CA2456403A1 - Panneau de refroidissement actif de materiau composite thermo-structural et methode de fabrication - Google Patents

Panneau de refroidissement actif de materiau composite thermo-structural et methode de fabrication Download PDF

Info

Publication number
CA2456403A1
CA2456403A1 CA002456403A CA2456403A CA2456403A1 CA 2456403 A1 CA2456403 A1 CA 2456403A1 CA 002456403 A CA002456403 A CA 002456403A CA 2456403 A CA2456403 A CA 2456403A CA 2456403 A1 CA2456403 A1 CA 2456403A1
Authority
CA
Canada
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.)
Abandoned
Application number
CA002456403A
Other languages
English (en)
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
Publication of CA2456403A1 publication Critical patent/CA2456403A1/fr
Abandoned legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/08Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
    • F28F21/081Heat exchange elements made from metals or metal alloys
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion or thrust chambers having cooling arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • F02K9/972Fluid cooling arrangements for nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • F02K9/974Nozzle- linings; Ablative coatings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005Combined with pressure or heat exchangers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/12Elements constructed in the shape of a hollow panel, e.g. with channels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0077Other 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
    • F28D2021/0078Other 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/10Nuclear 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)
CA002456403A 2003-01-30 2004-01-29 Panneau de refroidissement actif de materiau composite thermo-structural et methode de fabrication Abandoned CA2456403A1 (fr)

Applications Claiming Priority (2)

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
FR0301041 2003-01-30

Publications (1)

Publication Number Publication Date
CA2456403A1 true CA2456403A1 (fr) 2004-07-30

Family

ID=31726076

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002456403A Abandoned CA2456403A1 (fr) 2003-01-30 2004-01-29 Panneau de refroidissement actif de materiau composite thermo-structural et methode de 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)

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

Family Cites Families (14)

* 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
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
JP2004233043A (ja) 2004-08-19
FR2850742B1 (fr) 2005-09-23
DE102004004424A1 (de) 2005-01-20
GB2399163A (en) 2004-09-08
GB0400989D0 (en) 2004-02-18
FR2850742A1 (fr) 2004-08-06
US20040194941A1 (en) 2004-10-07

Similar Documents

Publication Publication Date Title
US20040194941A1 (en) Active cooling panel of thermostructural composite material and method for its manufacture
US20050077341A1 (en) Method of manufacturing an active cooling panel out of thermostructural composite material
US6397581B1 (en) Heat exchanger in composite material and method for making same
EP1432571B1 (fr) Materiau ceramique hybride a couches isolantes et structurelles en ceramique
US4580524A (en) Process for the preparation of fiber-reinforced ceramic composites by chemical vapor deposition
US20060006212A1 (en) Method of brazing composite material parts sealed with a silicon-based composition
US7153096B2 (en) Stacked laminate CMC turbine vane
US6151887A (en) Combustion chamber for rocket engine
EP1313932B1 (fr) Revetement a barriere thermique
US10458653B2 (en) Machinable CMC insert
US10465534B2 (en) Machinable CMC insert
CN107701326B (zh) 内燃发动机及用于涂覆内燃发动机部件的方法
US10401028B2 (en) Machinable CMC insert
JP2005320236A (ja) 不透過性耐熱構造複合材料から部品を製造する方法
US10472976B2 (en) Machinable CMC insert
US11643948B2 (en) Internal cooling circuits for CMC and method of manufacture
US20200063690A1 (en) Polymeric and metal cylinder head and method of making the same
GB2130244A (en) Forming coatings by hot isostatic compaction
US6482485B1 (en) Structural part including a portion made of thermostructural composite material cooled by fluid circulation
EP1511930B1 (fr) Structure de paroi
JP2016205389A (ja) ターボ機械用の複合シール
Hatta et al. Heat Exchangers for An Air‐Turbo‐Ram‐Jet Engine

Legal Events

Date Code Title Description
FZDE Discontinued