JPS5581228A - Combustor for gas turbine - Google Patents

Combustor for gas turbine

Info

Publication number
JPS5581228A
JPS5581228A JP15719678A JP15719678A JPS5581228A JP S5581228 A JPS5581228 A JP S5581228A JP 15719678 A JP15719678 A JP 15719678A JP 15719678 A JP15719678 A JP 15719678A JP S5581228 A JPS5581228 A JP S5581228A
Authority
JP
Japan
Prior art keywords
transition piece
ducts
duct
back side
face
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
JP15719678A
Other languages
Japanese (ja)
Inventor
Mitsutaka Shizutani
Fumio Kato
Yoshihiro Uchiyama
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP15719678A priority Critical patent/JPS5581228A/en
Publication of JPS5581228A publication Critical patent/JPS5581228A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE: To cool the back side of transition piece effectively by regulating air flow introduced thereinto, through provision of ducts and duct stays to the transition piece.
CONSTITUTION: Ducts 8 is provided on the outer surface of transition piece on the back side 1B near the turbine nozzle to form a conduit extending from the side face to the back face of the transition piece, and the ducts 8 are fixed directly to the transition piece by means of duct stays 9. By the flow regulating function of these duct 8 and duct stays 9, air passed along the side face of transition piece after being deflected by the front face 1A flows uniformly along the back-side surface of transition piece without causing separation. Further, since these ducts 8 and duct stays 9 are fixed directly to the transition piece, they also serve as fins so that back side of the transition piece can be cooled effectively and therefore temperature difference on the back side and the front side of the transition piece can be minimized. Thus, since temperature at the outlet of transition piece can be made uniform, it is enabled to improve reliability of gas turbine and to operate the same at a higher temperature.
COPYRIGHT: (C)1980,JPO&Japio
JP15719678A 1978-12-15 1978-12-15 Combustor for gas turbine Pending JPS5581228A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15719678A JPS5581228A (en) 1978-12-15 1978-12-15 Combustor for gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15719678A JPS5581228A (en) 1978-12-15 1978-12-15 Combustor for gas turbine

Publications (1)

Publication Number Publication Date
JPS5581228A true JPS5581228A (en) 1980-06-19

Family

ID=15644292

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15719678A Pending JPS5581228A (en) 1978-12-15 1978-12-15 Combustor for gas turbine

Country Status (1)

Country Link
JP (1) JPS5581228A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63259125A (en) * 1987-04-01 1988-10-26 ウエスチングハウス・カナダ・インコーポレイテッド Gas turbine
JP2011241824A (en) * 2010-05-20 2011-12-01 General Electric Co <Ge> System for cooling turbine combustor transition piece
JP2020148449A (en) * 2019-03-12 2020-09-17 ドゥサン ヘヴィー インダストリーズ アンド コンストラクション カンパニー リミテッド Transition piece assembly, transition piece module, and combustor and gas turbine including transition piece assembly

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63259125A (en) * 1987-04-01 1988-10-26 ウエスチングハウス・カナダ・インコーポレイテッド Gas turbine
JP2011241824A (en) * 2010-05-20 2011-12-01 General Electric Co <Ge> System for cooling turbine combustor transition piece
EP2388524A3 (en) * 2010-05-20 2018-03-21 General Electric Company System for cooling turbine combustor transition piece
JP2020148449A (en) * 2019-03-12 2020-09-17 ドゥサン ヘヴィー インダストリーズ アンド コンストラクション カンパニー リミテッド Transition piece assembly, transition piece module, and combustor and gas turbine including transition piece assembly
US11105211B2 (en) 2019-03-12 2021-08-31 Doosan Heavy Industries & Construction Co., Ltd. Transition piece assembly, transition piece module, and combustor and gas turbine including transition piece assembly

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