ATE331133T1 - Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds - Google Patents

Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds

Info

Publication number
ATE331133T1
ATE331133T1 AT02729605T AT02729605T ATE331133T1 AT E331133 T1 ATE331133 T1 AT E331133T1 AT 02729605 T AT02729605 T AT 02729605T AT 02729605 T AT02729605 T AT 02729605T AT E331133 T1 ATE331133 T1 AT E331133T1
Authority
AT
Austria
Prior art keywords
rocket engine
engine element
producing
wall structure
load bearing
Prior art date
Application number
AT02729605T
Other languages
English (en)
Inventor
Jan Haeggander
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
Priority claimed from SE0100078A external-priority patent/SE520268C2/sv
Application filed by Volvo Aero Corp filed Critical Volvo Aero Corp
Application granted granted Critical
Publication of ATE331133T1 publication Critical patent/ATE331133T1/de

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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device making

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Powder Metallurgy (AREA)
  • Testing Of Engines (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
AT02729605T 2001-01-11 2002-01-09 Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds ATE331133T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US26104801P 2001-01-11 2001-01-11
SE0100078A SE520268C2 (sv) 2001-01-11 2001-01-11 Del till en raketmotor för flytande bränsle samt förfarande för framställning av en del till en raketmotor

Publications (1)

Publication Number Publication Date
ATE331133T1 true ATE331133T1 (de) 2006-07-15

Family

ID=26655370

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02729605T ATE331133T1 (de) 2001-01-11 2002-01-09 Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds

Country Status (8)

Country Link
US (1) US6799418B2 (de)
EP (1) EP1352168B1 (de)
JP (1) JP4019217B2 (de)
AT (1) ATE331133T1 (de)
DE (1) DE60212568T2 (de)
ES (1) ES2266498T3 (de)
RU (1) RU2273756C2 (de)
WO (1) WO2002055862A1 (de)

Families Citing this family (8)

* 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
EP1398569A1 (de) * 2002-09-13 2004-03-17 Siemens Aktiengesellschaft Gasturbine
US7596940B2 (en) * 2005-03-22 2009-10-06 Pratt & Whitney Rocketdyne, Inc. Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing
DE102005050118B4 (de) * 2005-10-18 2009-04-09 Werkzeugbau Siegfried Hofmann Gmbh Anordnung zur Temperierung eines metallischen Körpers sowie Verwendung derselben
KR100674118B1 (ko) * 2006-07-07 2007-01-24 (주)씨앤스페이스 로켓 추진용 메탄엔진
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
US20100199626A1 (en) * 2008-12-31 2010-08-12 Benjamin Roland Harding Turbine engine exhaust gas tube mixer
FR3004368B1 (fr) * 2013-04-15 2015-09-25 Aircelle Sa Brasage sans outillage

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1264160B (de) * 1966-12-15 1968-03-21 Boelkow Gmbh Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
US3897316A (en) * 1972-05-17 1975-07-29 Us Air Force Method for manufacturing a composite wall for a regeneratively cooled thrust chamber of a liquid propellant rocket engine
DE3436419C2 (de) * 1983-10-07 1990-11-15 Yoshimichi Chigasaki Kanagawa Masuda Verfahren zur Herstellung von Raketenbrennkammern
FR2669966B1 (fr) * 1990-11-30 1993-03-26 Europ Propulsion Procede de fabrication de paroi de chambre de combustion, notamment pour moteur-fusee, et chambre de combustion obtenue par ce procede.
US5375325A (en) * 1992-05-26 1994-12-27 United Technologies Corporation Method of making a rocket chamber construction
DE4301041C1 (de) * 1993-01-16 1994-04-28 Deutsche Aerospace Verfahren zur Herstellung einer fluidgekühlten Wand in Röhrchenverbundbauweise
US5832719A (en) * 1995-12-18 1998-11-10 United Technologies Corporation Rocket thrust chamber
RU2139439C1 (ru) * 1998-05-20 1999-10-10 Федеральное государственное унитарное предприятие "Конструкторское бюро химавтоматики" Сопло камеры жидкостного ракетного двигателя
US6688100B1 (en) * 2002-07-16 2004-02-10 The Boeing Company Combustion chamber having a multiple-piece liner and associated assembly method

Also Published As

Publication number Publication date
EP1352168B1 (de) 2006-06-21
JP4019217B2 (ja) 2007-12-12
DE60212568T2 (de) 2007-06-14
DE60212568D1 (de) 2006-08-03
JP2004518059A (ja) 2004-06-17
WO2002055862A1 (en) 2002-07-18
RU2273756C2 (ru) 2006-04-10
EP1352168A1 (de) 2003-10-15
US6799418B2 (en) 2004-10-05
US20040103638A1 (en) 2004-06-03
RU2003123786A (ru) 2005-02-27
ES2266498T3 (es) 2007-03-01

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties