SI4278132T1 - Burner - Google Patents
BurnerInfo
- Publication number
- SI4278132T1 SI4278132T1 SI202230120T SI202230120T SI4278132T1 SI 4278132 T1 SI4278132 T1 SI 4278132T1 SI 202230120 T SI202230120 T SI 202230120T SI 202230120 T SI202230120 T SI 202230120T SI 4278132 T1 SI4278132 T1 SI 4278132T1
- Authority
- SI
- Slovenia
- Prior art keywords
- burner
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
-
- 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
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00016—Retrofitting in general, e.g. to respect new regulations on pollution
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP21151199.3A EP4027059A1 (en) | 2021-01-12 | 2021-01-12 | Burner, combustor, and method for retrofitting a combustion appliance |
| PCT/EP2022/050242 WO2022152622A1 (en) | 2021-01-12 | 2022-01-07 | Burner |
| EP22700316.7A EP4278132B1 (en) | 2021-01-12 | 2022-01-07 | Burner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SI4278132T1 true SI4278132T1 (en) | 2025-06-30 |
Family
ID=74180944
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SI202230120T SI4278132T1 (en) | 2021-01-12 | 2022-01-07 | Burner |
Country Status (13)
| Country | Link |
|---|---|
| US (1) | US20240060644A1 (en) |
| EP (2) | EP4027059A1 (en) |
| CA (1) | CA3204173A1 (en) |
| DK (1) | DK4278132T3 (en) |
| ES (1) | ES3026507T3 (en) |
| FI (1) | FI4278132T3 (en) |
| HR (1) | HRP20250489T1 (en) |
| HU (1) | HUE071337T2 (en) |
| LT (1) | LT4278132T (en) |
| PL (1) | PL4278132T3 (en) |
| PT (1) | PT4278132T (en) |
| SI (1) | SI4278132T1 (en) |
| WO (1) | WO2022152622A1 (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102663869B1 (en) * | 2022-01-18 | 2024-05-03 | 두산에너빌리티 주식회사 | Nozzle for combustor, combustor, and gas turbine including the same |
| EP4317779A1 (en) * | 2022-08-01 | 2024-02-07 | BDR Thermea Group B.V. | Retrofit kit assembly |
| EP4544235A1 (en) | 2022-06-22 | 2025-04-30 | BDR Thermea Group B.V. | Retrofit kit assembly |
| EP4317777A1 (en) * | 2022-08-01 | 2024-02-07 | BDR Thermea Group B.V. | Retrofit kit assembly |
| EP4317778A1 (en) * | 2022-08-01 | 2024-02-07 | BDR Thermea Group B.V. | Retrofit kit assembly |
| EP4317780A1 (en) * | 2022-08-01 | 2024-02-07 | BDR Thermea Group B.V. | Retrofit kit assembly |
| US12379108B2 (en) | 2023-01-06 | 2025-08-05 | Ge Vernova Infrastructure Technology Llc | Method of operating gas turbine combustor with multiple fuel stages |
| US20240230094A1 (en) * | 2023-01-06 | 2024-07-11 | Ge Infrastructure Technology Llc | Combustor head end section with integrated cooling system |
| US11867400B1 (en) * | 2023-02-02 | 2024-01-09 | Pratt & Whitney Canada Corp. | Combustor with fuel plenum with mixing passages having baffles |
| US20250347413A1 (en) * | 2024-05-09 | 2025-11-13 | Ge Infrastructure Technology Llc | Axial fuel stage injector with multiple mixing chambers, and combustor and gt system including same |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4100733A (en) | 1976-10-04 | 1978-07-18 | United Technologies Corporation | Premix combustor |
| DE2950535A1 (en) * | 1979-11-23 | 1981-06-11 | BBC AG Brown, Boveri & Cie., Baden, Aargau | COMBUSTION CHAMBER OF A GAS TURBINE WITH PRE-MIXING / PRE-EVAPORATING ELEMENTS |
| EP0059490B1 (en) * | 1981-03-04 | 1984-12-12 | BBC Aktiengesellschaft Brown, Boveri & Cie. | Annular combustion chamber with an annular burner for gas turbines |
| US6267585B1 (en) | 1995-12-19 | 2001-07-31 | Daimlerchrysler Aerospace Airbus Gmbh | Method and combustor for combusting hydrogen |
| US7416571B2 (en) * | 2005-03-09 | 2008-08-26 | Conocophillips Company | Compact mixer for the mixing of gaseous hydrocarbon and gaseous oxidants |
