JPS6413237U - - Google Patents

Info

Publication number
JPS6413237U
JPS6413237U JP10633887U JP10633887U JPS6413237U JP S6413237 U JPS6413237 U JP S6413237U JP 10633887 U JP10633887 U JP 10633887U JP 10633887 U JP10633887 U JP 10633887U JP S6413237 U JPS6413237 U JP S6413237U
Authority
JP
Japan
Prior art keywords
flow rate
adjustment mechanism
air
rate adjustment
distribution
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
JP10633887U
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 JP10633887U priority Critical patent/JPS6413237U/ja
Publication of JPS6413237U publication Critical patent/JPS6413237U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

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のガスタービン燃焼
器及びその周辺の断面図、第2図は本考案を実施
した場合の流量調整穴開口面積、燃焼器尾筒フロ
ースリーブ差圧及びタービン効率変化を示す図で
ある。 1……圧縮機吐出空気、2……インピンジメン
ト冷却穴、3……フロースリーブ。
Figure 1 is a cross-sectional view of the gas turbine combustor and its surroundings according to an embodiment of the present invention, and Figure 2 is a flow adjustment hole opening area, combustor transition pipe flow sleeve differential pressure, and turbine efficiency when the present invention is implemented. It is a figure showing a change. 1... Compressor discharge air, 2... Impingement cooling hole, 3... Flow sleeve.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 外表面のインピンジメント冷却するための多数
の空気孔と流入空気流量配分を調整できる流量調
整機構付空気孔とをもつスリーブによつて囲まれ
た燃焼器尾筒を設け、ガスタービン負荷に応じて
前記流量調整機構付空気孔の流路面積を変化させ
、前記インピンジメント冷却の空気の流量配分を
変えることを特徴とする流量調整機構付燃焼器尾
筒。
A combustor transition piece is surrounded by a sleeve that has a large number of air holes for impingement cooling on the outer surface and an air hole with a flow rate adjustment mechanism that can adjust the distribution of incoming air flow rate. A combustor transition piece with a flow rate adjustment mechanism, characterized in that the flow path area of the air hole with the flow rate adjustment mechanism is changed to change the flow rate distribution of the impingement cooling air.
JP10633887U 1987-07-13 1987-07-13 Pending JPS6413237U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10633887U JPS6413237U (en) 1987-07-13 1987-07-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10633887U JPS6413237U (en) 1987-07-13 1987-07-13

Publications (1)

Publication Number Publication Date
JPS6413237U true JPS6413237U (en) 1989-01-24

Family

ID=31339753

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10633887U Pending JPS6413237U (en) 1987-07-13 1987-07-13

Country Status (1)

Country Link
JP (1) JPS6413237U (en)

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