PT4278132T - Queimador - Google Patents

Queimador

Info

Publication number
PT4278132T
PT4278132T PT227003167T PT22700316T PT4278132T PT 4278132 T PT4278132 T PT 4278132T PT 227003167 T PT227003167 T PT 227003167T PT 22700316 T PT22700316 T PT 22700316T PT 4278132 T PT4278132 T PT 4278132T
Authority
PT
Portugal
Prior art keywords
burner
Prior art date
Application number
PT227003167T
Other languages
English (en)
Portuguese (pt)
Original Assignee
Crosstown H2R Ag
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=74180944&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=PT4278132(T) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Crosstown H2R Ag filed Critical Crosstown H2R Ag
Publication of PT4278132T publication Critical patent/PT4278132T/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002Gas turbine combustors adapted for fuels having low heating value [LHV]
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00016Retrofitting 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)
PT227003167T 2021-01-12 2022-01-07 Queimador PT4278132T (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP21151199.3A EP4027059A1 (fr) 2021-01-12 2021-01-12 Bruleur, chambre de combustion et procede d'adaptation d'un appareil de combustion

Publications (1)

Publication Number Publication Date
PT4278132T true PT4278132T (pt) 2025-05-06

Family

ID=74180944

Family Applications (1)

Application Number Title Priority Date Filing Date
PT227003167T PT4278132T (pt) 2021-01-12 2022-01-07 Queimador

Country Status (13)

Country Link
US (1) US20240060644A1 (fr)
EP (2) EP4027059A1 (fr)
CA (1) CA3204173A1 (fr)
DK (1) DK4278132T3 (fr)
ES (1) ES3026507T3 (fr)
FI (1) FI4278132T3 (fr)
HR (1) HRP20250489T1 (fr)
HU (1) HUE071337T2 (fr)
LT (1) LT4278132T (fr)
PL (1) PL4278132T3 (fr)
PT (1) PT4278132T (fr)
SI (1) SI4278132T1 (fr)
WO (1) WO2022152622A1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102663869B1 (ko) * 2022-01-18 2024-05-03 두산에너빌리티 주식회사 연소기용 노즐, 연소기 및 이를 포함하는 가스 터빈
EP4317780A1 (fr) * 2022-08-01 2024-02-07 BDR Thermea Group B.V. Ensemble kit de rattrapage
EP4317779A1 (fr) * 2022-08-01 2024-02-07 BDR Thermea Group B.V. Ensemble kit de rattrapage
EP4317777A1 (fr) * 2022-08-01 2024-02-07 BDR Thermea Group B.V. Ensemble kit de rattrapage
EP4317778A1 (fr) * 2022-08-01 2024-02-07 BDR Thermea Group B.V. Ensemble kit de rattrapage
EP4544228A1 (fr) 2022-06-22 2025-04-30 BDR Thermea Group B.V. Ensemble kit de modernisation à hydrogène pour un appareil de combustion de gaz
US12379108B2 (en) 2023-01-06 2025-08-05 Ge Vernova Infrastructure Technology Llc Method of operating gas turbine combustor with multiple fuel stages
US12305860B2 (en) 2023-01-06 2025-05-20 Ge Vernova Infrastructure Technology Llc Bundled tube fuel nozzle assembly for gas turbine combustor
US11867400B1 (en) * 2023-02-02 2024-01-09 Pratt & Whitney Canada Corp. Combustor with fuel plenum with mixing passages having baffles
US12601490B2 (en) * 2024-05-09 2026-04-14 Ge Infrastructure Technology Llc Axial fuel stage injector with multiple mixing chambers, and combustor and GT system including same

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4100733A (en) 1976-10-04 1978-07-18 United Technologies Corporation Premix combustor
DE2950535A1 (de) * 1979-11-23 1981-06-11 BBC AG Brown, Boveri & Cie., Baden, Aargau Brennkammer einer gasturbine mit vormisch/vorverdampf-elementen
EP0059490B1 (fr) * 1981-03-04 1984-12-12 BBC Aktiengesellschaft Brown, Boveri & Cie. Chambre de combustion annulaire avec brûleur annulaire pour turbines à gaz
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 (ja) * 2007-11-29 2012-03-28 株式会社日立製作所 バーナ,燃焼装置及び燃焼装置の改造方法
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
WO2015182154A1 (fr) 2014-05-30 2015-12-03 Kawasaki Jukogyo Kabushiki Kaisha Chambre de combustion pour turbine à gaz
US9759426B2 (en) 2014-07-31 2017-09-12 General Electric Company Combustor nozzles in gas turbine engines
DE102015003920A1 (de) * 2014-09-25 2016-03-31 Dürr Systems GmbH Brennerkopf eines Brenners und Gasturbine mit einem solchen Brenner
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 (ja) * 2017-04-28 2021-01-27 三菱パワー株式会社 燃料噴射器及びガスタービン
EP3425281B1 (fr) * 2017-07-04 2020-09-02 General Electric Company Buse pilote dotée de prémélange en ligne
US11156360B2 (en) * 2019-02-18 2021-10-26 General Electric Company Fuel nozzle assembly

Also Published As

Publication number Publication date
EP4278132A1 (fr) 2023-11-22
PL4278132T3 (pl) 2025-07-07
US20240060644A1 (en) 2024-02-22
HUE071337T2 (hu) 2025-08-28
FI4278132T3 (fi) 2025-05-20
HRP20250489T1 (hr) 2025-06-20
SI4278132T1 (sl) 2025-06-30
ES3026507T3 (en) 2025-06-11
WO2022152622A1 (fr) 2022-07-21
EP4027059A1 (fr) 2022-07-13
EP4278132B1 (fr) 2025-03-05
DK4278132T3 (da) 2025-05-19
CA3204173A1 (fr) 2022-07-21
LT4278132T (lt) 2025-05-12

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