JPS6361663U - - Google Patents

Info

Publication number
JPS6361663U
JPS6361663U JP15441186U JP15441186U JPS6361663U JP S6361663 U JPS6361663 U JP S6361663U JP 15441186 U JP15441186 U JP 15441186U JP 15441186 U JP15441186 U JP 15441186U JP S6361663 U JPS6361663 U JP S6361663U
Authority
JP
Japan
Prior art keywords
combustor
type
gas turbine
equalize
sector
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
JP15441186U
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 JP15441186U priority Critical patent/JPS6361663U/ja
Publication of JPS6361663U publication Critical patent/JPS6361663U/ja
Pending legal-status Critical Current

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Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

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

第1図は本考案のガスタービン燃焼器の構成を
示す断面図、第2図は第1図の―線断面図、
第3図は従来のガスタービン燃焼器の断面図、第
4図は従来のガスタービン内コンプレツサ吐出空
気の流れを示す断面図、第5図は第4図の―
線断面図である。 103……尾筒、104……燃焼器、107…
…ケーシング、201……ケーシング側、202
……ケーシング反対側、301……分流板。
Fig. 1 is a cross-sectional view showing the configuration of the gas turbine combustor of the present invention, Fig. 2 is a cross-sectional view taken along the line -- in Fig. 1,
Fig. 3 is a sectional view of a conventional gas turbine combustor, Fig. 4 is a sectional view showing the flow of compressor discharge air in a conventional gas turbine, and Fig. 5 is a sectional view of the conventional gas turbine combustor.
FIG. 103... Transition pipe, 104... Combustor, 107...
...Casing, 201...Casing side, 202
... Opposite side of casing, 301 ... Diversion plate.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] キヤン型あるいはセクター型燃焼器を有するガ
スタービンにおいて、燃焼器と第一段静翼をつな
ぐ燃焼器尾筒の側面に空気流れを均一化するため
コンプレツサ出口空気を分流する分流板を取り付
けたガスタービン燃焼器。
A gas turbine with a can-type or sector-type combustor, in which a flow divider plate is attached to the side of the combustor transition piece that connects the combustor and the first stage stationary blade to divide compressor outlet air in order to equalize the air flow. combustor.
JP15441186U 1986-10-09 1986-10-09 Pending JPS6361663U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15441186U JPS6361663U (en) 1986-10-09 1986-10-09

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15441186U JPS6361663U (en) 1986-10-09 1986-10-09

Publications (1)

Publication Number Publication Date
JPS6361663U true JPS6361663U (en) 1988-04-23

Family

ID=31074178

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15441186U Pending JPS6361663U (en) 1986-10-09 1986-10-09

Country Status (1)

Country Link
JP (1) JPS6361663U (en)

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