JP6176772B2 - 局所的な屈曲波修正機構を備えたパルスデトネーション管 - Google Patents

局所的な屈曲波修正機構を備えたパルスデトネーション管 Download PDF

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Publication number
JP6176772B2
JP6176772B2 JP2011208870A JP2011208870A JP6176772B2 JP 6176772 B2 JP6176772 B2 JP 6176772B2 JP 2011208870 A JP2011208870 A JP 2011208870A JP 2011208870 A JP2011208870 A JP 2011208870A JP 6176772 B2 JP6176772 B2 JP 6176772B2
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Japan
Prior art keywords
tube
pulse detonation
detonation
bending wave
wave
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Japanese (ja)
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JP2012078083A5 (enExample
JP2012078083A (ja
Inventor
マイケル・モスキンスキ
アダム・ラシード
ブライアン・ジーン・ブルゼク
ナレンドラ・ディガンバル・ジョシ
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General Electric Co
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General Electric Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/02Plants 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Incineration Of Waste (AREA)
JP2011208870A 2010-09-30 2011-09-26 局所的な屈曲波修正機構を備えたパルスデトネーション管 Expired - Fee Related JP6176772B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/895,368 2010-09-30
US12/895,368 US8707674B2 (en) 2010-09-30 2010-09-30 Pulse detonation tube with local flexural wave modifying feature

Publications (3)

Publication Number Publication Date
JP2012078083A JP2012078083A (ja) 2012-04-19
JP2012078083A5 JP2012078083A5 (enExample) 2014-10-30
JP6176772B2 true JP6176772B2 (ja) 2017-08-09

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ID=44677753

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011208870A Expired - Fee Related JP6176772B2 (ja) 2010-09-30 2011-09-26 局所的な屈曲波修正機構を備えたパルスデトネーション管

Country Status (4)

Country Link
US (1) US8707674B2 (enExample)
EP (1) EP2436903A2 (enExample)
JP (1) JP6176772B2 (enExample)
CA (1) CA2753033A1 (enExample)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012061742A1 (en) 2010-11-05 2012-05-10 ThermoChem Recovery International Solids circulation system and method for capture and conversion of reactive solids
US9499404B2 (en) 2011-09-27 2016-11-22 Thermochem Recovery International, Inc. System and method for syngas clean-up
CN103953459B (zh) * 2014-04-21 2016-06-08 西北工业大学 一种短距起爆高频爆震波的装置及其控制方法
ES2940894T3 (es) 2016-02-16 2023-05-12 Thermochem Recovery Int Inc Sistema y método de generación de gas producto de energía integrada de dos etapas
WO2017164888A1 (en) 2016-03-25 2017-09-28 Thermochem Recovery International, Inc. Three-stage energy-integrated product gas generation system and method
US10364398B2 (en) 2016-08-30 2019-07-30 Thermochem Recovery International, Inc. Method of producing product gas from multiple carbonaceous feedstock streams mixed with a reduced-pressure mixing gas
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
US9920926B1 (en) 2017-07-10 2018-03-20 Thermochem Recovery International, Inc. Pulse combustion heat exchanger system and method
US10099200B1 (en) 2017-10-24 2018-10-16 Thermochem Recovery International, Inc. Liquid fuel production system having parallel product gas generation
RU2684352C1 (ru) * 2018-07-16 2019-04-08 Общество С Ограниченной Ответственностью "Пульсирующие Детонационные Технологии" Регулируемое пульсирующее газодинамическое детонационное резонаторное выходное устройство для получения тяги
CN109915281B (zh) * 2019-03-06 2021-03-19 西北工业大学 一种有益于壁面冷却与起爆的脉冲爆震火箭发动机供油方案
US11555157B2 (en) 2020-03-10 2023-01-17 Thermochem Recovery International, Inc. System and method for liquid fuel production from carbonaceous materials using recycled conditioned syngas
RU2742319C1 (ru) * 2020-07-17 2021-02-04 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Способ работы детонационного ракетного двигателя
US11466223B2 (en) 2020-09-04 2022-10-11 Thermochem Recovery International, Inc. Two-stage syngas production with separate char and product gas inputs into the second stage
CN113153570B (zh) * 2021-05-27 2023-09-22 中国航空发动机研究院 一种脉冲爆震管性能计算方法和装置
RU207457U1 (ru) * 2021-07-26 2021-10-28 Общество С Ограниченной Ответственностью "Пульсирующие Детонационные Технологии" Выходное устройство двигателя прямой реакции
CN115822812B (zh) * 2022-12-21 2024-11-26 西北工业大学 脉冲爆震发动机多孔促爆主爆震室及促爆方法
CN119354406B (zh) * 2024-10-22 2025-12-19 西北工业大学 一种固定爆震波曲率损失的装置与方法

