PL4298382T3 - Sposób wtryskiwania wodoru do komory spalania zespołu komory spalania układu turbiny gazowej - Google Patents
Sposób wtryskiwania wodoru do komory spalania zespołu komory spalania układu turbiny gazowejInfo
- Publication number
- PL4298382T3 PL4298382T3 PL22709906.6T PL22709906T PL4298382T3 PL 4298382 T3 PL4298382 T3 PL 4298382T3 PL 22709906 T PL22709906 T PL 22709906T PL 4298382 T3 PL4298382 T3 PL 4298382T3
- Authority
- PL
- Poland
- Prior art keywords
- combustor
- combustion chamber
- gas turbine
- turbine system
- injecting hydrogen
- 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
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
- F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
- F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
-
- 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
- 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
- F23R3/36—Supply of different fuels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/35—Combustors or associated equipment
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
- F23C2900/9901—Combustion process using hydrogen, hydrogen peroxide water or brown gas as fuel
-
- 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]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Hydrogen, Water And Hydrids (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US202163153620P | 2021-02-25 | 2021-02-25 | |
| US17/678,134 US11808457B2 (en) | 2021-02-25 | 2022-02-23 | Hydrogen injection for enhanced combustion stability in gas turbine systems |
| PCT/US2022/017674 WO2022182853A1 (en) | 2021-02-25 | 2022-02-24 | Hydrogen injection for enhanced combustion stability in gas turbine systems |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL4298382T3 true PL4298382T3 (pl) | 2025-10-20 |
Family
ID=80735779
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL22709906.6T PL4298382T3 (pl) | 2021-02-25 | 2022-02-24 | Sposób wtryskiwania wodoru do komory spalania zespołu komory spalania układu turbiny gazowej |
Country Status (11)
| Country | Link |
|---|---|
| EP (1) | EP4298382B1 (pl) |
| JP (2) | JP7667294B2 (pl) |
| KR (2) | KR20250141856A (pl) |
| CN (1) | CN116917667B (pl) |
| CA (1) | CA3207755A1 (pl) |
| ES (1) | ES3035533T3 (pl) |
| HU (1) | HUE072683T2 (pl) |
| MX (1) | MX2023009016A (pl) |
| PL (1) | PL4298382T3 (pl) |
| SA (1) | SA523450230B1 (pl) |
| WO (1) | WO2022182853A1 (pl) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115839506B (zh) * | 2022-12-26 | 2024-06-25 | 西安交通大学 | 一种富氢燃料低排放分层旋流燃烧室 |
| WO2026048395A1 (ja) * | 2024-08-30 | 2026-03-05 | 国立研究開発法人宇宙航空研究開発機構 | 燃料噴射器、燃焼器、ガスタービン、及び燃焼器システム |
| CN119554662B (zh) * | 2025-01-03 | 2026-04-07 | 中国航发湖南动力机械研究所 | 氢燃料分级燃烧单元、全环燃烧室及航空发动机 |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5265851A (en) * | 1975-11-28 | 1977-05-31 | Matsushita Electric Industrial Co Ltd | Trimmer capacitor |
| US6096261A (en) * | 1997-11-20 | 2000-08-01 | Praxair Technology, Inc. | Coherent jet injector lance |
| CN100570216C (zh) * | 2005-06-24 | 2009-12-16 | 株式会社日立制作所 | 喷烧器、燃气轮机燃烧器、喷烧器的冷却方法及喷烧器的改造方法 |
| JP4728176B2 (ja) * | 2005-06-24 | 2011-07-20 | 株式会社日立製作所 | バーナ、ガスタービン燃焼器及びバーナの冷却方法 |
| US20100162711A1 (en) | 2008-12-30 | 2010-07-01 | General Electric Compnay | Dln dual fuel primary nozzle |
| EP2955445B1 (en) * | 2014-06-12 | 2019-11-27 | Kawasaki Jukogyo Kabushiki Kaisha | Multifuel gas turbine combustor |
| WO2015200346A1 (en) * | 2014-06-23 | 2015-12-30 | Air Products And Chemicals, Inc. | Solid fuel burner and method of operating |
| JP2019512661A (ja) | 2016-03-15 | 2019-05-16 | ケラー,ジェイ | 非予混合スワールバーナ先端及び燃焼戦略 |
| ES2975239T3 (es) | 2018-05-15 | 2024-07-04 | Air Prod & Chem | Sistema de combustión y procedimiento de funcionamiento de un sistema de combustión |
-
2022
- 2022-02-24 PL PL22709906.6T patent/PL4298382T3/pl unknown
- 2022-02-24 EP EP22709906.6A patent/EP4298382B1/en active Active
- 2022-02-24 MX MX2023009016A patent/MX2023009016A/es unknown
- 2022-02-24 WO PCT/US2022/017674 patent/WO2022182853A1/en not_active Ceased
- 2022-02-24 JP JP2023552113A patent/JP7667294B2/ja active Active
- 2022-02-24 CN CN202280014871.1A patent/CN116917667B/zh active Active
- 2022-02-24 HU HUE22709906A patent/HUE072683T2/hu unknown
- 2022-02-24 CA CA3207755A patent/CA3207755A1/en active Pending
- 2022-02-24 KR KR1020257031596A patent/KR20250141856A/ko active Pending
- 2022-02-24 ES ES22709906T patent/ES3035533T3/es active Active
- 2022-02-24 KR KR1020237026298A patent/KR102884260B1/ko active Active
-
2023
- 2023-08-08 SA SA523450230A patent/SA523450230B1/ar unknown
-
2025
- 2025-04-10 JP JP2025064940A patent/JP2025100688A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| WO2022182853A1 (en) | 2022-09-01 |
| CN116917667B (zh) | 2026-03-10 |
| EP4298382B1 (en) | 2025-04-02 |
| JP2024508474A (ja) | 2024-02-27 |
| JP2025100688A (ja) | 2025-07-03 |
| CN116917667A (zh) | 2023-10-20 |
| EP4298382A1 (en) | 2024-01-03 |
| SA523450230B1 (ar) | 2024-11-20 |
| JP7667294B2 (ja) | 2025-04-22 |
| KR20250141856A (ko) | 2025-09-29 |
| KR102884260B1 (ko) | 2025-11-10 |
| ES3035533T3 (en) | 2025-09-04 |
| HUE072683T2 (hu) | 2025-12-28 |
| KR20230128100A (ko) | 2023-09-01 |
| CA3207755A1 (en) | 2022-09-01 |
| MX2023009016A (es) | 2023-08-08 |
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