RU2523519C2 - Способ эксплуатации горелки, горелка, в частности для газовой турбины и газовая турбина - Google Patents
Способ эксплуатации горелки, горелка, в частности для газовой турбины и газовая турбина Download PDFInfo
- Publication number
- RU2523519C2 RU2523519C2 RU2011141846/06A RU2011141846A RU2523519C2 RU 2523519 C2 RU2523519 C2 RU 2523519C2 RU 2011141846/06 A RU2011141846/06 A RU 2011141846/06A RU 2011141846 A RU2011141846 A RU 2011141846A RU 2523519 C2 RU2523519 C2 RU 2523519C2
- Authority
- RU
- Russia
- Prior art keywords
- burner
- axis
- jet nozzle
- middle axis
- air
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 19
- 239000000446 fuel Substances 0.000 claims abstract description 60
- 239000011261 inert gas Substances 0.000 claims abstract description 35
- 239000007789 gas Substances 0.000 claims abstract description 16
- 239000012530 fluid Substances 0.000 claims abstract description 9
- 230000002093 peripheral effect Effects 0.000 claims description 12
- 238000001816 cooling Methods 0.000 claims description 3
- 230000003213 activating effect Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
- 238000002485 combustion reaction Methods 0.000 description 10
- 238000010586 diagram Methods 0.000 description 5
- 238000007664 blowing Methods 0.000 description 3
- 230000003111 delayed effect Effects 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- MWUXSHHQAYIFBG-UHFFFAOYSA-N Nitric oxide Chemical compound O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 230000004941 influx Effects 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000010349 pulsation Effects 0.000 description 1
- 230000003134 recirculating effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP09155341A EP2236932A1 (de) | 2009-03-17 | 2009-03-17 | Verfahren zum Betrieb eines Brenners und Brenner, insbesondere für eine Gasturbine |
| EP09155341.2 | 2009-03-17 | ||
| PCT/EP2010/053325 WO2010106034A2 (de) | 2009-03-17 | 2010-03-16 | Verfahren zum betrieb eines brenners und brenner, insbesondere für eine gasturbine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2011141846A RU2011141846A (ru) | 2013-04-27 |
| RU2523519C2 true RU2523519C2 (ru) | 2014-07-20 |
Family
ID=41021051
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2011141846/06A RU2523519C2 (ru) | 2009-03-17 | 2010-03-16 | Способ эксплуатации горелки, горелка, в частности для газовой турбины и газовая турбина |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US9032736B2 (enExample) |
| EP (2) | EP2236932A1 (enExample) |
| JP (1) | JP5460850B2 (enExample) |
| CN (1) | CN102356279B (enExample) |
| RU (1) | RU2523519C2 (enExample) |
| WO (1) | WO2010106034A2 (enExample) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2078898A1 (de) * | 2008-01-11 | 2009-07-15 | Siemens Aktiengesellschaft | Brenner und Verfahren zur Verringerung von selbstinduzierten Flammenschwingungen |
| EP2587158A1 (de) * | 2011-10-31 | 2013-05-01 | Siemens Aktiengesellschaft | Brennkammer für eine Gasturbine und Brenneranordnung |
| US20150159877A1 (en) * | 2013-12-06 | 2015-06-11 | General Electric Company | Late lean injection manifold mixing system |
| JP6440433B2 (ja) * | 2014-09-29 | 2018-12-19 | 川崎重工業株式会社 | 燃料噴射ノズル、燃料噴射モジュール、及びガスタービン |
| EP3301374A1 (en) * | 2016-09-29 | 2018-04-04 | Siemens Aktiengesellschaft | A pilot burner assembly with pilot-air supply |
| JP2022049136A (ja) * | 2020-09-16 | 2022-03-29 | 三菱重工業株式会社 | 燃料ノズルおよびガスタービン燃焼器 |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5263316A (en) * | 1989-12-21 | 1993-11-23 | Sundstrand Corporation | Turbine engine with airblast injection |
| WO1995016881A1 (en) * | 1993-12-17 | 1995-06-22 | Abb Stal Ab | Method and apparatus for atomizing liquid fuel |
| RU2055271C1 (ru) * | 1993-08-11 | 1996-02-27 | Липатов Петр Алексеевич | Способ создания поперечной струи воздуха с топливом в камере сгорания газотурбинной установки с циркуляционным течением в головной части |
| EP1331441A1 (en) * | 2002-01-21 | 2003-07-30 | National Aerospace Laboratory of Japan | Liquid atomizing nozzle |
