SE523812C2 - Brännkammare med innermantel av ett keramiskt kompositionesmaterial och förfarande för framställning - Google Patents

Brännkammare med innermantel av ett keramiskt kompositionesmaterial och förfarande för framställning

Info

Publication number
SE523812C2
SE523812C2 SE0201656A SE0201656A SE523812C2 SE 523812 C2 SE523812 C2 SE 523812C2 SE 0201656 A SE0201656 A SE 0201656A SE 0201656 A SE0201656 A SE 0201656A SE 523812 C2 SE523812 C2 SE 523812C2
Authority
SE
Sweden
Prior art keywords
fibers
composite material
combustion chamber
fiber structure
layers
Prior art date
Application number
SE0201656A
Other languages
English (en)
Swedish (sv)
Other versions
SE0201656D0 (sv
SE0201656L (sv
Inventor
Steffen Beyer
Helmut Knabe
Dieter Preclik
Original Assignee
Astrium Gmbh
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 Astrium Gmbh filed Critical Astrium Gmbh
Publication of SE0201656D0 publication Critical patent/SE0201656D0/xx
Publication of SE0201656L publication Critical patent/SE0201656L/xx
Publication of SE523812C2 publication Critical patent/SE523812C2/sv

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05004—Special materials for walls or lining
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S239/00—Fluid sprinkling, spraying, and diffusing
    • Y10S239/19—Nozzle materials
    • 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
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/249927—Fiber embedded in a metal matrix
    • 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
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31678—Of metal

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Ceramic Products (AREA)
  • Laminated Bodies (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
SE0201656A 2001-06-01 2002-05-31 Brännkammare med innermantel av ett keramiskt kompositionesmaterial och förfarande för framställning SE523812C2 (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10126926.9A DE10126926B4 (de) 2001-06-01 2001-06-01 Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung

Publications (3)

Publication Number Publication Date
SE0201656D0 SE0201656D0 (sv) 2002-05-31
SE0201656L SE0201656L (sv) 2002-12-02
SE523812C2 true SE523812C2 (sv) 2004-05-18

Family

ID=7687022

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0201656A SE523812C2 (sv) 2001-06-01 2002-05-31 Brännkammare med innermantel av ett keramiskt kompositionesmaterial och förfarande för framställning

Country Status (6)

Country Link
US (2) US6890660B2 (fr)
JP (1) JP4173975B2 (fr)
DE (1) DE10126926B4 (fr)
FR (1) FR2825417B1 (fr)
IT (1) ITMI20021190A1 (fr)
SE (1) SE523812C2 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6627019B2 (en) * 2000-12-18 2003-09-30 David C. Jarmon Process for making ceramic matrix composite parts with cooling channels
DE10126926B4 (de) * 2001-06-01 2015-02-19 Astrium Gmbh Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung
US7213392B2 (en) 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
DE102005036137A1 (de) * 2005-07-26 2007-02-01 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammer und Verfahren zur Herstellung einer Brennkammer
US7665307B2 (en) * 2005-12-22 2010-02-23 United Technologies Corporation Dual wall combustor liner
DE102006021539A1 (de) * 2006-05-08 2007-11-15 Eads Space Transportation Gmbh Verfahren zur Herstellung von Bauteilen für den Raketenbau
US20080207075A1 (en) * 2007-02-22 2008-08-28 Siemens Power Generation, Inc. Optimized fabric lay-up for improved ceramic matrix composites
DE102007048527B4 (de) * 2007-10-10 2014-03-27 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Schubtriebwerk
US20090235636A1 (en) * 2008-03-21 2009-09-24 Robert Oehrlein Reinforced, regeneratively cooled uni-body rocket engine
DE102008020198B8 (de) * 2008-04-15 2015-05-13 Astrium Gmbh Düsenerweiterung für ein Triebwerk und Verfahren zur Herstellung und Kühlung einer Düsenerweiterung
EP2233835A1 (fr) * 2009-03-23 2010-09-29 Siemens Aktiengesellschaft Chambre de combustion brasée avec des inserts en céramique
EP2833064A3 (fr) * 2013-07-31 2015-07-15 Siemens Aktiengesellschaft Centrale thermique au charbon
US10774648B2 (en) * 2016-10-04 2020-09-15 General Electric Company Methods and features for CMC component repairs
CN106762222B (zh) * 2016-11-29 2018-03-09 湖北三江航天江北机械工程有限公司 大型分段复合材料壳体连接结构及壳体缠绕方法
CN107023419B (zh) * 2017-05-03 2019-05-03 湖北航天技术研究院总体设计所 一种固体火箭发动机燃烧室壳体轻质接头
RU2720596C1 (ru) * 2018-11-08 2020-05-12 Федеральное государственное бюджетное образовательное учреждение высшего образования "Воронежский государственный технический университет" (ФГБОУ ВО "ВГТУ") Камера жидкостного ракетного двигателя
CN114057491B (zh) * 2021-11-19 2022-07-12 西北工业大学 一种陶瓷基复合材料脉冲爆震发动机燃烧室的制备方法

