MX365812B - Aparato y método para controlar un combustor de ganancia de presión. - Google Patents

Aparato y método para controlar un combustor de ganancia de presión.

Info

Publication number
MX365812B
MX365812B MX2013012584A MX2013012584A MX365812B MX 365812 B MX365812 B MX 365812B MX 2013012584 A MX2013012584 A MX 2013012584A MX 2013012584 A MX2013012584 A MX 2013012584A MX 365812 B MX365812 B MX 365812B
Authority
MX
Mexico
Prior art keywords
combustor
fuel injector
fuel
setting
control signal
Prior art date
Application number
MX2013012584A
Other languages
English (en)
Other versions
MX2013012584A (es
Inventor
Farshchian Soheil
Original Assignee
Exponential Tech Inc
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
Application filed by Exponential Tech Inc filed Critical Exponential Tech Inc
Publication of MX2013012584A publication Critical patent/MX2013012584A/es
Publication of MX365812B publication Critical patent/MX365812B/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling combustion
    • F23N5/20—Systems for controlling combustion with a time programme acting through electrical means, e.g. using time-delay relays
    • 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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/10—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect
    • 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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/10—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect
    • F02C5/11—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect using valveless combustion chambers
    • 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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • 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
    • F02K7/02—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 the jet being intermittent, i.e. pulse-jet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling 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
    • F23R7/00—Intermittent or explosive combustion chambers
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D7/00—Control of flow
    • G05D7/06—Control of flow characterised by the use of electric means
    • G05D7/0617—Control of flow characterised by the use of electric means specially adapted for fluid materials
    • 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 
    • F23C2205/00—Pulsating combustion
    • F23C2205/10—Pulsating combustion with pulsating fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling combustion
    • F23N5/18—Systems for controlling combustion using detectors sensitive to rate of flow of air or fuel
    • F23N2005/181—Systems for controlling combustion using detectors sensitive to rate of flow of air or fuel using detectors sensitive to rate of flow of air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling combustion
    • F23N5/18—Systems for controlling combustion using detectors sensitive to rate of flow of air or fuel
    • F23N2005/185—Systems for controlling combustion using detectors sensitive to rate of flow of air or fuel using detectors sensitive to rate of flow of fuel
    • 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)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Regulation And Control Of Combustion (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

Un método para controlar la operación de un combustor de ganancia de presión que comprende: determinar un ciclo de operación del inyector de combustible y una frecuencia de combustión que cumple con un valor determinado de carga de objetivo y una fracción de llenado de objetivo del combustor; determinar un ajuste de presión del suministro de combustible, un ajuste de sincronización del inyector de combustible y un ajuste de sincronización de encendido que logra el ciclo de operación del inyector de combustible y frecuencia de combustión determinados; y enviar una señal de control de presión del suministro de combustible con el ajuste de presión del suministro de combustible hacia un medio de presurización de combustible del combustor, una señal de control del inyector de combustible con el ajuste de sincronización del inyector de combustible hacia un inyector de combustible del combustor, y una señal de control de sincronización de encendido con el ajuste de sincronización de encendido a un ensamble de encendido del combustor.
MX2013012584A 2011-04-29 2012-04-27 Aparato y método para controlar un combustor de ganancia de presión. MX365812B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201161481117P 2011-04-29 2011-04-29
PCT/CA2012/000405 WO2012145836A1 (en) 2011-04-29 2012-04-27 Apparatus and method for controlling a pressure gain combustor

Publications (2)

Publication Number Publication Date
MX2013012584A MX2013012584A (es) 2014-09-01
MX365812B true MX365812B (es) 2019-06-12

Family

ID=47071519

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2013012584A MX365812B (es) 2011-04-29 2012-04-27 Aparato y método para controlar un combustor de ganancia de presión.