Family Cites Families (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US866330A (en) * 1906-11-24 1907-09-17 Almeron E Calkins Motor.
US1035454A (en) * 1909-03-29 1912-08-13 Isaac N Lewis Internal-combustion power apparatus.
US1980266A (en) * 1931-02-07 1934-11-13 Robert H Goddard Propulsion apparatus
US1856552A (en) * 1931-06-26 1932-05-03 Hadamik Frank Carbide rocket
US2523379A (en) * 1945-11-28 1950-09-26 Kollsman Paul Combustion products generator with combustion type precompressor
US2601471A (en) * 1947-05-22 1952-06-24 Vang Alfred Jet propulsion means having vibrator therein
US2677232A (en) * 1948-06-05 1954-05-04 Continental Aviat & Engineerin Combination pulse jet and ram jet engine
US2834181A (en) * 1950-10-07 1958-05-13 Snecma Jet propulsion unit comprising pulse jet units having ejector tubes within a ramjet unit
US2799136A (en) * 1951-04-09 1957-07-16 Phillips Petroleum Co Flame detection and control in aircraft engines
US2860484A (en) * 1956-06-04 1958-11-18 Schmidt Paul Apparatus for causing intermittent combustion of a fuel in a chamber as a means of producing useful energy
US3210930A (en) * 1962-02-01 1965-10-12 Atlantic Res Corp Gas generator
US3188805A (en) * 1963-02-14 1965-06-15 Charles L Gahagan Internal combustion engine
US3293852A (en) * 1963-03-19 1966-12-27 Boeing Co Plasma propulsion method and means
US3264824A (en) * 1964-10-16 1966-08-09 Warren J Bost Pulse jet reaction motor having intermittent combustion
US3449913A (en) * 1968-01-29 1969-06-17 John J Grebe Combustion process
JPH10141430A (ja) * 1996-11-06 1998-05-29 Toshiba Corp 器具載置塔
US6347509B1 (en) * 1999-07-15 2002-02-19 Mcdonnell Douglas Corporation C/O The Boeing Company Pulsed detonation engine with ejector bypass
US6584765B1 (en) * 2001-12-21 2003-07-01 United Technologies Corporation Pulse detonation engine having an aerodynamic valve
US6877310B2 (en) * 2002-03-27 2005-04-12 General Electric Company Shock wave reflector and detonation chamber
US7055308B2 (en) * 2003-05-30 2006-06-06 General Electric Company Detonation damper for pulse detonation engines
JP4411050B2 (ja) * 2003-10-29 2010-02-10 東邦瓦斯株式会社 ガスタービン装置
US6983586B2 (en) * 2003-12-08 2006-01-10 General Electric Company Two-stage pulse detonation system
GB0409664D0 (en) * 2004-04-30 2004-06-02 Denne William A Ultrasonic pulse jet engine
US20050279083A1 (en) * 2004-06-18 2005-12-22 General Electric Company Folded detonation initiator for constant volume combustion device
US7818956B2 (en) * 2005-05-13 2010-10-26 General Electric Company Pulse detonation assembly and hybrid engine
US7828546B2 (en) * 2005-06-30 2010-11-09 General Electric Company Naturally aspirated fluidic control for diverting strong pressure waves
US7669405B2 (en) * 2005-12-22 2010-03-02 General Electric Company Shaped walls for enhancement of deflagration-to-detonation transition
US20090320439A1 (en) * 2006-01-31 2009-12-31 General Electric Company Pulsed detonation combustor cleaning device and method of operation
US7966803B2 (en) * 2006-02-03 2011-06-28 General Electric Company Pulse detonation combustor with folded flow path
JP2008202906A (ja) * 2007-02-22 2008-09-04 General Electric Co <Ge> パルスデトネーション燃焼器清浄化装置および運転方法
JP2008272622A (ja) * 2007-04-26 2008-11-13 Tama Tlo Kk 溶射装置
JP5142873B2 (ja) * 2008-07-29 2013-02-13 カヤバ工業株式会社 緩衝器
US20110302904A1 (en) * 2010-06-11 2011-12-15 General Electric Company Pulsed Detonation Cleaning Device with Multiple Folded Flow Paths
US8881500B2 (en) * 2010-08-31 2014-11-11 General Electric Company Duplex tab obstacles for enhancement of deflagration-to-detonation transition
US20120192545A1 (en) * 2011-01-28 2012-08-02 General Electric Company Pulse Detonation Combustor Nozzles

Also Published As

Publication number Publication date
US20120079806A1 (en) 2012-04-05
CA2753033A1 (en) 2012-03-30
US8707674B2 (en) 2014-04-29
JP2012078083A (ja) 2012-04-19
EP2436903A2 (en) 2012-04-04

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