LT4278132T - Degiklis - Google Patents

Degiklis

Info

Publication number
LT4278132T
LT4278132T LTEPPCT/EP2022/050242T LTEP2022050242T LT4278132T LT 4278132 T LT4278132 T LT 4278132T LT EP2022050242 T LTEP2022050242 T LT EP2022050242T LT 4278132 T LT4278132 T LT 4278132T
Authority
LT
Lithuania
Prior art keywords
burner
Prior art date
Application number
LTEPPCT/EP2022/050242T
Other languages
English (en)
Lithuanian (lt)
Inventor
Jaan Hellat
Wolfgang Dieter KAPPIS
Sriwickrama Prithiviraj HARASGAMA
Franklin Marie Georges Martin GENIN
Khawar Syed
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=LT4278132(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 LT4278132T publication Critical patent/LT4278132T/lt

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)
LTEPPCT/EP2022/050242T 2021-01-12 2022-01-07 Degiklis LT4278132T (lt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP21151199.3A EP4027059A1 (de) 2021-01-12 2021-01-12 Brenner, brennkammer und verfahren zum nachrüsten eines verbrennungsgerätes
PCT/EP2022/050242 WO2022152622A1 (en) 2021-01-12 2022-01-07 Burner

Publications (1)

Publication Number Publication Date
LT4278132T true LT4278132T (lt) 2025-05-12

Family

ID=74180944

Family Applications (1)

Application Number Title Priority Date Filing Date
LTEPPCT/EP2022/050242T LT4278132T (lt) 2021-01-12 2022-01-07 Degiklis

Country Status (13)

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

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 (de) * 2022-08-01 2024-02-07 BDR Thermea Group B.V. Nachrüstkitanordnung
EP4317779A1 (de) * 2022-08-01 2024-02-07 BDR Thermea Group B.V. Nachrüstkitanordnung
EP4317777A1 (de) * 2022-08-01 2024-02-07 BDR Thermea Group B.V. Nachrüstkitanordnung
EP4317778A1 (de) * 2022-08-01 2024-02-07 BDR Thermea Group B.V. Nachrüstkitanordnung
EP4544228A1 (de) 2022-06-22 2025-04-30 BDR Thermea Group B.V. Wasserstoffnachrüstsatzanordnung für eine gasverbrennungsvorrichtung
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 (de) * 1981-03-04 1984-12-12 BBC Aktiengesellschaft Brown, Boveri & Cie. Ringbrennkammer mit Ringbrenner für Gasturbinen
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 (en) 2014-05-30 2015-12-03 Kawasaki Jukogyo Kabushiki Kaisha Combustor for gas turbine engine
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 (de) * 2017-07-04 2020-09-02 General Electric Company Pilotdüse mit inline-vormischung
US11156360B2 (en) * 2019-02-18 2021-10-26 General Electric Company Fuel nozzle assembly

Also Published As

Publication number Publication date
EP4278132A1 (de) 2023-11-22
PL4278132T3 (pl) 2025-07-07
US20240060644A1 (en) 2024-02-22
HUE071337T2 (hu) 2025-08-28
PT4278132T (pt) 2025-05-06
FI4278132T3 (fi) 2025-05-20
HRP20250489T1 (hr) 2025-06-20
SI4278132T1 (sl) 2025-06-30
ES3026507T3 (en) 2025-06-11
WO2022152622A1 (en) 2022-07-21
EP4027059A1 (de) 2022-07-13
EP4278132B1 (de) 2025-03-05
DK4278132T3 (da) 2025-05-19
CA3204173A1 (en) 2022-07-21

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