MX2018012246A - Metodos de suministro de combustible en motor de combustion. - Google Patents
Metodos de suministro de combustible en motor de combustion.Info
- Publication number
- MX2018012246A MX2018012246A MX2018012246A MX2018012246A MX2018012246A MX 2018012246 A MX2018012246 A MX 2018012246A MX 2018012246 A MX2018012246 A MX 2018012246A MX 2018012246 A MX2018012246 A MX 2018012246A MX 2018012246 A MX2018012246 A MX 2018012246A
- Authority
- MX
- Mexico
- Prior art keywords
- fuel
- combustion engine
- fuel supply
- injector
- premixer
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title abstract 15
- 238000002485 combustion reaction Methods 0.000 title abstract 3
- 238000002716 delivery method Methods 0.000 title 1
- 230000000712 assembly Effects 0.000 abstract 2
- 238000000429 assembly Methods 0.000 abstract 2
- 239000000203 mixture Substances 0.000 abstract 1
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
- F23R3/36—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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
-
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
-
- 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
- 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
- F05D2220/70—Application in combination with
- F05D2220/75—Application in combination with equipment using fuel having a low calorific value, e.g. low BTU fuel, waste end, syngas, biomass fuel or flare gas
-
- 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]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E50/00—Technologies for the production of fuel of non-fossil origin
- Y02E50/10—Biofuels, e.g. bio-diesel
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Un inyector de combustible (26) para un motor de combustión (10) incluye un cabezal inyector (28) que incluye una boquilla (44), un premezclador (48), y un distribuidor (70) estructurado para distribuir una pluralidad de diferentes combustibles a los diferentes conjuntos de orificios de abastecimiento de combustible (58, 60, 66, 114, 119) en el premezclador (48). Una unidad piloto (103) del inyector de combustible (26) se acopla al premezclador (48) e incluye un primer paso de abastecimiento de combustible (110) para un primer combustible y un segundo paso de abastecimiento de combustible (111) para un segundo combustible. Los múltiples conjuntos de orificios de abastecimiento de combustible (58, 60, 66, 114, 119) se posicionan dentro del inyector de combustible (26), los conjuntos de orificios de abastecimiento de combustible (58, 60, 66, 114, 119) que pueden conectarse de manera selectiva a una pluralidad de diferentes suministros de combustible (20, 22, 24), y ambos se localizan y dimensionan para acomodar una amplia gama de velocidades de flujo para permitir que un motor de combustión (10) acoplado con el inyector de combustible (26) funcione con los combustibles que tienen una gama de índice de Wobbe y composiciones.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/130,037 US10234142B2 (en) | 2016-04-15 | 2016-04-15 | Fuel delivery methods in combustion engine using wide range of gaseous fuels |
| PCT/US2017/023307 WO2017180295A1 (en) | 2016-04-15 | 2017-03-21 | Fuel delivery methods in combustion engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| MX2018012246A true MX2018012246A (es) | 2019-02-07 |
Family
ID=60038007
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| MX2018012246A MX2018012246A (es) | 2016-04-15 | 2017-03-21 | Metodos de suministro de combustible en motor de combustion. |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US10234142B2 (es) |
| CN (1) | CN108885004B (es) |
| GB (1) | GB2566174A (es) |
| MX (1) | MX2018012246A (es) |
| WO (1) | WO2017180295A1 (es) |
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| CN116917667A (zh) | 2021-02-25 | 2023-10-20 | 气体产品与化学公司 | 用于增强燃气轮机系统中的燃烧稳定性的氢气喷射 |
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-
2016
- 2016-04-15 US US15/130,037 patent/US10234142B2/en active Active
-
2017
- 2017-03-21 GB GB1818502.5A patent/GB2566174A/en not_active Withdrawn
- 2017-03-21 WO PCT/US2017/023307 patent/WO2017180295A1/en not_active Ceased
- 2017-03-21 CN CN201780022705.5A patent/CN108885004B/zh active Active
- 2017-03-21 MX MX2018012246A patent/MX2018012246A/es unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US20170299190A1 (en) | 2017-10-19 |
| WO2017180295A1 (en) | 2017-10-19 |
| CN108885004A (zh) | 2018-11-23 |
| GB201818502D0 (en) | 2018-12-26 |
| GB2566174A (en) | 2019-03-06 |
| CN108885004B (zh) | 2020-12-25 |
| US10234142B2 (en) | 2019-03-19 |
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