BR0315240A - Injetor de combustìvel - Google Patents
Injetor de combustìvelInfo
- Publication number
- BR0315240A BR0315240A BR0315240-5A BR0315240A BR0315240A BR 0315240 A BR0315240 A BR 0315240A BR 0315240 A BR0315240 A BR 0315240A BR 0315240 A BR0315240 A BR 0315240A
- Authority
- BR
- Brazil
- Prior art keywords
- fuel
- fuel injector
- chamber
- distributor
- outlets
- Prior art date
Links
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
- F23R3/02—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
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
-
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
-
- 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
-
- 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
- F05D2210/00—Working fluids
- F05D2210/40—Flow geometry or direction
- F05D2210/43—Radial inlet and axial outlet
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/231—Three-dimensional prismatic cylindrical
-
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/33—Arrangement of components symmetrical
Abstract
"INJETOR DE COMBUSTìVEL". A presente invenção refere-se a um injetor de combustível (1), compreendendo uma câmara (7) com uma entrada de combustível (8) e uma pluralidade de saídas de combustível (10), e compreendendo um distribuidor de combustível (18) que é disposto na câmara (7) com o propósito de distribuir o combustível introduzido na câmara (7) através da entrada de combustível (8) para as saídas (10). O distribuidor de combustível (18) compreende um corpo distribuidor genericamente simétrico giratório.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US31960102P | 2002-10-10 | 2002-10-10 | |
SE0202997A SE524736C2 (sv) | 2002-10-10 | 2002-10-10 | Bränsleinsprutare med bränslefördelare och motor med bränsleinsprutare |
PCT/SE2003/001479 WO2004033966A1 (en) | 2002-10-10 | 2003-09-23 | A fuel injector |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0315240A true BR0315240A (pt) | 2005-08-23 |
Family
ID=32095519
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR0315240-5A BR0315240A (pt) | 2002-10-10 | 2003-09-23 | Injetor de combustìvel |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP1554524B1 (pt) |
JP (1) | JP4365321B2 (pt) |
AT (1) | ATE439556T1 (pt) |
AU (1) | AU2003263715A1 (pt) |
BR (1) | BR0315240A (pt) |
DE (1) | DE60328810D1 (pt) |
PL (1) | PL205541B1 (pt) |
WO (1) | WO2004033966A1 (pt) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115653759A (zh) * | 2022-10-13 | 2023-01-31 | 中国航发四川燃气涡轮研究院 | 基于流量分配的加力燃烧室供油系统及控制流程设计方法 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3002353A (en) | 1957-12-19 | 1961-10-03 | Gen Electric | Fuel injector for a combustion chamber |
US2978870A (en) | 1957-12-26 | 1961-04-11 | Gen Electric | Fuel injector for a combustion chamber |
GB2158570B (en) * | 1984-05-10 | 1988-11-30 | Ex Cell O Corp | Mechanically operated fuel control system |
US4887425A (en) * | 1988-03-18 | 1989-12-19 | General Electric Company | Fuel spraybar |
EP0963534B1 (en) * | 1997-12-08 | 2003-02-26 | Volvo Aero Corporation | A flameholder device for afterburners in gas turbine engines |
-
2003
- 2003-09-23 BR BR0315240-5A patent/BR0315240A/pt not_active IP Right Cessation
- 2003-09-23 WO PCT/SE2003/001479 patent/WO2004033966A1/en active Application Filing
- 2003-09-23 JP JP2004542944A patent/JP4365321B2/ja not_active Expired - Fee Related
- 2003-09-23 PL PL375014A patent/PL205541B1/pl not_active IP Right Cessation
- 2003-09-23 EP EP03808011A patent/EP1554524B1/en not_active Expired - Lifetime
- 2003-09-23 AT AT03808011T patent/ATE439556T1/de not_active IP Right Cessation
- 2003-09-23 AU AU2003263715A patent/AU2003263715A1/en not_active Abandoned
- 2003-09-23 DE DE60328810T patent/DE60328810D1/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
AU2003263715A1 (en) | 2004-05-04 |
DE60328810D1 (de) | 2009-09-24 |
PL375014A1 (en) | 2005-11-14 |
EP1554524B1 (en) | 2009-08-12 |
EP1554524A1 (en) | 2005-07-20 |
JP2006502369A (ja) | 2006-01-19 |
WO2004033966A1 (en) | 2004-04-22 |
PL205541B1 (pl) | 2010-04-30 |
JP4365321B2 (ja) | 2009-11-18 |
ATE439556T1 (de) | 2009-08-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06A | Patent application procedure suspended [chapter 6.1 patent gazette] | ||
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 11A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2272 DE 22/07/2014. |