DE60212568D1 - Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds - Google Patents

Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds

Info

Publication number
DE60212568D1
DE60212568D1 DE60212568T DE60212568T DE60212568D1 DE 60212568 D1 DE60212568 D1 DE 60212568D1 DE 60212568 T DE60212568 T DE 60212568T DE 60212568 T DE60212568 T DE 60212568T DE 60212568 D1 DE60212568 D1 DE 60212568D1
Authority
DE
Germany
Prior art keywords
device member
rocket device
producing
wall structure
rocket
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE60212568T
Other languages
English (en)
Other versions
DE60212568T2 (de
Inventor
Jan Haeggander
Arne Boman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GKN Aerospace Sweden AB
Original Assignee
Volvo Aero AB
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 AB filed Critical Volvo Aero AB
Application granted granted Critical
Publication of DE60212568D1 publication Critical patent/DE60212568D1/de
Publication of DE60212568T2 publication Critical patent/DE60212568T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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)
  • Testing Of Engines (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Powder Metallurgy (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
DE60212568T 2001-01-11 2002-01-09 Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglied Expired - Lifetime DE60212568T2 (de)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US26104801P 2001-01-11 2001-01-11
SE0100078 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
US261048P 2001-01-11
PCT/SE2002/000025 WO2002055862A1 (en) 2001-01-11 2002-01-09 Rocket engine member and method for manufacturing a rocket engine member

Publications (2)

Publication Number Publication Date
DE60212568D1 true DE60212568D1 (de) 2006-08-03
DE60212568T2 DE60212568T2 (de) 2007-06-14

Family

ID=26655370

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60212568T Expired - Lifetime DE60212568T2 (de) 2001-01-11 2002-01-09 Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglied

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 (5)

* 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
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
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
DE60212568T2 (de) 2007-06-14
US20040103638A1 (en) 2004-06-03
RU2273756C2 (ru) 2006-04-10
ATE331133T1 (de) 2006-07-15
EP1352168A1 (de) 2003-10-15
RU2003123786A (ru) 2005-02-27
JP4019217B2 (ja) 2007-12-12
ES2266498T3 (es) 2007-03-01
WO2002055862A1 (en) 2002-07-18
US6799418B2 (en) 2004-10-05
JP2004518059A (ja) 2004-06-17
EP1352168B1 (de) 2006-06-21

Similar Documents

Publication Publication Date Title
IT1263646B (it) Sistema e procedimento per catturare calore trasferito da aria di raffreddamento compressa in una turbina a gas
DE60202212D1 (de) Kühlbares segment für turbomaschinen und turbinen mit brennkammer
BRPI0416514A (pt) sistema de camadas de alta temperatura para a dissipação de calor e processo para sua fabricação
PL357281A1 (en) A heat exchanger
NO981876L (no) Vµskekj°ling av elektroniske komponenter
DE60212568D1 (de) Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds
TW200721879A (en) Heater unit and semiconductor manufacturing apparatus including the same
JP2000345345A5 (de)
ATE295931T1 (de) Abreibbare dichtung
MXPA03011071A (es) Conjunto de intercambiador termico con tubos en forma de cuna con flujo de refrigerante equilibrado.
DE60213271D1 (de) Separator für brennstoffzelle und verfahren zu dessen herstellung
DK0921354T3 (da) Væskekølet ristplade
DE69602377D1 (de) Isoliersystem und verfahren zur herstellung eines solchen isoliersystems an einer leitung oder einem container
ATE219817T1 (de) Vorrichtung zur wärmeisolierung für eine dampfturbine
ATE335920T1 (de) Vorrichtung zur wärmerückgewinnung
WO1999051069A3 (en) Fiber heat sink and fiber heat exchanger
DE59911364D1 (de) Plattenförmige dauerelastische Hochtemperatur-Dichtung, insbesondere für Abgasanlagen von Verbrennungsmotoren
Horibe Forced Convection Heat Transfer Characteristics of Three Cylinders Formed Across (jointly worked)
Rose Boundary-layer flow with transpiration on an isothermal flat plate
BR9611778A (pt) Método e aparelho para geração de energia térmica
FR2745207B1 (fr) Procede de fabrication d'un echangeur thermique
SE8206196D0 (sv) Anordning vid vegg
SE0100078D0 (sv) Rocket engines
WO2000053908A8 (en) Gas turbine engine
KR960038338A (ko) 흡수기

Legal Events

Date Code Title Description
8364 No opposition during term of opposition