DE69923099D1 - Produktionsweise für einen regenerativen Wärmetauschkreislauf für hohen Wärmefluss, insbesondere für Raketenbrennkammern - Google Patents

Produktionsweise für einen regenerativen Wärmetauschkreislauf für hohen Wärmefluss, insbesondere für Raketenbrennkammern

Info

Publication number
DE69923099D1
DE69923099D1 DE69923099T DE69923099T DE69923099D1 DE 69923099 D1 DE69923099 D1 DE 69923099D1 DE 69923099 T DE69923099 T DE 69923099T DE 69923099 T DE69923099 T DE 69923099T DE 69923099 D1 DE69923099 D1 DE 69923099D1
Authority
DE
Germany
Prior art keywords
production method
combustion chambers
exchange circuit
heat exchange
rocket combustion
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.)
Expired - Lifetime
Application number
DE69923099T
Other languages
English (en)
Other versions
DE69923099T2 (de
Inventor
Daniel Cornu
Christophe Verdy
Monicault Jean-Michel De
Christian Coddet
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 Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE69923099D1 publication Critical patent/DE69923099D1/de
Application granted granted Critical
Publication of DE69923099T2 publication Critical patent/DE69923099T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/008—Rocket engine parts, e.g. nozzles, combustion chambers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/26—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass heat exchangers or the like
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/137—Spraying in vacuum or in an inert atmosphere
    • 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
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device making

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Coating By Spraying Or Casting (AREA)
DE69923099T 1998-03-20 1999-03-19 Produktionsweise für einen regenerativen Wärmetauschkreislauf für hohen Wärmefluss, insbesondere für Raketenbrennkammern Expired - Lifetime DE69923099T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9803438A FR2776215B1 (fr) 1998-03-20 1998-03-20 Procede de fabrication d'un circuit regeneratif a fort flux thermique, notamment pour chambre de combustion de moteur-fusee
FR9803438 1998-03-20

Publications (2)

Publication Number Publication Date
DE69923099D1 true DE69923099D1 (de) 2005-02-17
DE69923099T2 DE69923099T2 (de) 2005-12-29

Family

ID=9524276

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69923099T Expired - Lifetime DE69923099T2 (de) 1998-03-20 1999-03-19 Produktionsweise für einen regenerativen Wärmetauschkreislauf für hohen Wärmefluss, insbesondere für Raketenbrennkammern

Country Status (6)

Country Link
US (2) US6209199B1 (de)
EP (1) EP0943795B1 (de)
JP (1) JP4358347B2 (de)
CN (1) CN1197685C (de)
DE (1) DE69923099T2 (de)
FR (1) FR2776215B1 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6131280A (en) 1998-11-30 2000-10-17 United Technologies Corporation Method of repairing a rocket thrust chamber
US6921014B2 (en) * 2002-05-07 2005-07-26 General Electric Company Method for forming a channel on the surface of a metal substrate
DE10343049B3 (de) * 2003-09-16 2005-04-14 Eads Space Transportation Gmbh Brennkammer mit Kühleinrichtung und Verfahren zur Herstellung der Brennkammer
EP1926904A4 (de) * 2005-09-06 2013-04-10 Volvo Aero Corp Motorwandstruktur und verfahren zur herstellung einer motorwandstruktur
ATE479017T1 (de) * 2005-09-06 2010-09-15 Volvo Aero Corp Verfahren zur herstellung einer motorwandstruktur
FR2915493B1 (fr) 2007-04-30 2009-07-24 Snecma Sa Procede pour realiser un depot sur un substrat recouvert de sic
US8815371B2 (en) * 2008-09-22 2014-08-26 Siemens Energy, Inc. Structure and method for forming detailed channels for thin walled components using thermal spraying
US20100243228A1 (en) * 2009-03-31 2010-09-30 Price Richard J Method and Apparatus to Effect Heat Transfer
FR2947871B1 (fr) * 2009-07-09 2011-11-25 Snecma Barriere anti-condensation sur circuit regeneratif
US8528208B2 (en) * 2011-04-11 2013-09-10 General Electric Company Methods of fabricating a coated component using multiple types of fillers
US8601691B2 (en) * 2011-04-27 2013-12-10 General Electric Company Component and methods of fabricating a coated component using multiple types of fillers
DE102013226594A1 (de) * 2013-12-19 2015-06-25 Robert Bosch Gmbh Verfahren zum Herstellen eines Laufrads und eines Läufers
US10211126B2 (en) * 2014-10-14 2019-02-19 University Of The Witwatersrand, Johannesburg Method of manufacturing an object with microchannels provided therethrough
JP5823069B1 (ja) * 2015-01-23 2015-11-25 三菱重工業株式会社 ロケットエンジンの燃焼器の製造方法、ロケットエンジンの燃焼器、および、ロケットエンジン
US11383316B2 (en) 2017-10-16 2022-07-12 Karl F. HRANKA Wire arc hybrid manufacturing
CN108999727A (zh) * 2018-10-15 2018-12-14 北京动力机械研究所 防冲刷水冷喷管结构
CN113894453B (zh) * 2021-09-15 2022-06-17 蓝箭航天空间科技股份有限公司 一种异种金属的燃烧室结构的加工方法及燃烧室
CN115415543A (zh) * 2022-08-09 2022-12-02 中国地质大学（武汉） 一种异种金属封闭流道的整体化增材制造方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1264160B (de) * 1966-12-15 1968-03-21 Boelkow Gmbh Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
FR2012723A1 (de) * 1968-07-11 1970-03-20 Messerschmitt Boelkow Blohm
DE2418889A1 (de) * 1974-04-19 1975-11-20 Messerschmitt Boelkow Blohm Thermisch und mechanisch hochbelastbare waermetauscher
DE2418841C3 (de) * 1974-04-19 1979-04-26 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Wärmetauscher, insbesondere regenerativ gekühlte Brennkammern für Flüssigkeitsraketentriebwerke und Verfahren zu ihrer Herstellung
US4108241A (en) * 1975-03-19 1978-08-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Heat exchanger and method of making
US6098402A (en) * 1989-02-10 2000-08-08 Sawruk; Stephen D. Infra-red stealth masking device (IRSMD)
US4942653A (en) * 1989-08-25 1990-07-24 Rockwell International Corporation Production method for a channeled wall thrust nozzle
US5075966A (en) * 1990-09-04 1991-12-31 General Electric Company Method for fabricating a hollow component for a rocket engine
US5249357A (en) * 1993-01-27 1993-10-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of fabricating a rocket engine combustion chamber
US5780157A (en) * 1994-06-06 1998-07-14 Ultramet Composite structure
US5613299A (en) * 1994-11-09 1997-03-25 Ring; Peter J. Method of fabricating a rocket thrust chamber
JPH1018911A (ja) * 1996-07-02 1998-01-20 Mitsubishi Heavy Ind Ltd 流通路形成方法
US5875549A (en) * 1997-03-17 1999-03-02 Siemens Westinghouse Power Corporation Method of forming internal passages within articles and articles formed by same

Also Published As

Publication number Publication date
FR2776215A1 (fr) 1999-09-24
EP0943795B1 (de) 2005-01-12
FR2776215B1 (fr) 2000-06-16
EP0943795A1 (de) 1999-09-22
DE69923099T2 (de) 2005-12-29
CN1197685C (zh) 2005-04-20
US6516872B1 (en) 2003-02-11
JPH11309631A (ja) 1999-11-09
CN1234316A (zh) 1999-11-10
US6209199B1 (en) 2001-04-03
JP4358347B2 (ja) 2009-11-04

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