ATE263916T1 - Wärmetauscher aus verbundwerkstoff und dessen herstellungsverfahren - Google Patents

Wärmetauscher aus verbundwerkstoff und dessen herstellungsverfahren

Info

Publication number
ATE263916T1
ATE263916T1 AT99954068T AT99954068T ATE263916T1 AT E263916 T1 ATE263916 T1 AT E263916T1 AT 99954068 T AT99954068 T AT 99954068T AT 99954068 T AT99954068 T AT 99954068T AT E263916 T1 ATE263916 T1 AT E263916T1
Authority
AT
Austria
Prior art keywords
composite material
heat exchanger
production process
composite heat
forming
Prior art date
Application number
AT99954068T
Other languages
English (en)
Inventor
Jean-Pierre Vidal
Jean-Michel Larrieu
Jean-Pierre Ciais
Original Assignee
Moteurs D Aviat Ss N E C M A S
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 Moteurs D Aviat Ss N E C M A S filed Critical Moteurs D Aviat Ss N E C M A S
Application granted granted Critical
Publication of ATE263916T1 publication Critical patent/ATE263916T1/de

Links

Classifications

    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • 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
    • 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
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Ceramic Products (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Moulding By Coating Moulds (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
AT99954068T 1998-11-05 1999-11-05 Wärmetauscher aus verbundwerkstoff und dessen herstellungsverfahren ATE263916T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9813923A FR2785664B1 (fr) 1998-11-05 1998-11-05 Echangeur de chaleur en materiau composite et procede pour sa fabrication
PCT/FR1999/002708 WO2000028202A1 (fr) 1998-11-05 1999-11-05 Echangeur de chaleur en materiau composite et procede pour sa fabrication

Publications (1)

Publication Number Publication Date
ATE263916T1 true ATE263916T1 (de) 2004-04-15

Family

ID=9532395

Family Applications (1)

Application Number Title Priority Date Filing Date
AT99954068T ATE263916T1 (de) 1998-11-05 1999-11-05 Wärmetauscher aus verbundwerkstoff und dessen herstellungsverfahren

Country Status (14)

Country Link
US (1) US6397581B1 (de)
EP (1) EP1045971B1 (de)
JP (1) JP4249396B2 (de)
KR (1) KR100613827B1 (de)
CN (1) CN1113164C (de)
AT (1) ATE263916T1 (de)
CA (1) CA2317707C (de)
DE (1) DE69916240T2 (de)
FR (1) FR2785664B1 (de)
IL (1) IL137097A (de)
NO (1) NO323992B1 (de)
RU (1) RU2249166C2 (de)
UA (1) UA55499C2 (de)
WO (1) WO2000028202A1 (de)

