SE0000896L - Anordning för styrning av flödesseparationslinjen hos raketmunstycken - Google Patents

Anordning för styrning av flödesseparationslinjen hos raketmunstycken

Info

Publication number
SE0000896L
SE0000896L SE0000896A SE0000896A SE0000896L SE 0000896 L SE0000896 L SE 0000896L SE 0000896 A SE0000896 A SE 0000896A SE 0000896 A SE0000896 A SE 0000896A SE 0000896 L SE0000896 L SE 0000896L
Authority
SE
Sweden
Prior art keywords
controlling
separation line
flow separation
rocket nozzles
nozzle
Prior art date
Application number
SE0000896A
Other languages
Unknown language ( )
English (en)
Other versions
SE516049C2 (sv
SE0000896D0 (sv
Inventor
Arne Boman
Original Assignee
Volvo Aero Corp
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 Volvo Aero Corp filed Critical Volvo Aero Corp
Priority to SE0000896A priority Critical patent/SE516049C2/sv
Publication of SE0000896D0 publication Critical patent/SE0000896D0/sv
Priority to PCT/SE2001/000554 priority patent/WO2001069069A1/en
Priority to UA2001117854A priority patent/UA69452C2/uk
Priority to US09/980,456 priority patent/US6574952B2/en
Priority to DE60108015T priority patent/DE60108015T2/de
Priority to CNB018005489A priority patent/CN1177999C/zh
Priority to RU2001133734/06A priority patent/RU2262613C2/ru
Priority to EP01915997A priority patent/EP1179131B1/en
Priority to AU42941/01A priority patent/AU4294101A/en
Priority to JP2001567924A priority patent/JP4570309B2/ja
Priority to ES01915997T priority patent/ES2233616T3/es
Publication of SE0000896L publication Critical patent/SE0000896L/sv
Publication of SE516049C2 publication Critical patent/SE516049C2/sv

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97—Rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Testing Of Engines (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Jet Pumps And Other Pumps (AREA)
SE0000896A 2000-03-17 2000-03-17 Anordning för styrning av flödesseparationslinjen hos raketmunstycken SE516049C2 (sv)

Priority Applications (11)

Application Number Priority Date Filing Date Title
SE0000896A SE516049C2 (sv) 2000-03-17 2000-03-17 Anordning för styrning av flödesseparationslinjen hos raketmunstycken
ES01915997T ES2233616T3 (es) 2000-03-17 2001-03-16 Aparato para el control de la linea de sepracion de flujo de las toberas de cohetes.
DE60108015T DE60108015T2 (de) 2000-03-17 2001-03-16 Einrichtung zur beeinflussung der ablösungsgrenze bei raketendüsen
UA2001117854A UA69452C2 (uk) 2000-03-17 2001-03-16 Пристрій для управління лінією відриву потоку в ракетних соплах
US09/980,456 US6574952B2 (en) 2000-03-17 2001-03-16 Apparatus for controlling the flow separation line of rocket nozzles
PCT/SE2001/000554 WO2001069069A1 (en) 2000-03-17 2001-03-16 An apparatus for controlling the flow separation line of rocket nozzles
CNB018005489A CN1177999C (zh) 2000-03-17 2001-03-16 一种用于对火箭发动机喷嘴中的气流分隔线进行控制的装置
RU2001133734/06A RU2262613C2 (ru) 2000-03-17 2001-03-16 Устройство для регулирования линии разделения потока сопел реактивных двигателей
EP01915997A EP1179131B1 (en) 2000-03-17 2001-03-16 An apparatus for controlling the flow separation line of rocket nozzles
AU42941/01A AU4294101A (en) 2000-03-17 2001-03-16 An apparatus for controlling the flow separation line of rocket nozzles
JP2001567924A JP4570309B2 (ja) 2000-03-17 2001-03-16 ロッケトノズルのフローセパレーションラインを制御する装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0000896A SE516049C2 (sv) 2000-03-17 2000-03-17 Anordning för styrning av flödesseparationslinjen hos raketmunstycken

Publications (3)

Publication Number Publication Date
SE0000896D0 SE0000896D0 (sv) 2000-03-17
SE0000896L true SE0000896L (sv) 2001-09-18
SE516049C2 SE516049C2 (sv) 2001-11-12

Family

ID=20278855

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0000896A SE516049C2 (sv) 2000-03-17 2000-03-17 Anordning för styrning av flödesseparationslinjen hos raketmunstycken

Country Status (11)

Country Link
US (1) US6574952B2 (sv)
EP (1) EP1179131B1 (sv)
JP (1) JP4570309B2 (sv)
CN (1) CN1177999C (sv)
AU (1) AU4294101A (sv)
DE (1) DE60108015T2 (sv)
ES (1) ES2233616T3 (sv)
RU (1) RU2262613C2 (sv)
SE (1) SE516049C2 (sv)
UA (1) UA69452C2 (sv)
WO (1) WO2001069069A1 (sv)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103444556A (zh) * 2013-08-17 2013-12-18 东瑞食品集团有限公司 一种高床发酵型养猪系统

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080098741A1 (en) * 2006-10-25 2008-05-01 United Technologies Corporation Annular isolator dual mode scramjet engine
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3585800A (en) * 1967-07-27 1971-06-22 Aerojet General Co Transpiration-cooled devices
DE2022517A1 (de) * 1970-05-08 1971-11-25 Messerschmitt Boelkow Blohm Raketentriebwerksduese mit Grenzschichtabsaugung
US3925982A (en) * 1973-09-11 1975-12-16 Martin Marietta Corp Fluid-dynamic shock ring for controlled flow separation in a rocket engine exhaust nozzle
US5619851A (en) * 1989-02-08 1997-04-15 United Technologies Corporation Rocket nozzle for a rocket engine
FR2691209B1 (fr) * 1992-05-18 1995-09-01 Europ Propulsion Enceinte contenant des gaz chauds refroidie par transpiration, notamment chambre propulsive de moteur-fusee, et procede de fabrication.
FR2705737B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à divergent échancré.
US6176077B1 (en) * 1996-02-12 2001-01-23 Volvo Aero Corporation Rocket engine nozzle
RU2117814C1 (ru) * 1996-10-30 1998-08-20 Владимир Ильич Масютин Оптимальное сопло жидкостного ракетного двигателя ракет стратегического назначения

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103444556A (zh) * 2013-08-17 2013-12-18 东瑞食品集团有限公司 一种高床发酵型养猪系统

Also Published As

Publication number Publication date
UA69452C2 (uk) 2004-09-15
EP1179131B1 (en) 2004-12-29
US20020152752A1 (en) 2002-10-24
SE516049C2 (sv) 2001-11-12
ES2233616T3 (es) 2005-06-16
AU4294101A (en) 2001-09-24
WO2001069069A1 (en) 2001-09-20
CN1364217A (zh) 2002-08-14
DE60108015D1 (de) 2005-02-03
US6574952B2 (en) 2003-06-10
CN1177999C (zh) 2004-12-01
JP4570309B2 (ja) 2010-10-27
RU2262613C2 (ru) 2005-10-20
SE0000896D0 (sv) 2000-03-17
EP1179131A1 (en) 2002-02-13
JP2003527528A (ja) 2003-09-16
DE60108015T2 (de) 2005-12-08

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Legal Events

Date Code Title Description
NUG Patent has lapsed