JP2016035336A5 - - Google Patents

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Publication number
JP2016035336A5
JP2016035336A5 JP2014157350A JP2014157350A JP2016035336A5 JP 2016035336 A5 JP2016035336 A5 JP 2016035336A5 JP 2014157350 A JP2014157350 A JP 2014157350A JP 2014157350 A JP2014157350 A JP 2014157350A JP 2016035336 A5 JP2016035336 A5 JP 2016035336A5
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JP
Japan
Prior art keywords
fuel nozzle
fuel
plate
gas turbine
nozzle plate
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JP2014157350A
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Japanese (ja)
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JP2016035336A (en
JP6301774B2 (en
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Priority to JP2014157350A priority Critical patent/JP6301774B2/en
Priority claimed from JP2014157350A external-priority patent/JP6301774B2/en
Priority to CN201510455129.6A priority patent/CN105318355B/en
Priority to US14/813,987 priority patent/US20160033136A1/en
Priority to EP15179363.5A priority patent/EP2980483B1/en
Publication of JP2016035336A publication Critical patent/JP2016035336A/en
Publication of JP2016035336A5 publication Critical patent/JP2016035336A5/ja
Application granted granted Critical
Publication of JP6301774B2 publication Critical patent/JP6301774B2/en
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図4は、ガスタービン燃焼器7のバーナ18を構成する燃料ノズル15と燃料ノズルプレート14とを接合する比較例の接合方法を示したものであり、この図4に示した比較例の接合方法では、燃料ノズル15の上流側近傍の側面40bと、燃料ノズルプレート14の下流側端部41bとの双方を、燃料ノズルプレート14に対して下流側から接合部42を形成して接合している。 FIG. 4 shows a joining method of a comparative example in which the fuel nozzle 15 constituting the burner 18 of the gas turbine combustor 7 and the fuel nozzle plate 14 are joined. The joining method of the comparative example shown in FIG. Then, both the side surface 40b in the vicinity of the upstream side of the fuel nozzle 15 and the downstream end portion 41b of the fuel nozzle plate 14 are joined to the fuel nozzle plate 14 by forming a joining portion 42 from the downstream side . .

1:ガスタービンプラント、2:空気、3:圧縮機、4:圧縮空気、5:燃料、6:燃焼ガス、7:ガスタービン燃焼器、8:ガスタービン、9:発電機、10:エンドカバー、11:前側外筒、12:後側外筒、13:空気孔プレート、14:燃料ノズルプレート、15:燃料ノズル、16:ライナ、17:後側外筒とライナの間の流路、18:バーナ、19:冷却するための冷却空気、20:燃料供給管、21:空気孔プレートの空気孔、22:燃料と圧縮機の混合気、23:燃焼室、24:火炎、30:燃焼ノズルの下流側端部、40:燃料ノズルの上流側端部、40b:燃料ノズルの上流側近傍の側面、41:燃料ノズルプレートの上流側端部、41b:燃料ノズルプレートの下流側端部、43:燃料ノズルの周囲の空間、44:燃焼ノズル取り付け用孔、42、45:接合部、50:燃焼ノズルの段差部、51:燃焼ノズル取り付け用孔の段差部、52:燃料ノズルの軸方向、60:外形漸減形状部、70、72:テーパー部、71:燃料ノズルの半径方向、80:燃料ノズルの上流側端部のフランジ部、81:燃料ノズルのフランジ部と燃料ノズルプレートの接触部、90:オリフィス部。 1: gas turbine plant, 2: air, 3: compressor, 4: compressed air, 5: fuel, 6: combustion gas, 7: gas turbine combustor, 8: gas turbine, 9: generator, 10: end cover 11: front outer cylinder, 12: rear outer cylinder, 13: air hole plate, 14: fuel nozzle plate, 15: fuel nozzle, 16: liner, 17: flow path between the rear outer cylinder and liner, 18 : Burner, 19: Cooling air for cooling, 20: Fuel supply pipe, 21: Air hole in the air hole plate, 22: Mixture of fuel and compressor, 23: Combustion chamber, 24: Flame, 30: Combustion nozzle 40: upstream end of the fuel nozzle, 40b: side surface near the upstream side of the fuel nozzle, 41: upstream end of the fuel nozzle plate, 41b: downstream end of the fuel nozzle plate, 43 : Space around the fuel nozzle, 44: Fuel Nozzle mounting holes, 42 and 45: junction, 50: stepped portion of the fuel nozzle, 51: stepped portion of the combustion nozzle mounting hole, 52: axial direction of the fuel nozzle, 60: outer tapering shape portion, 70, 72: Tapered portion, 71: radial direction of fuel nozzle, 80: flange portion at upstream end of fuel nozzle, 81: contact portion between flange portion of fuel nozzle and fuel nozzle plate, 90: orifice portion.

