FR2791589B1 - Procede de fabrication d'une tuyere de moteur de fusee a refroidissement et tuyere obtenue - Google Patents

Procede de fabrication d'une tuyere de moteur de fusee a refroidissement et tuyere obtenue

Info

Publication number
FR2791589B1
FR2791589B1 FR0004017A FR0004017A FR2791589B1 FR 2791589 B1 FR2791589 B1 FR 2791589B1 FR 0004017 A FR0004017 A FR 0004017A FR 0004017 A FR0004017 A FR 0004017A FR 2791589 B1 FR2791589 B1 FR 2791589B1
Authority
FR
France
Prior art keywords
nozzle
manufacturing
rocket motor
cooling rocket
cooling
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
FR0004017A
Other languages
English (en)
Other versions
FR2791589A1 (fr
Inventor
Joachim Kretschmer
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.)
Daimler AG
Original Assignee
DaimlerChrysler AG
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 DaimlerChrysler AG filed Critical DaimlerChrysler AG
Publication of FR2791589A1 publication Critical patent/FR2791589A1/fr
Application granted granted Critical
Publication of FR2791589B1 publication Critical patent/FR2791589B1/fr
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
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/008—Rocket engine parts, e.g. nozzles, combustion chambers
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/40—Cooling arrangements
    • 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
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/15—Two-dimensional spiral
    • 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
    • F05D2250/25—Three-dimensional helical
    • 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)
  • Coating By Spraying Or Casting (AREA)
  • Moulding By Coating Moulds (AREA)
FR0004017A 1999-04-01 2000-03-30 Procede de fabrication d'une tuyere de moteur de fusee a refroidissement et tuyere obtenue Expired - Lifetime FR2791589B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19915082A DE19915082C1 (de) 1999-04-01 1999-04-01 Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk

Publications (2)

Publication Number Publication Date
FR2791589A1 FR2791589A1 (fr) 2000-10-06
FR2791589B1 true FR2791589B1 (fr) 2001-11-16

Family

ID=7903388

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0004017A Expired - Lifetime FR2791589B1 (fr) 1999-04-01 2000-03-30 Procede de fabrication d'une tuyere de moteur de fusee a refroidissement et tuyere obtenue

Country Status (5)

Country Link
US (2) US6470671B1 (fr)
JP (1) JP4465485B2 (fr)
DE (1) DE19915082C1 (fr)
FR (1) FR2791589B1 (fr)
SE (1) SE520969C2 (fr)

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JP4537509B2 (ja) * 1998-05-07 2010-09-01 株式会社リコー 画像形成装置
FR2836699B1 (fr) * 2002-03-04 2005-02-11 Eads Launch Vehicles Moteur de fusee
US6883220B2 (en) * 2002-07-17 2005-04-26 The Boeing Company Method for forming a tube-walled article
EP1398569A1 (fr) * 2002-09-13 2004-03-17 Siemens Aktiengesellschaft Turbine à gaz
CA2444917A1 (fr) * 2002-10-18 2004-04-18 United Technologies Corporation Cuivre pulverise a froid sur des composants de moteur-fusee
US6802179B2 (en) * 2002-12-02 2004-10-12 Aerojet-General Corporation Nozzle with spiral internal cooling channels
US20070163228A1 (en) * 2006-01-19 2007-07-19 United Technologies Corporation Gas augmented rocket engine
JP4887133B2 (ja) * 2006-12-21 2012-02-29 株式会社リコー 画像形成装置
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
FR2915528B1 (fr) 2007-04-25 2012-07-06 Astrium Sas Procede et dispositif pour alimenter un moteur de propulsion spatiale en ergols cryogeniques liquides.
DE102010019958B4 (de) * 2010-05-08 2016-05-04 MTU Aero Engines AG Verfahren zur Herstellung eines Einlaufbelags
RU2480611C1 (ru) * 2012-01-11 2013-04-27 Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" Способ изготовления камеры жидкостного ракетного двигателя
RU2480610C1 (ru) * 2012-01-11 2013-04-27 Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" Камера жидкостного ракетного двигателя
CN107076055B (zh) 2014-09-25 2018-11-02 帕奇德科尼克斯有限责任公司 流体加压供给装置、系统以及方法
CN105710606A (zh) * 2015-11-25 2016-06-29 沈阳黎明航空发动机(集团)有限责任公司 一种燃气发生器喷嘴头的加工方法
US9835114B1 (en) 2017-06-06 2017-12-05 The United States Of America As Represented By The Administrator Of Nasa Freeform deposition method for coolant channel closeout
US10471542B1 (en) * 2017-06-27 2019-11-12 United States Of America As Represented By The Administrator Of Nasa Cladding and freeform deposition for coolant channel closeout
CN110925114A (zh) * 2019-12-27 2020-03-27 哈尔滨工程大学 一种发动机壳体冷却装置
CN115539248B (zh) * 2022-10-20 2024-09-13 合肥工业大学 一种火箭发动机壳体及其制备方法

