FR2850742B1 - Panneau de refroidissement actif en materiau composite thermostructural et procede pour sa fabrication - Google Patents

Panneau de refroidissement actif en materiau composite thermostructural et procede pour sa fabrication

Info

Publication number
FR2850742B1
FR2850742B1 FR0301041A FR0301041A FR2850742B1 FR 2850742 B1 FR2850742 B1 FR 2850742B1 FR 0301041 A FR0301041 A FR 0301041A FR 0301041 A FR0301041 A FR 0301041A FR 2850742 B1 FR2850742 B1 FR 2850742B1
Authority
FR
France
Prior art keywords
producing
same
composite material
active cooling
cooling panel
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
FR0301041A
Other languages
English (en)
Other versions
FR2850742A1 (fr
Inventor
Jean Michel Larrieu
Gilles Uhrig
Jacques Thebault
Clement Bouquet
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.)
Safran Ceramics SA
Original Assignee
SNECMA Propulsion Solide SA
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 SNECMA Propulsion Solide SA filed Critical SNECMA Propulsion Solide SA
Priority to FR0301041A priority Critical patent/FR2850742B1/fr
Priority to GB0400989A priority patent/GB2399163A/en
Priority to US10/765,416 priority patent/US20040194941A1/en
Priority to DE102004004424A priority patent/DE102004004424A1/de
Priority to CA002456403A priority patent/CA2456403A1/fr
Priority to JP2004023396A priority patent/JP2004233043A/ja
Publication of FR2850742A1 publication Critical patent/FR2850742A1/fr
Application granted granted Critical
Publication of FR2850742B1 publication Critical patent/FR2850742B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
    • F28F21/081—Heat exchange elements made from metals or metal alloys
    • 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
    • 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
    • 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
    • F02K9/974—Nozzle- linings; Ablative coatings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/12—Elements constructed in the shape of a hollow panel, e.g. with channels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0077—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for tempering, e.g. with cooling or heating circuits for temperature control of elements
    • F28D2021/0078—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for tempering, e.g. with cooling or heating circuits for temperature control of elements in the form of cooling walls
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00—Energy generation of nuclear origin
    • Y02E30/10—Nuclear fusion reactors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Ceramic Products (AREA)
  • Laminated Bodies (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR0301041A 2003-01-30 2003-01-30 Panneau de refroidissement actif en materiau composite thermostructural et procede pour sa fabrication Expired - Fee Related FR2850742B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR0301041A FR2850742B1 (fr) 2003-01-30 2003-01-30 Panneau de refroidissement actif en materiau composite thermostructural et procede pour sa fabrication
GB0400989A GB2399163A (en) 2003-01-30 2004-01-16 A cooling panel made of thermostructural composite material and a method of its manufacture
US10/765,416 US20040194941A1 (en) 2003-01-30 2004-01-27 Active cooling panel of thermostructural composite material and method for its manufacture
DE102004004424A DE102004004424A1 (de) 2003-01-30 2004-01-28 Aktive Kühltafel aus Thermostruktur-Kompositwerkstoff und Verfahren zur Herstellung selbiger
CA002456403A CA2456403A1 (fr) 2003-01-30 2004-01-29 Panneau de refroidissement actif de materiau composite thermo-structural et methode de fabrication
JP2004023396A JP2004233043A (ja) 2003-01-30 2004-01-30 熱構造複合材料の活性冷却パネルおよびその製造方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0301041A FR2850742B1 (fr) 2003-01-30 2003-01-30 Panneau de refroidissement actif en materiau composite thermostructural et procede pour sa fabrication

Publications (2)

Publication Number Publication Date
FR2850742A1 FR2850742A1 (fr) 2004-08-06
FR2850742B1 true FR2850742B1 (fr) 2005-09-23

Family

ID=31726076

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0301041A Expired - Fee Related FR2850742B1 (fr) 2003-01-30 2003-01-30 Panneau de refroidissement actif en materiau composite thermostructural et procede pour sa fabrication

Country Status (6)

Country Link
US (1) US20040194941A1 (fr)
JP (1) JP2004233043A (fr)
CA (1) CA2456403A1 (fr)
DE (1) DE102004004424A1 (fr)
FR (1) FR2850742B1 (fr)
GB (1) GB2399163A (fr)

