of JPS60143272U publication Critical patent/JPS60143272U/en
Application granted granted Critical
Publication of JPH0233021Y2 publication Critical patent/JPH0233021Y2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (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 drawings]

第１図は尾筒の斜視図、第２図はその縦断断面図、第３
図は第２図のＡ部龜示す尾筒部分として使用する高温部
材板の冷却空気流路を示す断面図、第４図は第３図のＢ
二Ｂ線断面図、第５図は高温部材板の斜視図である。Figure 1 is a perspective view of the transition piece, Figure 2 is its vertical sectional view, and Figure 3 is a perspective view of the transition piece.
The figure is a sectional view showing the cooling air flow path of the high-temperature member plate used as the tail piece part shown in section A in figure 2, and figure 4 is B in figure 3.
A sectional view taken along the line 2B, and FIG. 5 is a perspective view of the high-temperature member plate.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 冷却空気流路幅（幅）Ｃを小さく、冷却空気流路ピッチ
ｐを太き（選定し、冷却空気入口孔および出口孔面積を
冷、却空気流路面積の２倍以上とした高温部材板で少な
くとも一部分を構成したことを特徴とするガスタービン
燃焼器の尾筒。A high-temperature member board in which the cooling air flow path width (width) C is small, the cooling air flow path pitch p is thick (selected), and the area of the cooling air inlet hole and outlet hole is at least twice the area of the cooling air flow path. A transition piece of a gas turbine combustor, characterized in that at least a portion of the transition piece comprises:
JP3064084U 1984-03-05 1984-03-05 Gas turbine combustor transition piece Granted JPS60143272U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3064084U JPS60143272U (en) 1984-03-05 1984-03-05 Gas turbine combustor transition piece

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3064084U JPS60143272U (en) 1984-03-05 1984-03-05 Gas turbine combustor transition piece

Publications (2)

Publication Number Publication Date
JPS60143272U true JPS60143272U (en) 1985-09-21
JPH0233021Y2 JPH0233021Y2 (en) 1990-09-06

Family

ID=30530520

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3064084U Granted JPS60143272U (en) 1984-03-05 1984-03-05 Gas turbine combustor transition piece

Country Status (1)

Country Link
JP (1) JPS60143272U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8834154B2 (en) 2012-11-28 2014-09-16 Mitsubishi Heavy Industries, Ltd. Transition piece of combustor, and gas turbine having the same

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5743678U (en) * 1980-08-22 1982-03-10

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5743678U (en) * 1980-08-22 1982-03-10

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8834154B2 (en) 2012-11-28 2014-09-16 Mitsubishi Heavy Industries, Ltd. Transition piece of combustor, and gas turbine having the same

Also Published As

Publication number Publication date
JPH0233021Y2 (en) 1990-09-06

Similar Documents

Publication Publication Date Title
JPS60143272U (en) Gas turbine combustor transition piece
JPS5967720U (en) air conditioner
JPS58173701U (en) gas turbine
JPS604687U (en) Drainage
JPS59120367U (en) combustor
JPS59185516U (en) air conditioner
JPS614178U (en) Cooling structure of combustor transition piece
JPS5913821U (en) burner
JPS6055826U (en) Forced supply and exhaust combustion equipment
JPS5959671U (en) gas turbine combustor
JPS6139266U (en) gas turbine combustor
JPS59163866U (en) Solar collector for air heating
JPS59132054U (en) Air-cooled heat pump type air conditioner
JPS60128164U (en) combustor
JPS6052301U (en) axial flow turbomachinery
JPS58142301U (en) Multi-stage air motor
JPS6143675U (en) Gas turbine combustor transition piece
JPS5893646U (en) Outdoor combustor
JPS59141102U (en) Gas turbine stator blade shroud structure
JPS59186607U (en) boiler
JPS5932863U (en) gas turbine combustor
JPS60148815U (en) combustor
JPS60133361U (en) Thermal equipment with heat exchanger
JPS60141428U (en) Turbo combustion device
JPS60185068U (en) Once-through turbine runner