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 PDFInfo
- 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- Withdrawn
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)
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 (ja) |
JP (1) | JP2004233043A (ja) |
CA (1) | CA2456403A1 (ja) |
DE (1) | DE102004004424A1 (ja) |
FR (1) | FR2850742B1 (ja) |
GB (1) | GB2399163A (ja) |
Families Citing this family (25)
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 |
WO2008076008A1 (en) * | 2006-12-19 | 2008-06-26 | Volvo Aero Corporation | Wall of a rocket engine |
DE102007016375A1 (de) * | 2007-03-31 | 2008-10-02 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Bauteile für Wärmesenken |
EP2376763A2 (en) * | 2008-12-08 | 2011-10-19 | Firestar Engineering, LLC | Regeneratively cooled porous media jacket |
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 (en) | 2009-07-07 | 2011-01-13 | Firestar Engineering Llc | Detonation wave arrestor |
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 (en) * | 2013-10-07 | 2020-08-12 | 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 |
CN118003043A (zh) * | 2022-09-26 | 2024-05-10 | 宁德文达镁铝科技有限公司 | 供油稳定的油压夹具底板油路加工方法 |
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)
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)
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 (ja) * | 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 |
-
2003
- 2003-01-30 FR FR0301041A patent/FR2850742B1/fr not_active Expired - Fee Related
-
2004
- 2004-01-16 GB GB0400989A patent/GB2399163A/en not_active Withdrawn
- 2004-01-27 US US10/765,416 patent/US20040194941A1/en not_active Abandoned
- 2004-01-28 DE DE102004004424A patent/DE102004004424A1/de not_active Withdrawn
- 2004-01-29 CA CA002456403A patent/CA2456403A1/en not_active Abandoned
- 2004-01-30 JP JP2004023396A patent/JP2004233043A/ja active Pending
Patent Citations (3)
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 |
---|---|
JP2004233043A (ja) | 2004-08-19 |
FR2850742B1 (fr) | 2005-09-23 |
GB0400989D0 (en) | 2004-02-18 |
DE102004004424A1 (de) | 2005-01-20 |
FR2850742A1 (fr) | 2004-08-06 |
US20040194941A1 (en) | 2004-10-07 |
CA2456403A1 (en) | 2004-07-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |