BR112013032010A2 - sistema de ignição para um motor estatojato giratório, combinação, sistema de combustão para um motor estatojato giratório, sistema de injeção para um motor estatojato giratório, motor estatojato giratório e turbina de impulso para um motor estatojato giratório - Google Patents
sistema de ignição para um motor estatojato giratório, combinação, sistema de combustão para um motor estatojato giratório, sistema de injeção para um motor estatojato giratório, motor estatojato giratório e turbina de impulso para um motor estatojato giratórioInfo
- Publication number
- BR112013032010A2 BR112013032010A2 BR112013032010A BR112013032010A BR112013032010A2 BR 112013032010 A2 BR112013032010 A2 BR 112013032010A2 BR 112013032010 A BR112013032010 A BR 112013032010A BR 112013032010 A BR112013032010 A BR 112013032010A BR 112013032010 A2 BR112013032010 A2 BR 112013032010A2
- Authority
- BR
- Brazil
- Prior art keywords
- jet engine
- rotary jet
- rotary
- combination
- thrust turbine
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- 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
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
- F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
- F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust
-
- 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
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
-
- 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
- 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
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
-
- 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
- F23R2900/00012—Details of sealing 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
- F23R2900/03343—Pilot burners operating in premixed mode
-
- 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)
- Ignition Installations For Internal Combustion Engines (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
abstract not avaible
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161497569P | 2011-06-16 | 2011-06-16 | |
PCT/CA2012/000502 WO2012171094A1 (en) | 2011-06-16 | 2012-05-25 | Combustion systems and combustion system components for rotary ramjet engines |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112013032010A2 true BR112013032010A2 (pt) | 2016-12-20 |
Family
ID=47356452
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112013032010A BR112013032010A2 (pt) | 2011-06-16 | 2012-05-25 | sistema de ignição para um motor estatojato giratório, combinação, sistema de combustão para um motor estatojato giratório, sistema de injeção para um motor estatojato giratório, motor estatojato giratório e turbina de impulso para um motor estatojato giratório |
Country Status (8)
Country | Link |
---|---|
US (1) | US9702562B2 (pt) |
EP (1) | EP2721273A4 (pt) |
KR (1) | KR20140042859A (pt) |
CN (1) | CN103703229B (pt) |
BR (1) | BR112013032010A2 (pt) |
CA (1) | CA2839456C (pt) |
RU (1) | RU2013157399A (pt) |
WO (1) | WO2012171094A1 (pt) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2849525A1 (en) * | 2011-09-23 | 2013-03-28 | Socpra Sciences Et Genie S.E.C. | Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall |
US11208893B2 (en) | 2015-05-25 | 2021-12-28 | Socpra Sciences Et Genie S.E.C. | High temperature ceramic rotary turbomachinery |
CN104847498B (zh) * | 2015-05-27 | 2016-04-06 | 厦门大学 | 导流驻涡一体化的级间燃烧室 |
US10788213B2 (en) * | 2015-08-27 | 2020-09-29 | Arizona Board Of Regents On Behalf Of Arizona State University | Rayleigh-Taylor assisted combustion with micro-flameholders |
WO2018097832A1 (en) * | 2016-11-25 | 2018-05-31 | Socpra Sciences Et Genie S.E.C. | High g-field combustion |
CA3044942A1 (en) * | 2016-11-25 | 2018-05-31 | Societe De Commercialisation Des Produits De La Recherche Appliquee Socpra Sciences Et Genie S.E.C. | High temperature ceramic rotary turbomachinery |
US10539073B2 (en) | 2017-03-20 | 2020-01-21 | Chester L Richards, Jr. | Centrifugal gas compressor |
US10794331B2 (en) * | 2017-07-31 | 2020-10-06 | The Boeing Company | Scramjets and associated aircraft and methods |
PL243763B1 (pl) * | 2018-01-16 | 2023-10-09 | Politechnika Warszawska | Rotacyjny silnik cieplny |
RU2690236C1 (ru) * | 2018-04-03 | 2019-05-31 | Сергей Евгеньевич Угловский | Сверхзвуковая вращающаяся ракета |
GB201819696D0 (en) * | 2018-12-03 | 2019-01-16 | Rolls Royce Plc | Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine |
GB201819695D0 (en) * | 2018-12-03 | 2019-01-16 | Rolls Royce Plc | Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine |
CN112377323B (zh) * | 2020-10-27 | 2022-12-20 | 中国空气动力研究与发展中心 | 一种应用于降低超燃冲压发动机的燃烧减阻方法及装置 |
US11473505B2 (en) | 2020-11-04 | 2022-10-18 | Delavan Inc. | Torch igniter cooling system |
US11608783B2 (en) | 2020-11-04 | 2023-03-21 | Delavan, Inc. | Surface igniter cooling system |
US11692488B2 (en) | 2020-11-04 | 2023-07-04 | Delavan Inc. | Torch igniter cooling system |
US11635027B2 (en) | 2020-11-18 | 2023-04-25 | Collins Engine Nozzles, Inc. | Fuel systems for torch ignition devices |
US11421602B2 (en) | 2020-12-16 | 2022-08-23 | Delavan Inc. | Continuous ignition device exhaust manifold |
US11635210B2 (en) | 2020-12-17 | 2023-04-25 | Collins Engine Nozzles, Inc. | Conformal and flexible woven heat shields for gas turbine engine components |
US11754289B2 (en) | 2020-12-17 | 2023-09-12 | Delavan, Inc. | Axially oriented internally mounted continuous ignition device: removable nozzle |
US11209164B1 (en) * | 2020-12-18 | 2021-12-28 | Delavan Inc. | Fuel injector systems for torch igniters |
US11680528B2 (en) | 2020-12-18 | 2023-06-20 | Delavan Inc. | Internally-mounted torch igniters with removable igniter heads |
CN114321014A (zh) * | 2021-12-24 | 2022-04-12 | 中国科学院工程热物理研究所 | 一种离心压气机径向扩压器局部自循环流动控制结构 |
CN114234231B (zh) * | 2021-12-27 | 2022-11-22 | 中国航发沈阳发动机研究所 | 一种兼顾雷达隐身外形的火焰稳定器 |
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US1387166A (en) * | 1918-08-05 | 1921-08-09 | Pazos-Martinez Richard | Internal-combustion turbine |
US1388707A (en) * | 1918-10-01 | 1921-08-23 | John O Heinze | Turbine |
US1864741A (en) * | 1923-06-15 | 1932-06-28 | Charles N Koch | Combustion turbine and method of feeding and burning fuel |
US2471892A (en) * | 1944-02-14 | 1949-05-31 | Lockheed Aircraft Corp | Reactive propulsion power plant having radial flow compressor and turbine means |
US2448972A (en) * | 1944-10-20 | 1948-09-07 | Edward W Gizara | Internal-combusstion engine |
US2490064A (en) * | 1945-01-12 | 1949-12-06 | Kollsman Paul | Thermodynamic machine |
US2577918A (en) * | 1946-05-08 | 1951-12-11 | Kellogg M W Co | Air jacketed combustion chamber flame tube |
US2530281A (en) * | 1947-03-26 | 1950-11-14 | Barsby Charles Rutland | Rotary internal-combustion engine |
US2782593A (en) * | 1951-06-08 | 1957-02-26 | United Aircraft Corp | Multi-unit ramjet |
US2655906A (en) * | 1952-08-05 | 1953-10-20 | Holley Carburetor Co | Two-cycle combustion chamber |
US2830439A (en) * | 1954-02-24 | 1958-04-15 | Rolls Royce | Combustion equipment for gas turbines with hot gas extraction and mixing means |
US2979900A (en) * | 1957-11-12 | 1961-04-18 | United Aircraft Corp | Ducted fan flameholder |
US3946553A (en) * | 1975-03-10 | 1976-03-30 | United Technologies Corporation | Two-stage premixed combustor |
US5709076A (en) | 1992-09-14 | 1998-01-20 | Lawlor; Shawn P. | Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall |
US5372005A (en) | 1992-09-14 | 1994-12-13 | Lawler; Shawn P. | Method and apparatus for power generation |
CN1187232A (zh) * | 1995-06-07 | 1998-07-08 | 肖恩·P·劳勒 | 用于产生动力的改进方法和装置 |
AU721469B2 (en) * | 1996-12-16 | 2000-07-06 | Ramgen Power Systems, Llc | Ramjet engine for power generation |
ZA993917B (en) | 1998-06-17 | 2000-01-10 | Ramgen Power Systems Inc | Ramjet engine for power generation. |
AU2341100A (en) | 1998-08-17 | 2000-04-17 | Ramgen Power Systems, Inc. | Apparatus and method for fuel-air mixing before supply of low pressure lean pre-mix to combustor |
US20040016226A1 (en) | 2001-07-23 | 2004-01-29 | Ramgen Power Systems, Inc. | Radial impulse turbine for rotary ramjet engine |
US20030014960A1 (en) | 2001-07-23 | 2003-01-23 | Ramgen Power Systems, Inc. | Impulse turbine for rotary ramjet engine |
US6694743B2 (en) | 2001-07-23 | 2004-02-24 | Ramgen Power Systems, Inc. | Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall |
CA2382382A1 (fr) | 2002-04-16 | 2003-10-16 | Universite De Sherbrooke | Moteur rotatif continu a combustion induite par onde de choc |
US7685824B2 (en) | 2005-09-09 | 2010-03-30 | The Regents Of The University Of Michigan | Rotary ramjet turbo-generator |
EP2475859B1 (en) | 2009-09-10 | 2018-12-05 | The Regents of the University of Michigan | Rayleigh-taylor assisted combustion and combustors adapted to exploit rayleigh-taylor instability for increasing combustion rates therein |
CN101705883A (zh) | 2009-11-12 | 2010-05-12 | 李珊 | 冲压转子发动机 |
US8726670B2 (en) * | 2010-06-24 | 2014-05-20 | General Electric Company | Ejector purge of cavity adjacent exhaust flowpath |
-
2012
- 2012-05-25 CN CN201280036022.2A patent/CN103703229B/zh active Active
- 2012-05-25 WO PCT/CA2012/000502 patent/WO2012171094A1/en active Application Filing
- 2012-05-25 EP EP12800390.2A patent/EP2721273A4/en not_active Withdrawn
- 2012-05-25 KR KR1020147001113A patent/KR20140042859A/ko not_active Application Discontinuation
- 2012-05-25 US US14/126,782 patent/US9702562B2/en active Active
- 2012-05-25 RU RU2013157399/06A patent/RU2013157399A/ru not_active Application Discontinuation
- 2012-05-25 CA CA2839456A patent/CA2839456C/en active Active
- 2012-05-25 BR BR112013032010A patent/BR112013032010A2/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
RU2013157399A (ru) | 2015-07-27 |
US20140290259A1 (en) | 2014-10-02 |
CN103703229B (zh) | 2016-08-31 |
US9702562B2 (en) | 2017-07-11 |
CA2839456C (en) | 2017-06-27 |
EP2721273A1 (en) | 2014-04-23 |
EP2721273A4 (en) | 2015-04-15 |
CN103703229A (zh) | 2014-04-02 |
KR20140042859A (ko) | 2014-04-07 |
WO2012171094A1 (en) | 2012-12-20 |
CA2839456A1 (en) | 2012-12-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |