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FR2700583B1 - Procede de fabrication d'une paroi refroidie par fluide formee de petits tubes assembles. - Google Patents

Procede de fabrication d'une paroi refroidie par fluide formee de petits tubes assembles.

Info

Publication number
FR2700583B1
FR2700583B1 FR9400330A FR9400330A FR2700583B1 FR 2700583 B1 FR2700583 B1 FR 2700583B1 FR 9400330 A FR9400330 A FR 9400330A FR 9400330 A FR9400330 A FR 9400330A FR 2700583 B1 FR2700583 B1 FR 2700583B1
Authority
FR
France
Prior art keywords
producing
wall formed
cooled wall
fluid cooled
assembled tubes
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 - Fee Related
Application number
FR9400330A
Other languages
English (en)
Other versions
FR2700583A1 (fr
Inventor
Christoph Caesar
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.)
Airbus Defence and Space GmbH
Original Assignee
Deutsche Aerospace 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 Deutsche Aerospace AG filed Critical Deutsche Aerospace AG
Publication of FR2700583A1 publication Critical patent/FR2700583A1/fr
Application granted granted Critical
Publication of FR2700583B1 publication Critical patent/FR2700583B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/08—Cooling thereof; Tube walls
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR9400330A 1993-01-16 1994-01-13 Procede de fabrication d'une paroi refroidie par fluide formee de petits tubes assembles. Expired - Fee Related FR2700583B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4301041A DE4301041C1 (de) 1993-01-16 1993-01-16 Verfahren zur Herstellung einer fluidgekühlten Wand in Röhrchenverbundbauweise

Publications (2)

Publication Number Publication Date
FR2700583A1 FR2700583A1 (fr) 1994-07-22
FR2700583B1 true FR2700583B1 (fr) 1995-11-17

Family

ID=6478327

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9400330A Expired - Fee Related FR2700583B1 (fr) 1993-01-16 1994-01-13 Procede de fabrication d'une paroi refroidie par fluide formee de petits tubes assembles.

Country Status (2)

Country Link
DE (1) DE4301041C1 (fr)
FR (1) FR2700583B1 (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5832719A (en) * 1995-12-18 1998-11-10 United Technologies Corporation Rocket thrust chamber
DE19915082C1 (de) * 1999-04-01 2000-07-13 Daimler Chrysler Ag Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk
ATE331133T1 (de) * 2001-01-11 2006-07-15 Volvo Aero Corp Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds
EP1352166B1 (fr) * 2001-01-11 2006-04-12 Volvo Aero Corporation Tuyere de sortie et son procede de production
EP1352170B1 (fr) * 2001-01-11 2006-06-07 Volvo Aero Corporation Element de moteur-fusee et procede de fabrication d'un element de moteur-fusee
US7051513B2 (en) * 2003-06-06 2006-05-30 United Technologies Corporation Rocket engine tubular chamber with single piece jacket
DE102005050873B4 (de) * 2005-10-21 2020-08-06 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung einer segmentierten Beschichtung und nach dem Verfahren hergestelltes Bauteil
RU2391539C1 (ru) * 2008-12-17 2010-06-10 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Тракт охлаждения камеры жидкостного ракетного двигателя
RU2392478C1 (ru) * 2008-12-17 2010-06-20 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Тракт охлаждения камеры жидкостного ракетного двигателя
RU2392476C1 (ru) * 2008-12-17 2010-06-20 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Камера жидкостного ракетного двигателя
RU2391533C1 (ru) * 2008-12-17 2010-06-10 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Камера жидкостного ракетного двигателя
RU2403424C2 (ru) * 2008-12-17 2010-11-10 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Тракт охлаждения камеры жидкостного ракетного двигателя
RU2392479C1 (ru) * 2008-12-17 2010-06-20 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ изготовления тракта охлаждения теплонапряженных конструкций
RU2555418C1 (ru) * 2014-01-09 2015-07-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Камера жидкостного ракетного двигателя
RU2643927C1 (ru) * 2016-06-06 2018-02-06 Акционерное общество Центральный научно-исследовательский институт специального машиностроения Камера сгорания прямоточного воздушно-реактивного двигателя из композиционных материалов

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3190070A (en) * 1950-04-05 1965-06-22 Thiokol Chemical Corp Reaction motor construction
US2844939A (en) * 1954-10-04 1958-07-29 Gen Electric Tube-bundle combustion chamber
US3692637A (en) * 1969-11-24 1972-09-19 Carl Helmut Dederra Method of fabricating a hollow structure having cooling channels
DE2137109C3 (de) * 1971-07-24 1980-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Herstellung einer regenerativ gekühlten Raketenbrennkammer
DE2657474A1 (de) * 1976-12-18 1978-06-22 Messerschmitt Boelkow Blohm Verfahren zum herstellen von regenerativ gekuehlten raketenbrennkammern und/oder schubduesen
US4576874A (en) * 1984-10-03 1986-03-18 Westinghouse Electric Corp. Spalling and corrosion resistant ceramic coating for land and marine combustion turbines
JPH0791660B2 (ja) * 1989-08-30 1995-10-04 株式会社日立製作所 環境遮断用耐熱壁を備えた地上機器
IL99473A0 (en) * 1990-09-20 1992-08-18 United Technologies Corp Columnar ceramic thermal barrier coating with improved adherence
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.
DE4137638C2 (de) * 1991-11-15 1994-08-11 Mtu Muenchen Gmbh Bauteil mit einer vor thermischer Belastung zu schützenden Wand

Also Published As

Publication number Publication date
FR2700583A1 (fr) 1994-07-22
DE4301041C1 (de) 1994-04-28

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Legal Events

Date Code Title Description
ST Notification of lapse