SE0000895D0 - Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp - Google Patents

Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp

Info

Publication number
SE0000895D0
SE0000895D0 SE0000895A SE0000895A SE0000895D0 SE 0000895 D0 SE0000895 D0 SE 0000895D0 SE 0000895 A SE0000895 A SE 0000895A SE 0000895 A SE0000895 A SE 0000895A SE 0000895 D0 SE0000895 D0 SE 0000895D0
Authority
SE
Sweden
Prior art keywords
nozzle wall
rocket
heat transfer
controlling
type
Prior art date
Application number
SE0000895A
Other languages
English (en)
Other versions
SE0000895L (sv
SE516046C2 (sv
Inventor
Jan Lundgren
Arne Boman
Mats Olofsson
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 SE0000895A priority Critical patent/SE516046C2/sv
Publication of SE0000895D0 publication Critical patent/SE0000895D0/sv
Priority to DE60108016T priority patent/DE60108016T2/de
Priority to EP01915998A priority patent/EP1179132B1/en
Priority to AU42942/01A priority patent/AU4294201A/en
Priority to JP2001567925A priority patent/JP4570310B2/ja
Priority to ES01915998T priority patent/ES2233617T3/es
Priority to CNB018005497A priority patent/CN1178000C/zh
Priority to UA2001117853A priority patent/UA70364C2/uk
Priority to PCT/SE2001/000555 priority patent/WO2001069070A1/en
Priority to RU2001133736/06A priority patent/RU2264555C2/ru
Priority to US09/980,481 priority patent/US6675571B2/en
Publication of SE0000895L publication Critical patent/SE0000895L/sv
Publication of SE516046C2 publication Critical patent/SE516046C2/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)
  • Testing Of Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
SE0000895A 2000-03-17 2000-03-17 Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp SE516046C2 (sv)

Priority Applications (11)

Application Number Priority Date Filing Date Title
SE0000895A SE516046C2 (sv) 2000-03-17 2000-03-17 Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp
US09/980,481 US6675571B2 (en) 2000-03-17 2001-03-16 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines
JP2001567925A JP4570310B2 (ja) 2000-03-17 2001-03-16 膨張サイクル型ロケットエンジンのノズル壁への熱伝達を制御するための装置
EP01915998A EP1179132B1 (en) 2000-03-17 2001-03-16 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines
AU42942/01A AU4294201A (en) 2000-03-17 2001-03-16 Apparatus for controlling the heat transfer to the nozzle wall of expander cyclerocket engines
DE60108016T DE60108016T2 (de) 2000-03-17 2001-03-16 Einrichtung um den wärmeübertrag auf die wände von expansionsdüsen von raketen zu regeln
ES01915998T ES2233617T3 (es) 2000-03-17 2001-03-16 Aparato para controlar la transmision de calor a la pared de la tobera en motores de cohete de ciclo de expansion.
CNB018005497A CN1178000C (zh) 2000-03-17 2001-03-16 用于控制传导到膨胀循环式火箭发动机中喷嘴侧壁上的热量的装置
UA2001117853A UA70364C2 (uk) 2000-03-17 2001-03-16 Пристрій для збільшення переносу тепла до холодоагенту на внутрішній стороні стінки сопел ракетних двигунів з розширювальним циклом
PCT/SE2001/000555 WO2001069070A1 (en) 2000-03-17 2001-03-16 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines
RU2001133736/06A RU2264555C2 (ru) 2000-03-17 2001-03-16 Устройство для регулирования передачи тепла стенке сопла ракетных двигателей с циклом расширения

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0000895A SE516046C2 (sv) 2000-03-17 2000-03-17 Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp

Publications (3)

Publication Number Publication Date
SE0000895D0 true SE0000895D0 (sv) 2000-03-17
SE0000895L SE0000895L (sv) 2001-09-18
SE516046C2 SE516046C2 (sv) 2001-11-12

Family

ID=20278854

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0000895A SE516046C2 (sv) 2000-03-17 2000-03-17 Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp

Country Status (11)

Country Link
US (1) US6675571B2 (sv)
EP (1) EP1179132B1 (sv)
JP (1) JP4570310B2 (sv)
CN (1) CN1178000C (sv)
AU (1) AU4294201A (sv)
DE (1) DE60108016T2 (sv)
ES (1) ES2233617T3 (sv)
RU (1) RU2264555C2 (sv)
SE (1) SE516046C2 (sv)
UA (1) UA70364C2 (sv)
WO (1) WO2001069070A1 (sv)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE512942C2 (sv) * 1998-10-02 2000-06-12 Volvo Aero Corp Förfarande för tillverkning av utloppsmunstycken för raketmotorer
DE10054333B4 (de) 2000-11-02 2006-11-30 Eads Space Transportation Gmbh Brennkammer mit erhöhtem Wärmeeintrag in eine Kühleinrichtung
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2022517A1 (de) 1970-05-08 1971-11-25 Messerschmitt Boelkow Blohm Raketentriebwerksduese mit Grenzschichtabsaugung
JPS62261652A (ja) * 1986-05-07 1987-11-13 Natl Space Dev Agency Japan<Nasda> 液体ロケツトエンジン
US4799543A (en) * 1987-11-12 1989-01-24 Arthur H. Iversen Means for temperature control of heated surfaces
US5410874A (en) * 1990-11-19 1995-05-02 United Technologies Corporation Method and apparatus for increasing combustion chamber pressure in a high pressure expander cycle rocket engine
DE4116396C2 (de) * 1991-05-18 1996-04-25 Grace Gmbh Modifizierte amorphe Kieselsäure, Verfahren zu deren Herstellung und Antiblockingmittel
US5267437A (en) * 1991-05-23 1993-12-07 United Technologies Corporation Dual mode 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.
JPH07243351A (ja) * 1994-03-03 1995-09-19 Mitsubishi Heavy Ind Ltd 流体熱交換装置
US5832719A (en) * 1995-12-18 1998-11-10 United Technologies Corporation Rocket thrust chamber
DE10054333B4 (de) * 2000-11-02 2006-11-30 Eads Space Transportation Gmbh Brennkammer mit erhöhtem Wärmeeintrag in eine Kühleinrichtung

Also Published As

Publication number Publication date
DE60108016D1 (de) 2005-02-03
EP1179132A1 (en) 2002-02-13
SE0000895L (sv) 2001-09-18
DE60108016T2 (de) 2005-12-08
ES2233617T3 (es) 2005-06-16
CN1178000C (zh) 2004-12-01
CN1364218A (zh) 2002-08-14
UA70364C2 (uk) 2004-10-15
WO2001069070A1 (en) 2001-09-20
AU4294201A (en) 2001-09-24
US6675571B2 (en) 2004-01-13
JP4570310B2 (ja) 2010-10-27
EP1179132B1 (en) 2004-12-29
RU2264555C2 (ru) 2005-11-20
US20020134071A1 (en) 2002-09-26
SE516046C2 (sv) 2001-11-12
JP2003527529A (ja) 2003-09-16

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