BR112012031715A2 - motor de detonação em pulso de multitubos sem válvula - Google Patents

motor de detonação em pulso de multitubos sem válvula

Info

Publication number
BR112012031715A2
BR112012031715A2 BR112012031715A BR112012031715A BR112012031715A2 BR 112012031715 A2 BR112012031715 A2 BR 112012031715A2 BR 112012031715 A BR112012031715 A BR 112012031715A BR 112012031715 A BR112012031715 A BR 112012031715A BR 112012031715 A2 BR112012031715 A2 BR 112012031715A2
Authority
BR
Brazil
Prior art keywords
blasting
tubes
valve
air
detonation
Prior art date
Application number
BR112012031715A
Other languages
English (en)
Inventor
Alejandro Juan
Kristjan Gottfried
Original Assignee
Exponential Technologies 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 Technologies Inc filed Critical Exponential Technologies Inc
Publication of BR112012031715A2 publication Critical patent/BR112012031715A2/pt

Links

Classifications

    • 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
    • F02K7/04—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 with resonant 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
    • 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
    • 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
    • F02K7/06—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 with combustion chambers having valves
    • F02K7/067—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 with combustion chambers having valves having aerodynamic valves
    • 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 
    • F23C15/00—Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass
    • 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
    • F23C2900/03004—Tubular combustion chambers with swirling fuel/air flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Characterised By The Charging Evacuation (AREA)

Abstract

motor de detonação em pulso de multitubos sem válvula. é revelado um motor de detonação em pulso de multitubos sem vãlvula incluindo uma pluralidade de tubos de detonação onde cada tubo de detonação compreende uma saída de descarga independente, e a pluralidade de tubos de detonação interconectada a um orificio comum de mistura ar/combustível. no motor revelado, uma mistura ar/combustível é detonada nos tubos de detonação simultaneamente, e o orifício comum de entrada de mistura ar/combustível minimiza comtra pressão causada pela detonação da mistura ar/combustível por direcional múltiplas ondas de choque inversas uma contra outra e usar efetivamente as contrapressões como superfícies de reação recíprocas e efetivamente reduzir o efeito de ondas de choque de retorno em movimentação para montante. os tubos de detonação podem ser não lineares, e podem ter descargas independentes. as descargas independentes podem ser acopladas a um bocal adaptador terminando em uma saída de escape combinada.
BR112012031715A 2010-06-15 2011-06-15 motor de detonação em pulso de multitubos sem válvula BR112012031715A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US35482910P 2010-06-15 2010-06-15
PCT/CA2011/050362 WO2011156923A2 (en) 2010-06-15 2011-06-15 Multitube valveless pulse detonation engine

Publications (1)

Publication Number Publication Date
BR112012031715A2 true BR112012031715A2 (pt) 2016-11-01

Family

ID=45095080

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012031715A BR112012031715A2 (pt) 2010-06-15 2011-06-15 motor de detonação em pulso de multitubos sem válvula

Country Status (6)

Country Link
US (1) US9359973B2 (pt)
JP (1) JP5892622B2 (pt)
CN (1) CN103069142B (pt)
BR (1) BR112012031715A2 (pt)
CA (1) CA2803247A1 (pt)
WO (1) WO2011156923A2 (pt)

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CN110159431B (zh) * 2019-05-24 2024-08-20 长沙市云智航科技有限公司 一种多气缸的涡轮旋转式发动机
CN111207009B (zh) * 2019-12-26 2023-01-13 中国空气动力研究与发展中心 利用外加瞬时能量源在超声速气流中起爆斜爆震波的方法
CN111120144B (zh) * 2020-01-07 2021-01-05 姚长水 自适应变频互控式脉冲爆震航空发动机及其使用方法
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Also Published As

Publication number Publication date
CN103069142B (zh) 2016-08-03
RU2012157366A (ru) 2014-07-20
CN103069142A (zh) 2013-04-24
US20110302908A1 (en) 2011-12-15
JP2013528777A (ja) 2013-07-11
JP5892622B2 (ja) 2016-03-23
CA2803247A1 (en) 2011-12-22
WO2011156923A2 (en) 2011-12-22
WO2011156923A3 (en) 2012-02-02
US9359973B2 (en) 2016-06-07

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Legal Events

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B08F Application fees: dismissal - article 86 of industrial property law
B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)