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FR2872072B1 (fr) * 2004-06-24 2006-09-29 Snecma Propulsion Solide Sa Procede de brasage de pieces en materiau composite thermostructural siliciure
US20060113063A1 (en) * 2004-10-15 2006-06-01 Lalit Chordia Thin-plate microchannel structure
DE102004057497B4 (de) * 2004-11-29 2012-01-12 Siemens Ag Wärmeaustauschvorrichtung und Verfahren zum Herstellen der Wärmeaustauschvorrichtung sowie Anordnung eines Bauelements und der Wärmeaustauschvorrichtung und Verfahren zum Herstellen der Anordnung
US20060157234A1 (en) * 2005-01-14 2006-07-20 Honeywell International Inc. Microchannel heat exchanger fabricated by wire electro-discharge machining
US7665307B2 (en) * 2005-12-22 2010-02-23 United Technologies Corporation Dual wall combustor liner
EP2094964A4 (fr) * 2006-12-19 2013-05-01 Volvo Aero Corp Paroi de moteur-fusée
DE102007016375A1 (de) * 2007-03-31 2008-10-02 Deutsches Zentrum für Luft- und Raumfahrt e.V. Bauteile für Wärmesenken
JP5711665B2 (ja) * 2008-12-08 2015-05-07 ファイアースター エンジニアリング，エルエルシー 多孔質媒体を用いる再生冷却型ジャケット
FR2945580B1 (fr) * 2009-05-15 2015-12-25 Snecma Chambre de combustion de moteur pour un vehicule capable de se deplacer dans l'air ou dans l'espace et son procede de fabrication.
FR2945581B1 (fr) * 2009-05-15 2014-05-02 Snecma Divergent de moteur pour un vehicule capable de se deplacer dans l'air ou dans l'espace et son procede de fabrication.
US20100294461A1 (en) * 2009-05-22 2010-11-25 General Electric Company Enclosure for heat transfer devices, methods of manufacture thereof and articles comprising the same
WO2011005875A1 (fr) 2009-07-07 2011-01-13 Firestar Engineering Llc Dispositif d'arrêt d'onde de détonation
DE202011002197U1 (de) * 2011-02-01 2012-02-02 Dana Gmbh Wärmetauscher
FR2971763B1 (fr) * 2011-02-22 2013-03-15 Airbus Operations Sas Echangeur thermique incorpore dans une paroi d'un aeronef
US8870523B2 (en) * 2011-03-07 2014-10-28 General Electric Company Method for manufacturing a hot gas path component and hot gas path turbine component
US10161691B2 (en) * 2012-01-16 2018-12-25 The Boeing Company Multi-channel cooling plenum
US10598378B2 (en) 2013-10-07 2020-03-24 United Technologies Corporation Bonded combustor wall for a turbine engine
US10079165B2 (en) 2014-05-20 2018-09-18 Applied Materials, Inc. Electrostatic chuck with independent zone cooling and reduced crosstalk
DE102014017031A1 (de) * 2014-11-19 2016-05-19 Fachhochschule Düsseldorf Wärmeübertragerelement und Verfahren zur Wärmeübertragung
US10520193B2 (en) * 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
DE102016102095A1 (de) * 2016-02-05 2017-08-10 Alinox Ag Verfahren zum Herstellen eines Verbundmetallgegenstands mit eingebettetem Heizelement, sowie danach hergestellter Verbundmetallgegenstand
CN112459926B (zh) * 2020-12-01 2021-07-06 蓝箭航天空间科技股份有限公司 一种推力室身部组件焊接加工工艺及航天器推力室
CN113074387B (zh) * 2021-04-29 2022-02-25 北京航空航天大学 一种带有桁架结构的再生冷却通道
CN115415750B (zh) * 2022-09-26 2024-02-02 宁德文达镁铝科技有限公司 油压夹具的底板油路的加工方法

Family Cites Families (14)

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Publication number Priority date Publication date Assignee Title
US3246689A (en) * 1963-12-23 1966-04-19 Johns Manville Heating or cooling wall panels
US4246960A (en) * 1979-03-26 1981-01-27 Olin Corporation Fail safe heat exchanger
DE3246541A1 (de) * 1982-12-16 1984-06-20 Reinhard 6911 Campione Hering Verfahren zur herstellung von platten oder formkoerpern
DE3436419C2 (de) * 1983-10-07 1990-11-15 Yoshimichi Chigasaki Kanagawa Masuda Verfahren zur Herstellung von Raketenbrennkammern
US4838031A (en) * 1987-08-06 1989-06-13 Avco Corporation Internally cooled combustion chamber liner
US5022459A (en) * 1988-12-06 1991-06-11 Chiles Daniel T Flexible hose heat exchanger construction with combination locating and thawing wire
DE4015204C1 (fr) * 1990-05-11 1991-10-17 Mtu Muenchen Gmbh
US5520976A (en) * 1993-06-30 1996-05-28 Simmonds Precision Products Inc. Composite enclosure for electronic hardware
FR2748471B1 (fr) 1996-05-07 1998-06-12 Commissariat Energie Atomique Assemblage par brasage de materiaux ceramiques contenant du carbure de silicium
FR2749787B1 (fr) 1996-06-12 1998-07-24 Commissariat Energie Atomique Procede d'assemblage a l'aide d'un joint epais de pieces en materiaux a base de sic par brasage refractaire et joint refractaire et epais ainsi obtenu
DE19730674A1 (de) * 1997-07-17 1999-01-21 Deutsch Zentr Luft & Raumfahrt Brennkammer und Verfahren zur Herstellung einer Brennkammer
FR2785664B1 (fr) * 1998-11-05 2001-02-02 Snecma Echangeur de chaleur en materiau composite et procede pour sa fabrication
BE1013874A3 (nl) * 2000-12-15 2002-11-05 Stroobants Marcel Decoratieve radiator.
US8584738B2 (en) * 2002-06-14 2013-11-19 Lockheed Martin Corporation Apparatus and method for extracting heat from a device

Also Published As

Publication number Publication date
DE102004004424A1 (de) 2005-01-20
JP2004233043A (ja) 2004-08-19
GB2399163A (en) 2004-09-08
FR2850742A1 (fr) 2004-08-06
GB0400989D0 (en) 2004-02-18
US20040194941A1 (en) 2004-10-07
CA2456403A1 (fr) 2004-07-30

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20091030