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3212257A (en) * 1964-10-23 1965-10-19 Hercules Powder Co Ltd Rocket motor
GB1215002A (en) * 1967-02-02 1970-12-09 Courtaulds Ltd Coating carbon with metal
US4063684A (en) * 1975-11-25 1977-12-20 The United States Of America As Represented By The Secretary Of The Air Force Composite rocket nozzle structure
US4967599A (en) * 1980-05-19 1990-11-06 Societe Europeenne De Propulsion Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a solid propellant rocket motor
GB8613472D0 (en) * 1986-06-04 1986-08-20 Royal Ordnance Plc Components for propellant engine combustion chambers
US4999240A (en) * 1986-07-21 1991-03-12 Brotz Gregory R Metalized fiber/member structures and methods of producing same
US4817890A (en) * 1986-10-14 1989-04-04 General Electric Company Multiple-propellant air vehicle and propulsion system
FR2610044A1 (fr) * 1986-10-14 1988-07-29 Gen Electric Systeme de propulsion comportant une garniture perfectionnee de la chambre de combustion et procede de fabrication d'une telle fabrication
US5147368A (en) * 1991-04-05 1992-09-15 Brown Alan W Nucleus splitter
JP2673078B2 (ja) * 1992-05-27 1997-11-05 東芝電池株式会社 アルカリ二次電池用のペースト式電極
US5451448A (en) * 1993-07-01 1995-09-19 The United States Of America As Represented By The United States National Aeronautics And Space Administration Flexible ceramic thermal protection system resistant to high aeroacoustic noise comprising a three-dimensional woven-fiber structure having a multilayer top fabric layer, a bottom fabric layer and an intermediate rib fabric layer
US5780157A (en) * 1994-06-06 1998-07-14 Ultramet Composite structure
JP3282443B2 (ja) * 1994-06-09 2002-05-13 住友電気工業株式会社 金属不織布とその製造方法
DE19505357C1 (de) * 1995-02-17 1996-05-23 Daimler Benz Aerospace Ag Verfahren zur Kühlung von Triebwerkswänden und Wandstruktur zur Durchführung desselben
DE19602731C1 (de) * 1996-01-26 1997-07-10 Daimler Benz Aerospace Ag Wandstruktur für treibstoffgekühlte Triebwerkswände
US6418973B1 (en) * 1996-10-24 2002-07-16 Boeing North American, Inc. Integrally woven ceramic composites
US5842342A (en) * 1997-02-21 1998-12-01 Northrop Grumman Corporation Fiber reinforced ceramic matrix composite internal combustion engine intake/exhaust port liners
DE19730674A1 (de) * 1997-07-17 1999-01-21 Deutsch Zentr Luft & Raumfahrt Brennkammer und Verfahren zur Herstellung einer Brennkammer
DE19746598C2 (de) * 1997-10-22 2000-12-07 Dornier Gmbh Keramikverbundwerkstoff und seine Verwendung
FR2772049B1 (fr) * 1997-12-04 2000-02-18 Aerospatiale Piece en materiau composite a matrice metallique a haute rigidite et a grande stabilite dans une direction longitudinale
DE19801407C2 (de) * 1998-01-16 1999-12-02 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen
DE19802298C2 (de) * 1998-01-22 2000-11-23 Daimler Chrysler Ag Verfahren zur Erzielung funktioneller Metall-, Keramik- oder Keramik/Metall-Schichten auf der Innenwand von Hohlkörpern
DE19804232C2 (de) * 1998-02-04 2000-06-29 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen
DE19858197B4 (de) * 1998-12-17 2005-05-04 Eads Space Transportation Gmbh Triebwerk
DE19901422C2 (de) * 1999-01-18 2000-11-16 Daimler Chrysler Ag Brennkammer-Kühlstruktur für ein Raketentriebwerk
DE10126926B4 (de) * 2001-06-01 2015-02-19 Astrium Gmbh Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung
DE10318514B3 (de) * 2003-04-24 2004-09-16 Dornier Gmbh Mehrschichtiges keramisches Verbundmaterial mit thermischer Schutzwirkung

Also Published As

Publication number Publication date
US7293403B2 (en) 2007-11-13
US20030021974A1 (en) 2003-01-30
DE10126926B4 (de) 2015-02-19
SE0201656D0 (sv) 2002-05-31
JP4173975B2 (ja) 2008-10-29
ITMI20021190A0 (it) 2002-05-31
DE10126926A1 (de) 2002-12-12
JP2003014235A (ja) 2003-01-15
US20040128979A1 (en) 2004-07-08
US6890660B2 (en) 2005-05-10
FR2825417B1 (fr) 2006-12-08
FR2825417A1 (fr) 2002-12-06
ITMI20021190A1 (it) 2003-12-01
SE0201656L (sv) 2002-12-02

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NUG Patent has lapsed