Country Status (8)

Country Link
US (1) US10451275B2 (es)
EP (1) EP2702258A4 (es)
JP (1) JP6038885B2 (es)
CN (1) CN103688037B (es)
CA (1) CA2834285C (es)
MX (1) MX365812B (es)
RU (1) RU2594845C2 (es)
WO (1) WO2012145836A1 (es)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013134475A1 (en) * 2012-03-07 2013-09-12 Waters Technologies Corporation Limiting a rate of pressurization in a pressurized flow system having a configurable system volume
DK2850364T3 (da) * 2012-03-29 2021-11-15 Pureteq As Anordning til forbrænding af flydende brændstof
US10060618B2 (en) 2012-11-07 2018-08-28 Exponential Technologies, Inc. Pressure-gain combustion apparatus and method
DE102013010706B3 (de) * 2013-06-27 2014-11-20 Airbus Defence and Space GmbH Hochfrequenzstabilisierte Verbrennung in Fluggasturbinen
CA2980285C (en) 2015-03-19 2024-06-18 University Of Maryland, College Park Systems and methods for anti-phase operation of pulse combustors
CN105180205B (zh) * 2015-08-14 2017-08-25 中国神华能源股份有限公司 富氧燃烧烟气循环系统控制方法
US10557438B2 (en) 2015-12-18 2020-02-11 North American Wave Engine Corporation Systems and methods for air-breathing wave engines for thrust production
US10627111B2 (en) * 2017-03-27 2020-04-21 United Technologies Coproration Rotating detonation engine multi-stage mixer
US10436110B2 (en) 2017-03-27 2019-10-08 United Technologies Corporation Rotating detonation engine upstream wave arrestor
EP3781868B1 (en) 2018-04-17 2022-11-30 North American Wave Engine Corporation Method and apparatus for the start-up and control of pulse combustors using selective injector operation
US11421601B2 (en) 2019-03-28 2022-08-23 Woodward, Inc. Second stage combustion for igniter
US11578661B2 (en) * 2019-09-19 2023-02-14 Pratt & Whitney Canada Corp. Systems and methods for starting a gas turbine engine
EP4168661A1 (en) * 2020-06-23 2023-04-26 Woodward, Inc. Ignition system for power generation engine
CN113553675B (zh) * 2021-07-29 2022-12-13 上海电力大学 一种喷射器优化方法及装置
CN113777215B (zh) * 2021-09-26 2023-08-25 西安航天动力研究所 一种用于射流助爆研究的试验装置

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4819873A (en) * 1986-04-16 1989-04-11 Nea Technologies, Inc. Method and apparatus for combusting fuel in a pulse combustor
US4767313A (en) * 1986-04-16 1988-08-30 Nea Technologies, Inc. Pulse combustion energy system
US5123835A (en) * 1991-03-04 1992-06-23 The United States Of America As Represented By The United States Department Of Energy Pulse combustor with controllable oscillations
US5349811A (en) * 1992-12-16 1994-09-27 Avco Corporation Pulsed fuel injection system for reducing NOx emissions
US6505462B2 (en) 2001-03-29 2003-01-14 General Electric Company Rotary valve for pulse detonation engines
RU2285142C2 (ru) * 2003-12-02 2006-10-10 Игорь Васильевич Гаранин Способ работы и устройство энергосиловой детонационной установки
JP2005176553A (ja) * 2003-12-12 2005-06-30 Jfe Engineering Kk 複合発電方法及び装置
US7637096B2 (en) * 2004-11-25 2009-12-29 Rolls-Royce Plc Pulse jet engine having pressure sensor means for controlling fuel delivery into a combustion chamber
KR101307032B1 (ko) * 2005-06-22 2013-09-11 엘리멘트 식스 리미티드 고등급의 색을 갖는 다이아몬드 층
JP2007016608A (ja) * 2005-07-05 2007-01-25 Ishikawajima Harima Heavy Ind Co Ltd パルスデトネーション回転駆動装置
RU2300004C2 (ru) * 2005-08-12 2007-05-27 Константин Валентинович Мигалин Пульсирующий воздушно-реактивный двигатель
US20070180814A1 (en) * 2006-02-03 2007-08-09 General Electric Company Direct liquid fuel injection and ignition for a pulse detonation combustor
US7758334B2 (en) * 2006-03-28 2010-07-20 Purdue Research Foundation Valveless pulsed detonation combustor
US8292022B2 (en) * 2006-04-17 2012-10-23 Soundblast Technologies Llc System and method for generating and controlling conducted acoustic waves for geophysical exploration
RU64707U1 (ru) * 2006-09-06 2007-07-10 Виталий Николаевич Федорец Детонационный двигатель с непрерывным циклом работы
US8726630B2 (en) * 2006-12-01 2014-05-20 General Electric Company System and method for passive valving for pulse detonation combustors
US20090133377A1 (en) * 2007-11-15 2009-05-28 General Electric Company Multi-tube pulse detonation combustor based engine
AT506592B1 (de) * 2008-08-26 2009-10-15 Edmund Ing Lorenz Verbrennungsturbine mit diskontinuierlicher verbrennung
US8602758B2 (en) 2008-09-17 2013-12-10 Exponential Technologies, Inc. Indexed positive displacement rotary motion device
US20100154380A1 (en) * 2008-12-22 2010-06-24 General Electric Company Control system for a land-based simple cycle hybrid engine for power generation
US9732600B2 (en) 2009-08-27 2017-08-15 Exponential Technologies, Inc. Heating apparatus
US20110126511A1 (en) * 2009-11-30 2011-06-02 General Electric Company Thrust modulation in a multiple combustor pulse detonation engine using cross-combustor detonation initiation
US8683780B2 (en) * 2010-12-28 2014-04-01 Masayoshi Shimo Gas turbine engine and pulse detonation combustion system

