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
- Authority
- JP
- Japan
- Prior art keywords
- fuel nozzle
- fuel
- plate
- gas turbine
- nozzle plate
- 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.)
- Granted
Links
- 239000000446 fuel Substances 0.000 description 22
- 238000011144 upstream manufacturing Methods 0.000 description 5
- 239000007789 gas Substances 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
Description
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.
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)
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)
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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 |
-
2014
- 2014-08-01 JP JP2014157350A patent/JP6301774B2/en active Active
-
2015
- 2015-07-29 CN CN201510455129.6A patent/CN105318355B/en active Active
- 2015-07-30 US US14/813,987 patent/US20160033136A1/en not_active Abandoned
- 2015-07-31 EP EP15179363.5A patent/EP2980483B1/en active Active
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