| RU2215243C2 (ru) * | 1997-12-15 | 2003-10-27 | Юнайтед Текнолоджиз Корпорейшн | Топливная форсунка с предварительным смешением топлива (варианты), и способ сжигания топлива (варианты) |
| RU2241177C2 (ru) * | 2002-07-02 | 2004-11-27 | Кашапов Рафаэль Салихзянович | Камера сгорания |
| EP1526332A2 (de) * | 2003-10-20 | 2005-04-27 | Rolls-Royce Deutschland Ltd & Co KG | Kraftstoffeinspritzdüse |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2694624B1 (fr) * | 1992-08-05 | 1994-09-23 | Snecma | Chambre de combustion à plusieurs injecteurs de carburant. |
| US5599371A (en) * | 1994-12-30 | 1997-02-04 | Corning Incorporated | Method of using precision burners for oxidizing halide-free, silicon-containing compounds |
| US6267585B1 (en) * | 1995-12-19 | 2001-07-31 | Daimlerchrysler Aerospace Airbus Gmbh | Method and combustor for combusting hydrogen |
| US5778676A (en) * | 1996-01-02 | 1998-07-14 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US6176894B1 (en) | 1998-06-17 | 2001-01-23 | Praxair Technology, Inc. | Supersonic coherent gas jet for providing gas into a liquid |
| US6427446B1 (en) * | 2000-09-19 | 2002-08-06 | Power Systems Mfg., Llc | Low NOx emission combustion liner with circumferentially angled film cooling holes |
| DE10112864A1 (de) | 2001-03-16 | 2002-09-19 | Alstom Switzerland Ltd | Verfahren zum Zünden einer thermischen Turbomaschine |
| JP2004170010A (ja) * | 2002-11-21 | 2004-06-17 | Hitachi Ltd | ガスタービン燃焼器及びガスタービン燃焼器の燃料供給方法 |
| US6623267B1 (en) * | 2002-12-31 | 2003-09-23 | Tibbs M. Golladay, Jr. | Industrial burner |
| JP2005061715A (ja) * | 2003-08-13 | 2005-03-10 | Ishikawajima Harima Heavy Ind Co Ltd | 希薄予蒸発予混合燃焼器 |
| US7000403B2 (en) * | 2004-03-12 | 2006-02-21 | Power Systems Mfg., Llc | Primary fuel nozzle having dual fuel capability |
| JP2007232325A (ja) * | 2006-03-03 | 2007-09-13 | Hitachi Ltd | ガスタービン燃焼器 |
| JP4959620B2 (ja) * | 2007-04-26 | 2012-06-27 | 株式会社日立製作所 | 燃焼器及び燃焼器の燃料供給方法 |
| EP2078898A1 (de) * | 2008-01-11 | 2009-07-15 | Siemens Aktiengesellschaft | Brenner und Verfahren zur Verringerung von selbstinduzierten Flammenschwingungen |
-
2009
- 2009-03-17 EP EP09155341A patent/EP2236932A1/de not_active Withdrawn
-
2010
- 2010-03-16 CN CN201080012113.3A patent/CN102356279B/zh not_active Expired - Fee Related
- 2010-03-16 EP EP10711184A patent/EP2409087A2/de not_active Withdrawn
- 2010-03-16 US US13/256,293 patent/US9032736B2/en not_active Expired - Fee Related
- 2010-03-16 WO PCT/EP2010/053325 patent/WO2010106034A2/de not_active Ceased
- 2010-03-16 JP JP2012500211A patent/JP5460850B2/ja not_active Expired - Fee Related
- 2010-03-16 RU RU2011141846/06A patent/RU2523519C2/ru not_active IP Right Cessation
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5263316A (en) * | 1989-12-21 | 1993-11-23 | Sundstrand Corporation | Turbine engine with airblast injection |
| RU2055271C1 (ru) * | 1993-08-11 | 1996-02-27 | Липатов Петр Алексеевич | Способ создания поперечной струи воздуха с топливом в камере сгорания газотурбинной установки с циркуляционным течением в головной части |
| WO1995016881A1 (en) * | 1993-12-17 | 1995-06-22 | Abb Stal Ab | Method and apparatus for atomizing liquid fuel |
| RU2215243C2 (ru) * | 1997-12-15 | 2003-10-27 | Юнайтед Текнолоджиз Корпорейшн | Топливная форсунка с предварительным смешением топлива (варианты), и способ сжигания топлива (варианты) |
| EP1331441A1 (en) * | 2002-01-21 | 2003-07-30 | National Aerospace Laboratory of Japan | Liquid atomizing nozzle |
| RU2241177C2 (ru) * | 2002-07-02 | 2004-11-27 | Кашапов Рафаэль Салихзянович | Камера сгорания |
| EP1526332A2 (de) * | 2003-10-20 | 2005-04-27 | Rolls-Royce Deutschland Ltd & Co KG | Kraftstoffeinspritzdüse |
Also Published As
| Publication number | Publication date |
|---|---|
| RU2011141846A (ru) | 2013-04-27 |
| US20120000203A1 (en) | 2012-01-05 |
| EP2409087A2 (de) | 2012-01-25 |
| US9032736B2 (en) | 2015-05-19 |
| EP2236932A1 (de) | 2010-10-06 |
| CN102356279B (zh) | 2014-03-12 |
| JP5460850B2 (ja) | 2014-04-02 |
| JP2012520984A (ja) | 2012-09-10 |
| WO2010106034A2 (de) | 2010-09-23 |
| CN102356279A (zh) | 2012-02-15 |
| WO2010106034A3 (de) | 2011-05-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20180317 |