JP2014157350A 2014-08-01 2014-08-01 Gas turbine combustor Active JP6301774B2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2014157350A JP6301774B2 (en) 2014-08-01 2014-08-01 Gas turbine combustor
CN201510455129.6A CN105318355B (en) 2014-08-01 2015-07-29 Gas turbine burner
US14/813,987 US20160033136A1 (en) 2014-08-01 2015-07-30 Gas turbine combustor
EP15179363.5A EP2980483B1 (en) 2014-08-01 2015-07-31 Gas turbine combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014157350A JP6301774B2 (en) 2014-08-01 2014-08-01 Gas turbine combustor

Publications (3)

Publication Number Publication Date
JP2016035336A JP2016035336A (en) 2016-03-17
JP2016035336A5 true JP2016035336A5 (en) 2017-02-16
JP6301774B2 JP6301774B2 (en) 2018-03-28

Family

ID=53773318

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014157350A Active JP6301774B2 (en) 2014-08-01 2014-08-01 Gas turbine combustor

Country Status (4)

Country Link
US (1) US20160033136A1 (en)
EP (1) EP2980483B1 (en)
JP (1) JP6301774B2 (en)
CN (1) CN105318355B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6423760B2 (en) 2015-06-24 2018-11-14 三菱日立パワーシステムズ株式会社 Fuel nozzle structure of gas turbine combustor
JP6633982B2 (en) * 2016-07-01 2020-01-22 三菱日立パワーシステムズ株式会社 Gas turbine combustor and method for manufacturing fuel nozzle of gas turbine combustor
FR3059047B1 (en) * 2016-11-21 2020-08-28 Safran Helicopter Engines COMBUSTION CHAMBER INJECTOR FOR A TURBOMACHINE AND ITS MANUFACTURING PROCESS
JP6863718B2 (en) * 2016-11-21 2021-04-21 三菱パワー株式会社 Gas turbine combustor
US10920673B2 (en) * 2017-03-16 2021-02-16 General Electric Company Gas turbine with extraction-air conditioner
CN107023830B (en) * 2017-05-26 2023-11-07 泉州市明燃厨房设备有限公司 Burner nozzle base
CN107477611B (en) * 2017-07-20 2019-08-09 中国科学院工程热物理研究所 Burner
KR102049042B1 (en) * 2017-10-27 2019-11-26 두산중공업 주식회사 Fuel nozzle assembly, combustor and gas turbine having the same
JP7287811B2 (en) * 2019-03-25 2023-06-06 三菱重工業株式会社 Combustor and gas turbine
CN111237087B (en) * 2020-01-19 2024-03-22 西北工业大学 Micro-pore plate active and passive composite cooling structure for aerospace power and cooling method
JP7257350B2 (en) 2020-03-16 2023-04-13 三菱重工業株式会社 gas turbine combustor
JP2021162184A (en) * 2020-03-31 2021-10-11 三菱パワー株式会社 Gas turbine combustor and method for manufacturing fuel nozzle
JP2023131352A (en) * 2022-03-09 2023-09-22 三菱重工業株式会社 Burner, and gas turbine

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3975141A (en) * 1974-06-25 1976-08-17 The United States Of America As Represented By The Secretary Of The Army Combustion liner swirler
JPS5469537A (en) * 1977-11-15 1979-06-04 Hitachi Zosen Corp Joining method for tube and tube plate in heat exchanger or the like
JPS5496537A (en) * 1978-01-17 1979-07-31 Nissan Motor Co Ltd Coating method
JPS5671595A (en) * 1979-11-19 1981-06-15 Toshiba Corp Welding method for tube and tube plate in heat exchanger
US5575153A (en) * 1993-04-07 1996-11-19 Hitachi, Ltd. Stabilizer for gas turbine combustors and gas turbine combustor equipped with the stabilizer
CN1242201C (en) * 2001-07-10 2006-02-15 三菱重工业株式会社 Premixing nozzle, burner and gas turbine
US6813889B2 (en) * 2001-08-29 2004-11-09 Hitachi, Ltd. Gas turbine combustor and operating method thereof
US6857271B2 (en) * 2002-12-16 2005-02-22 Power Systems Mfg., Llc Secondary fuel nozzle with readily customizable pilot fuel flow rate
US8122721B2 (en) * 2006-01-04 2012-02-28 General Electric Company Combustion turbine engine and methods of assembly
JP2009014297A (en) * 2007-07-06 2009-01-22 Hitachi Ltd Gas turbine combustor
JP4906689B2 (en) * 2007-11-29 2012-03-28 株式会社日立製作所 Burner, combustion device, and method for modifying combustion device
US8061142B2 (en) * 2008-04-11 2011-11-22 General Electric Company Mixer for a combustor
US8230687B2 (en) * 2008-09-02 2012-07-31 General Electric Company Multi-tube arrangement for combustor and method of making the multi-tube arrangement
US20100071377A1 (en) * 2008-09-19 2010-03-25 Fox Timothy A Combustor Apparatus for Use in a Gas Turbine Engine
EP2189720A1 (en) * 2008-11-21 2010-05-26 Siemens Aktiengesellschaft Burner assembly
JP2011058775A (en) * 2009-09-14 2011-03-24 Hitachi Ltd Gas turbine combustor
JP5470662B2 (en) * 2011-01-27 2014-04-16 株式会社日立製作所 Gas turbine combustor
JP5393745B2 (en) * 2011-09-05 2014-01-22 川崎重工業株式会社 Gas turbine combustor
JP5630424B2 (en) * 2011-11-21 2014-11-26 三菱日立パワーシステムズ株式会社 Gas turbine combustor
US9296038B2 (en) * 2011-12-29 2016-03-29 Solar Turbines Incorporated Method and apparatus for swaged liquid injector spoke
US9267690B2 (en) * 2012-05-29 2016-02-23 General Electric Company Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same
JP5926635B2 (en) * 2012-07-04 2016-05-25 三菱日立パワーシステムズ株式会社 Gas turbine combustor
JP5908361B2 (en) * 2012-07-24 2016-04-26 三菱日立パワーシステムズ株式会社 Gas turbine combustor
DE102012216080A1 (en) * 2012-08-17 2014-02-20 Dürr Systems GmbH burner

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