EA200200936A1 - Двигатель с кумулятивным зарядом - Google Patents
Двигатель с кумулятивным зарядомInfo
- Publication number
- EA200200936A1 EA200200936A1 EA200200936A EA200200936A EA200200936A1 EA 200200936 A1 EA200200936 A1 EA 200200936A1 EA 200200936 A EA200200936 A EA 200200936A EA 200200936 A EA200200936 A EA 200200936A EA 200200936 A1 EA200200936 A1 EA 200200936A1
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- charge
- released
- forming chamber
- hole
- compression zone
- Prior art date
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
-
- 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
-
- 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
- F05D2250/232—Three-dimensional prismatic conical
-
- 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
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/292—Three-dimensional machined; miscellaneous tapered
-
- 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
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/712—Shape curved concave
-
- 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)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
Двигатель с кумулятивным зарядом включает в себя кольцевую формирующую заряд камеру (3), образованную посредством соединения внутреннего (1) и внешнего (2) корпусов. Центральное сквозное отверстие во внутреннем корпусе позволяет выпускать выхлопные газы. Внешний корпус содержит, в основном, круглый диск с внутренним коническим вогнутым углублением и сквозные отверстия для введения топлива и воспламенения. Формирующая заряд камера имеет предпочтительно коническую форму, более широкую при основании и постепенно суживающуюся по площади поперечного сечения при поднятии в вершине. Эта конструкция образует кольцевую точку смыкания или сужение по направлению к вершине, которое создает первичную зону сжатия. Вторичная зона сжатия создается на вершине внешнего корпуса как раз за сужением, создавая гиперзвуковые газы, по мере того как в основном противоположно направленные потоки выхлопных газов сталкиваются и выпускаются через сквозное отверстие во внутреннем корпусе. Двигатель с кумулятивным зарядом может быть использован в многочисленных применениях, включая как устройство импульсного непосредственного двигателя, так и силовой привод турбины, или многочисленные инструменты и приспособления.Международная заявка была опубликована вместе с отчетом о международном поиске.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/517,130 US6430919B1 (en) | 2000-03-02 | 2000-03-02 | Shaped charged engine |
PCT/US2001/006617 WO2001065103A1 (en) | 2000-03-02 | 2001-03-02 | Shaped charge engine |
Publications (2)
Publication Number | Publication Date |
---|---|
EA200200936A1 true EA200200936A1 (ru) | 2003-02-27 |
EA004390B1 EA004390B1 (ru) | 2004-04-29 |
Family
ID=24058482
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EA200200936A EA004390B1 (ru) | 2000-03-02 | 2001-03-02 | Двигатель с кумулятивным зарядом |
Country Status (11)
Country | Link |
---|---|
US (3) | US6430919B1 (ru) |
EP (1) | EP1264100A4 (ru) |
JP (1) | JP2004500515A (ru) |
KR (1) | KR20030025908A (ru) |
CN (1) | CN1522339A (ru) |
AU (1) | AU2001274804A1 (ru) |
BR (1) | BR0108902A (ru) |
CA (1) | CA2401759A1 (ru) |
EA (1) | EA004390B1 (ru) |
MX (1) | MXPA02008619A (ru) |
WO (1) | WO2001065103A1 (ru) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080000215A1 (en) * | 2000-03-02 | 2008-01-03 | Duncan Ronnie J | Engine systems and methods |
US6874452B2 (en) | 2002-01-15 | 2005-04-05 | Joseph S. Adams | Resonant combustion chamber and recycler for linear motors |
JP4618612B2 (ja) * | 2004-03-29 | 2011-01-26 | 国立大学法人横浜国立大学 | パルスデトネーションエンジン着火方法及びその装置 |
US20090090110A1 (en) * | 2007-10-04 | 2009-04-09 | Honeywell International, Inc. | Faceted dome assemblies for gas turbine engine combustors |
GB2519155B (en) * | 2013-10-11 | 2016-10-12 | Reaction Engines Ltd | Engine |
CN104373247B (zh) * | 2014-09-26 | 2016-06-22 | 汤广武 | 内爆式推动器 |
IT202100001439A1 (it) * | 2021-01-26 | 2022-07-26 | Sidereus Space Dynamics S R L | Motore a razzo a doppia modalità di funzionamento e metodo di funzionamento di detto motore |
CN117869126A (zh) * | 2024-03-12 | 2024-04-12 | 西安航天动力研究所 | 一种火箭发动机燃烧室的直流式点火结构 |
Family Cites Families (36)
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US864821A (en) * | 1905-05-22 | 1907-09-03 | Heinrich Zoelly | Explosive-turbine. |
US2810261A (en) * | 1952-10-15 | 1957-10-22 | Plessey Co Ltd | Combustion control system |
US2951339A (en) * | 1959-03-31 | 1960-09-06 | United Aircraft Corp | Combustion chamber swirler |
DE1233207B (de) * | 1960-06-29 | 1967-01-26 | Klein Hans Christof | Vorrichtung zur periodischen Erzeugung von hochverdichtetem Arbeitsgas fuer Waermekraftmaschinen |
US3185871A (en) * | 1961-07-20 | 1965-05-25 | Jr Albert G Bodine | Alternating current magnetohydrodynamic generator |
US4034673A (en) | 1976-02-23 | 1977-07-12 | Calspan Corporation | Armor penetration shaped-charge projectile |
US4170110A (en) | 1976-07-19 | 1979-10-09 | Edward Radin | Combustion process |
US4074858A (en) | 1976-11-01 | 1978-02-21 | Institute Of Gas Technology | High pressure pulsed water jet apparatus and process |
US4510748A (en) | 1979-11-05 | 1985-04-16 | Adams Joseph S | Compression wave former |
JPS5853690A (ja) | 1981-09-25 | 1983-03-30 | Jidosha Kiki Co Ltd | ベ−ンポンプ |
US4938112A (en) | 1984-06-22 | 1990-07-03 | Washington Research Foundation | Apparatus and method for the acceleration of projectiles to hypervelocities |
DE3661224D1 (en) * | 1985-02-26 | 1988-12-22 | Bbc Brown Boveri & Cie | Gas turbine combustor |
FR2661454B1 (fr) | 1985-07-12 | 1994-02-11 | Onera | Perfectionnements apportes aux propulseurs de type statoreacteur. |
US4726184A (en) | 1985-09-09 | 1988-02-23 | Rockwell International Corporation | Rocket engine assembly |
FR2588372B1 (fr) | 1985-10-08 | 1989-07-13 | Thomson Brandt Armements | Dispositif de pilotage pour projectile guide au moyen de tuyeres laterales |
DE3603497C1 (de) | 1986-02-05 | 1993-01-07 | Rheinmetall Gmbh | Geschoss fuer eine Panzerabwehrwaffe zur Bekaempfung eines Panzers von oben |
US4724738A (en) | 1986-04-22 | 1988-02-16 | Johnson Family Enterprises | Space entry actuator launch system |
CH672366A5 (ru) * | 1986-12-09 | 1989-11-15 | Bbc Brown Boveri & Cie | |
GB8701578D0 (en) | 1987-01-24 | 1987-02-25 | Jaguar Cars | Supercharging i c engines |
JP2565988B2 (ja) | 1988-07-29 | 1996-12-18 | 株式会社東芝 | 連結式パルス燃焼装置 |
US5052176A (en) | 1988-09-28 | 1991-10-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Combination turbojet-ramjet-rocket propulsion system |
US5090891A (en) | 1989-06-26 | 1992-02-25 | Indugas, Inc. | Hybrid combustion device and system therefor |
FR2656382B1 (fr) | 1989-12-21 | 1994-07-08 | Europ Propulsion | Moteur a propulsion combinee a haute adaptabilite pour aeronef ou avion spatial. |
