GB2399163A - A cooling panel made of thermostructural composite material and a method of its manufacture - Google Patents

A cooling panel made of thermostructural composite material and a method of its manufacture Download PDF

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Publication number
GB2399163A
GB2399163A GB0400989A GB0400989A GB2399163A GB 2399163 A GB2399163 A GB 2399163A GB 0400989 A GB0400989 A GB 0400989A GB 0400989 A GB0400989 A GB 0400989A GB 2399163 A GB2399163 A GB 2399163A
Authority
GB
United Kingdom
Prior art keywords
parts
panel
sealing layer
face
composite material
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.)
Withdrawn
Application number
GB0400989A
Other languages
English (en)
Other versions
GB0400989D0 (en
Inventor
Jean-Michel Larrieu
Gilles Uhrig
Jaques 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
Publication of GB0400989D0 publication Critical patent/GB0400989D0/en
Publication of GB2399163A publication Critical patent/GB2399163A/en
Withdrawn legal-status Critical Current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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
GB0400989A 2003-01-30 2004-01-16 A cooling panel made of thermostructural composite material and a method of its manufacture Withdrawn GB2399163A (en)

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
GB0400989D0 GB0400989D0 (en) 2004-02-18
GB2399163A true GB2399163A (en) 2004-09-08

Family

ID=31726076

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0400989A Withdrawn GB2399163A (en) 2003-01-30 2004-01-16 A cooling panel made of thermostructural composite material and a method of its manufacture

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)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US20100229565A1 (en) * 2006-12-19 2010-09-16 Arne Boman Wall of a rocket engine
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
CN102648025A (zh) 2009-07-07 2012-08-22 火星工程有限公司 爆震波防止器
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
EP3055530B1 (fr) * 2013-10-07 2020-08-12 United Technologies Corporation Paroi de dispositif de combustion assemblée par soudage pour un moteur à turbine
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
CN115751376A (zh) * 2022-11-14 2023-03-07 北京航空航天大学 一种轴向曲线型的再生冷却通道

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4838031A (en) * 1987-08-06 1989-06-13 Avco Corporation Internally cooled combustion chamber liner
WO2000028202A1 (fr) * 1998-11-05 2000-05-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation - S.N.E.C.M.A. Echangeur de chaleur en materiau composite et procede pour sa fabrication

Family Cites Families (12)

* Cited by examiner, † Cited by third party
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
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
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4838031A (en) * 1987-08-06 1989-06-13 Avco Corporation Internally cooled combustion chamber liner
WO2000028202A1 (fr) * 1998-11-05 2000-05-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation - S.N.E.C.M.A. Echangeur de chaleur en materiau composite et procede pour sa fabrication
US6397581B1 (en) * 1998-11-05 2002-06-04 Societe Nationale d'Etude et de Construction de Moteurs d'Aviation—S.N.E.C.M.A. Heat exchanger in composite material and method for making same

Also Published As

Publication number Publication date
CA2456403A1 (fr) 2004-07-30
JP2004233043A (ja) 2004-08-19
FR2850742B1 (fr) 2005-09-23
DE102004004424A1 (de) 2005-01-20
GB0400989D0 (en) 2004-02-18
FR2850742A1 (fr) 2004-08-06
US20040194941A1 (en) 2004-10-07

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Legal Events

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WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)