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US3190070A (en) * 1950-04-05 1965-06-22 Thiokol Chemical Corp Reaction motor construction
GB794660A (en) * 1954-08-30 1958-05-07 Havilland Engine Co Ltd Heat exchangers
US3241311A (en) * 1957-04-05 1966-03-22 United Aircraft Corp Turbofan engine
US3099909A (en) * 1959-05-21 1963-08-06 United Aircraft Corp Nozzle construction
US3170286A (en) * 1962-03-26 1965-02-23 Stein Samuel Injector-valve device
US3349464A (en) * 1962-06-29 1967-10-31 Aerojet General Co Method of making rocket combustion chamber
US3289943A (en) * 1962-08-17 1966-12-06 Westinghouse Electric Corp Thermal barrier for thrust vehicle nozzle
US3224678A (en) * 1962-10-04 1965-12-21 Marquardt Corp Modular thrust chamber
US3170266A (en) 1962-11-07 1965-02-23 Reynolds Metals Co Soffit systems
US3267664A (en) * 1963-03-19 1966-08-23 North American Aviation Inc Method of and device for cooling
DE1264160B (de) * 1966-12-15 1968-03-21 Boelkow Gmbh Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
US3460759A (en) * 1967-03-07 1969-08-12 Nasa Combustion chamber
US3692637A (en) * 1969-11-24 1972-09-19 Carl Helmut Dederra Method of fabricating a hollow structure having cooling channels
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
US4148121A (en) * 1974-06-12 1979-04-10 Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung Method and apparatus for manufacturing rotationally symmetrical constructional parts such as nozzles and combination chambers of rocket engines
DE2522681C2 (de) * 1975-05-22 1983-04-14 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorrichtung zur Montage von spiralförmig gebogenen Rohren zur Herstellung von rotationssymmetrischen Bauteilen
US4131057A (en) * 1976-09-29 1978-12-26 Phillips Petroleum Company Apparatus for forming a convoluted container sidewall
FR2482666B1 (fr) * 1980-05-19 1985-06-21 Europ Propulsion Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur
DE3942022A1 (de) * 1989-12-20 1991-06-27 Mtu Muenchen Gmbh Verfahren und vorrichtung zur kuehlung eines flugtriebwerkes
US5221045A (en) * 1991-09-23 1993-06-22 The Babcock & Wilcox Company Bulge formed cooling channels with a variable lead helix on a hollow body of revolution
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US5546656A (en) * 1994-11-30 1996-08-20 United Technologies Corporation Fabrication of rocket thrust chambers
DE19520885C2 (de) * 1995-06-08 1999-05-20 Daimler Benz Ag Verfahren zum thermischen Spritzen von Schichten aus Metallegierungen oder Metallen und seine Verwendung

Also Published As

Publication number Publication date
JP4465485B2 (ja) 2010-05-19
SE0001068L (sv) 2000-10-02
FR2791589A1 (fr) 2000-10-06
US6470671B1 (en) 2002-10-29
DE19915082C1 (de) 2000-07-13
US20020056762A1 (en) 2002-05-16
SE520969C2 (sv) 2003-09-16
US6543135B2 (en) 2003-04-08
JP2000320404A (ja) 2000-11-21
SE0001068D0 (sv) 2000-03-27

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