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FR2840974B1 (fr) 2002-06-13 2005-12-30 Snecma Propulsion Solide Anneau d'etancheite pour cahmbre de combustion et chambre de combustion comportant un tel anneau
FR2850742B1 (fr) * 2003-01-30 2005-09-23 Snecma Propulsion Solide Panneau de refroidissement actif en materiau composite thermostructural et procede pour sa fabrication
FR2850741B1 (fr) * 2003-01-30 2005-09-23 Snecma Propulsion Solide Procede de fabrication d'un panneau de refroidissement actif en materiau composite thermostructural
KR20050004524A (ko) * 2003-07-02 2005-01-12 최동민 연소장치
FR2871847B1 (fr) * 2004-06-17 2006-09-29 Snecma Moteurs Sa Montage d'un distributeur de turbine sur une chambre de combustion a parois en cmc dans une turbine a gaz
FR2872072B1 (fr) * 2004-06-24 2006-09-29 Snecma Propulsion Solide Sa Procede de brasage de pieces en materiau composite thermostructural siliciure
EP1672281A1 (de) * 2004-12-16 2006-06-21 Siemens Aktiengesellschaft Hitzeschildelement
US7431074B1 (en) 2006-03-20 2008-10-07 Fellman Michael L Radiator structure
DE102006021539A1 (de) * 2006-05-08 2007-11-15 Eads Space Transportation Gmbh Verfahren zur Herstellung von Bauteilen für den Raketenbau
JP5029257B2 (ja) * 2007-01-17 2012-09-19 東京エレクトロン株式会社 載置台構造及び処理装置
US8127555B2 (en) * 2007-12-13 2012-03-06 Pratt & Whitney Rocketdyne, Inc. Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle
US7914904B2 (en) * 2008-03-25 2011-03-29 General Electric Company Component in a combustion system, and process for preventing slag, ash, and char buildup
DE102010032612A1 (de) * 2010-07-28 2012-03-29 Martin GmbH für Umwelt- und Energietechnik Verfahren zum Schutz von Wärmetauscherrohren in Dampfkesselanlagen, Formkörper, Wärmetauscherrohr und Dampfkesselanlage
JP5769519B2 (ja) * 2011-06-30 2015-08-26 コバレントマテリアル株式会社 強化用繊維材料と強化用繊維材料を用いた繊維強化セラミックス複合材料及びこれらの製造方法
CN102784987B (zh) * 2012-06-18 2014-11-19 航天材料及工艺研究所 一种C/C复合材料内置Ni基高温合金管的焊接方法
FR3001409B1 (fr) * 2013-01-29 2015-07-03 Herakles Procede de fabrication d'une structure alveolaire de forme courbee en materiau composite
US9018511B2 (en) 2013-03-08 2015-04-28 Hamilton Sundstrand Space Systems International, Inc. Spring-loaded heat exchanger fins
US9624786B2 (en) 2013-03-15 2017-04-18 Rolls-Royce Corporation Braze materials and method for joining of ceramic matrix composites
WO2015054244A1 (en) * 2013-10-07 2015-04-16 United Technologies Corporation Bonded combustor wall for a turbine engine
JP2016142484A (ja) * 2015-02-03 2016-08-08 イビデン株式会社 準カプセル溶融塩蓄熱材
US10520193B2 (en) * 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
US10947162B2 (en) 2017-04-13 2021-03-16 Rolls-Royce Corporation Braze alloys for joining or repairing ceramic matrix composite (CMC) components
CN108644028B (zh) * 2018-03-12 2020-01-24 上海卫星工程研究所 一种大推力双向摇摆轨控发动机高温隔热屏
CN109336630B (zh) * 2018-08-29 2021-06-11 宁波华源精特金属制品有限公司 一种支架及其制备方法
GB2595744B (en) * 2020-06-01 2022-11-16 Desmond Lewis Stephen Reduced velocity ramjet
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
KR20240001130A (ko) * 2021-04-28 2024-01-03 오와다 카본 인더스트리얼 가부시키가이샤 내열 구조체 및 열처리로용 부재
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages
FR3146880A1 (fr) * 2023-03-20 2024-09-27 Airbus Operations (S.A.S.) Ensemble de propulsion comprenant un système de conditionnement de carburant positionné à l’arrière d’une zone d’éjection de débris, aéronef comprenant au moins un tel ensemble de propulsion

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US4838031A (en) * 1987-08-06 1989-06-13 Avco Corporation Internally cooled combustion chamber liner
US4832999A (en) * 1987-10-27 1989-05-23 Avco Lycoming/Textron Honeycomb structure assemblies
FR2664585B1 (fr) * 1990-07-13 1993-08-06 Europ Propulsion Structures refractaires refroidies et procede pour leur fabrication.
US5352529A (en) * 1991-05-13 1994-10-04 Auto-Air Composites, Inc. Lightweight thrust vectoring panel
FR2685655B1 (fr) 1991-12-31 1995-08-18 Europ Propulsion Procede de formation d'un passage etanche dans une piece en materiau composite refractaire, et application a la realisation d'une structure composite refractaire refroidie par circulation de fluide.
RU2044989C1 (ru) * 1993-05-21 1995-09-27 Институт внедрения изобретений и новой техники Пластинчатый теплообменник
DE4322431C2 (de) * 1993-07-06 1997-04-10 Mtu Muenchen Gmbh Kühlstruktur und Verfahren zu ihrer Herstellung
AU4044997A (en) 1996-07-24 1998-02-10 Mcdonnell Douglas Corporation Two-step brazing process for joining materials with different coefficients of thermal expansion
DE19804232C2 (de) * 1998-02-04 2000-06-29 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen

Also Published As

Publication number Publication date
EP1045971A1 (de) 2000-10-25
FR2785664A1 (fr) 2000-05-12
EP1045971B1 (de) 2004-04-07
FR2785664B1 (fr) 2001-02-02
KR20010033870A (ko) 2001-04-25
RU2249166C2 (ru) 2005-03-27
DE69916240T2 (de) 2005-04-14
CA2317707A1 (en) 2000-05-18
NO20003477L (no) 2000-09-04
US6397581B1 (en) 2002-06-04
UA55499C2 (uk) 2003-04-15
NO323992B1 (no) 2007-07-30
DE69916240D1 (de) 2004-05-13
CA2317707C (en) 2007-01-09
NO20003477D0 (no) 2000-07-05
JP4249396B2 (ja) 2009-04-02
KR100613827B1 (ko) 2006-08-18
CN1113164C (zh) 2003-07-02
WO2000028202A1 (fr) 2000-05-18
IL137097A0 (en) 2001-06-14
JP2002529679A (ja) 2002-09-10
IL137097A (en) 2003-07-31
CN1287592A (zh) 2001-03-14

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