Also Published As

Publication number Publication date
JP6038885B2 (ja) 2016-12-07
CA2834285C (en) 2019-09-03
US10451275B2 (en) 2019-10-22
RU2013153337A (ru) 2015-08-10
CA2834285A1 (en) 2012-11-01
MX2013012584A (es) 2014-09-01
RU2594845C2 (ru) 2016-08-20
US20140260294A1 (en) 2014-09-18
JP2014515088A (ja) 2014-06-26
CN103688037A (zh) 2014-03-26
WO2012145836A1 (en) 2012-11-01
EP2702258A4 (en) 2015-02-25
CN103688037B (zh) 2016-05-04
EP2702258A1 (en) 2014-03-05

Similar Documents

Publication Publication Date Title
MX365812B (es) Aparato y método para controlar un combustor de ganancia de presión.
WO2012115941A3 (en) Variable gas substitution for dual fuel engine and method
WO2012103112A3 (en) Em energy application for combustion engines
WO2010076645A8 (en) High operation repeatability and stability fuel injection system for an internal combustion engine
WO2009075335A1 (ja) ガスタービンの制御方法およびガスタービン発電装置
WO2013076564A8 (en) Control apparatus for internal combustion engine and control method of internal combustion engine
WO2012051122A3 (en) Method and apparatus for converting diesel engines to blended gaseous and diesel fuel engines
WO2014008062A3 (en) Systems and methods for low-power lamp compatibility with a leading-edge dimmer and a magnetic transformer
GB201309361D0 (en) Method for operating an engine
MX343101B (es) Dispositivo de control remoto para vehiculo.
WO2013118151A3 (en) A system and method for controlling the ignition timing of an internal combustion engine
GB201208936D0 (en) An engine and a method of operating a direct injection engine
MX2019010633A (es) Sistema y metodo para la combustion de combustibles solidos y sus derivados.
WO2012107013A3 (de) Axialkolbenmotor sowie verfahren zum betrieb eines axialkolbenmotors
IN2012DN01963A (es)
WO2014200677A3 (en) System and method for control of fuel injector spray
GB201516977D0 (en) A Fuel Injector For A Gas Turbine Engine Combustion Chamber
GB2566877A (en) Fuel heating
HK1215724A1 (zh) 用於在內燃機運行中修正利用燃料噴射裝置噴射的燃料量的方法
IN2014DE01003A (es)
MX2020001785A (es) Sistema de horno y metodo para operar un horno.
PL406238A1 (pl) Sposób i układ do wytwarzania energii poprzez recykling materiałów podczas procesu spalania paliwa
MX2015001831A (es) Procedimiento y sistema para reducir la cantidad de combustible en vehículos equipados con inyectores de combustible y que se pueden abastecer con mas de un combustible.
PL2721347T3 (pl) Sposób wtryskiwania paliwa do komory spalania turbiny gazowej oraz układ wtryskowy do realizacji tego sposobu
WO2015110893A8 (en) Method and apparatus for controlling fuel injection of an internal combustion engine

Legal Events

Date Code Title Description
FG Grant or registration