JPS6239158U - - Google Patents

Info

Publication number
JPS6239158U
JPS6239158U JP13114985U JP13114985U JPS6239158U JP S6239158 U JPS6239158 U JP S6239158U JP 13114985 U JP13114985 U JP 13114985U JP 13114985 U JP13114985 U JP 13114985U JP S6239158 U JPS6239158 U JP S6239158U
Authority
JP
Japan
Prior art keywords
combustor
transition piece
inlet
gas turbine
piece inlet
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
JP13114985U
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 JP13114985U priority Critical patent/JPS6239158U/ja
Publication of JPS6239158U publication Critical patent/JPS6239158U/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 drawings]

第1図は本考案の1実施例にかかる燃焼器車室
の一部破断側面図、第2図は従来の燃焼器車室の
一部破断側面図である。 3…燃焼器部、4…尾筒部、5…タービン部、
9…段違いダクト。
FIG. 1 is a partially cutaway side view of a combustor casing according to an embodiment of the present invention, and FIG. 2 is a partially cutaway side view of a conventional combustor casing. 3... Combustor section, 4... Transition section, 5... Turbine section,
9...Uneven duct.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ガスタービン燃焼器の燃焼器出口部と、尾筒入
口部とを接続するに際し、該尾筒入口部を上記燃
焼器出口部よりも予め軸心寄りに段違いにオフセ
ツトして、上記燃焼器出口部と上記尾筒入口部と
をダクトで接続したことを特徴とするガスタービ
ン燃焼器。
When connecting the combustor outlet of the gas turbine combustor and the transition piece inlet, the transition piece inlet is offset in advance toward the axial center from the combustor outlet so that the transition piece inlet is connected to the combustor outlet. A gas turbine combustor characterized in that the and the transition tube inlet are connected by a duct.
JP13114985U 1985-08-28 1985-08-28 Pending JPS6239158U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13114985U JPS6239158U (en) 1985-08-28 1985-08-28

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13114985U JPS6239158U (en) 1985-08-28 1985-08-28

Publications (1)

Publication Number Publication Date
JPS6239158U true JPS6239158U (en) 1987-03-09

Family

ID=31029320

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13114985U Pending JPS6239158U (en) 1985-08-28 1985-08-28

Country Status (1)

Country Link
JP (1) JPS6239158U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003106526A (en) * 2001-09-27 2003-04-09 Osaka Gas Co Ltd Gas turbine combustion device and gas turbine therewith

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003106526A (en) * 2001-09-27 2003-04-09 Osaka Gas Co Ltd Gas turbine combustion device and gas turbine therewith
JP4608154B2 (en) * 2001-09-27 2011-01-05 大阪瓦斯株式会社 Gas turbine combustion apparatus and gas turbine provided with the same

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