| 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 |
| US8424311B2 (en) | 2009-02-27 | 2013-04-23 | General Electric Company | Premixed direct injection disk |
| US8276385B2 (en) * | 2009-10-08 | 2012-10-02 | General Electric Company | Staged multi-tube premixing injector |
| US8800289B2 (en) * | 2010-09-08 | 2014-08-12 | General Electric Company | Apparatus and method for mixing fuel in a gas turbine nozzle |
| US8984887B2 (en) * | 2011-09-25 | 2015-03-24 | General Electric Company | Combustor and method for supplying fuel to a combustor |
| US9004912B2 (en) * | 2011-11-11 | 2015-04-14 | General Electric Company | Combustor and method for supplying fuel to a combustor |
| US8438851B1 (en) * | 2012-01-03 | 2013-05-14 | General Electric Company | Combustor assembly for use in a turbine engine and methods of assembling same |
| US20130232979A1 (en) | 2012-03-12 | 2013-09-12 | General Electric Company | System for enhancing mixing in a multi-tube fuel nozzle |
| US9677766B2 (en) * | 2012-11-28 | 2017-06-13 | General Electric Company | Fuel nozzle for use in a turbine engine and method of assembly |
| US9476592B2 (en) | 2013-09-19 | 2016-10-25 | General Electric Company | System for injecting fuel in a gas turbine combustor |
| US9435540B2 (en) * | 2013-12-11 | 2016-09-06 | General Electric Company | Fuel injector with premix pilot nozzle |
| CN106461211B (en) | 2014-05-30 | 2019-03-22 | 川崎重工业株式会社 | Combustion device of gas turbine engine |
| US9759426B2 (en) | 2014-07-31 | 2017-09-12 | General Electric Company | Combustor nozzles in gas turbine engines |
| DE102015003920A1 (en) * | 2014-09-25 | 2016-03-31 | Dürr Systems GmbH | Burner head of a burner and gas turbine with such a burner |
| US10309653B2 (en) * | 2016-03-04 | 2019-06-04 | General Electric Company | Bundled tube fuel nozzle with internal cooling |
| US10295190B2 (en) * | 2016-11-04 | 2019-05-21 | General Electric Company | Centerbody injector mini mixer fuel nozzle assembly |
| JP6822894B2 (en) * | 2017-04-28 | 2021-01-27 | 三菱パワー株式会社 | Fuel injector and gas turbine |
| EP3425281B1 (en) * | 2017-07-04 | 2020-09-02 | General Electric Company | Pilot nozzle with inline premixing |
-
2021
- 2021-01-12 EP EP21151199.3A patent/EP4027059A1/en not_active Withdrawn
-
2022
- 2022-01-07 DK DK22700316.7T patent/DK4278132T3/en active
- 2022-01-07 FI FIEP22700316.7T patent/FI4278132T3/en active
- 2022-01-07 SI SI202230120T patent/SI4278132T1/en unknown
- 2022-01-07 LT LTEPPCT/EP2022/050242T patent/LT4278132T/en unknown
- 2022-01-07 PL PL22700316.7T patent/PL4278132T3/en unknown
- 2022-01-07 EP EP22700316.7A patent/EP4278132B1/en active Active
- 2022-01-07 ES ES22700316T patent/ES3026507T3/en active Active
- 2022-01-07 PT PT227003167T patent/PT4278132T/en unknown
- 2022-01-07 HU HUE22700316A patent/HUE071337T2/en unknown
- 2022-01-07 HR HRP20250489TT patent/HRP20250489T1/en unknown
- 2022-01-07 CA CA3204173A patent/CA3204173A1/en active Pending
- 2022-01-07 US US18/261,062 patent/US20240060644A1/en active Pending
- 2022-01-07 WO PCT/EP2022/050242 patent/WO2022152622A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| HRP20250489T1 (en) | 2025-06-20 |
| DK4278132T3 (en) | 2025-05-19 |
| PL4278132T3 (en) | 2025-07-07 |
| CA3204173A1 (en) | 2022-07-21 |
| US20240060644A1 (en) | 2024-02-22 |
| EP4278132B1 (en) | 2025-03-05 |
| PT4278132T (en) | 2025-05-06 |
| ES3026507T3 (en) | 2025-06-11 |
| FI4278132T3 (en) | 2025-05-20 |
| LT4278132T (en) | 2025-05-12 |
| EP4278132A1 (en) | 2023-11-22 |
| EP4027059A1 (en) | 2022-07-13 |
| WO2022152622A1 (en) | 2022-07-21 |
| HUE071337T2 (en) | 2025-08-28 |
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