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US5194690A (en) | 1990-02-21 | 1993-03-16 | Teledyne Industries, Inc. | Shock compression jet gun |
US5111746A (en) | 1991-06-21 | 1992-05-12 | The United States Of America As Represented By The Secretary Of The Army | Multiple stage munition |
US5345758A (en) | 1993-04-14 | 1994-09-13 | Adroit Systems, Inc. | Rotary valve multiple combustor pulse detonation engine |
US6003301A (en) | 1993-04-14 | 1999-12-21 | Adroit Systems, Inc. | Exhaust nozzle for multi-tube detonative engines |
US5901550A (en) | 1993-04-14 | 1999-05-11 | Adroit Systems, Inc. | Liquid fueled pulse detonation engine with controller and inlet and exit valves |
US5873240A (en) | 1993-04-14 | 1999-02-23 | Adroit Systems, Inc. | Pulsed detonation rocket engine |
US5557926A (en) | 1994-06-24 | 1996-09-24 | Lockheed-Martin | Pulse detonation apparatus with inner and outer Spherical valves |
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FR2734025B1 (fr) * | 1995-05-11 | 1997-08-01 | Europ Propulsion | Moteur fusee a propergol liquide, a impulsions |
US6000214A (en) | 1996-07-08 | 1999-12-14 | Scragg; Robert L. | Detonation cycle gas turbine engine system having intermittent fuel and air delivery |
US5831155A (en) | 1996-12-02 | 1998-11-03 | Atlantic Research Corporation | Apparatus and method for simulating rocket-to-ramjet transition in a propulsion system |
US5890459A (en) | 1997-09-12 | 1999-04-06 | Southwest Research Institute | System and method for a dual fuel, direct injection combustion engine |
-
2000
- 2000-03-02 US US09/517,130 patent/US6430919B1/en not_active Expired - Fee Related
-
2001
- 2001-03-02 EP EP01941451A patent/EP1264100A4/en not_active Withdrawn
- 2001-03-02 CN CNA018089151A patent/CN1522339A/zh active Pending
- 2001-03-02 EA EA200200936A patent/EA004390B1/ru not_active IP Right Cessation
- 2001-03-02 AU AU2001274804A patent/AU2001274804A1/en not_active Abandoned
- 2001-03-02 BR BR0108902-1A patent/BR0108902A/pt not_active IP Right Cessation
- 2001-03-02 CA CA002401759A patent/CA2401759A1/en not_active Abandoned
- 2001-03-02 KR KR1020027011503A patent/KR20030025908A/ko not_active Application Discontinuation
- 2001-03-02 JP JP2001563775A patent/JP2004500515A/ja active Pending
- 2001-03-02 MX MXPA02008619A patent/MXPA02008619A/es unknown
- 2001-03-02 WO PCT/US2001/006617 patent/WO2001065103A1/en not_active Application Discontinuation
-
2002
- 2002-06-14 US US10/172,406 patent/US6658838B2/en not_active Expired - Fee Related
-
2003
- 2003-10-15 US US10/687,452 patent/US20040134184A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EA004390B1 (ru) | 2004-04-29 |
US20030046920A1 (en) | 2003-03-13 |
US6658838B2 (en) | 2003-12-09 |
EP1264100A1 (en) | 2002-12-11 |
BR0108902A (pt) | 2003-12-09 |
EP1264100A4 (en) | 2003-09-10 |
US6430919B1 (en) | 2002-08-13 |
AU2001274804A1 (en) | 2001-09-12 |
JP2004500515A (ja) | 2004-01-08 |
CN1522339A (zh) | 2004-08-18 |
MXPA02008619A (es) | 2004-09-06 |
CA2401759A1 (en) | 2001-09-07 |
KR20030025908A (ko) | 2003-03-29 |
WO2001065103A1 (en) | 2001-09-07 |
US20040134184A1 (en) | 2004-07-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PD1A | Registration of transfer to a eurasian application by order of succession in title | ||
MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): AM AZ BY KZ KG MD TJ TM RU |