AU2003223917A1 - Method for the production of soldered heat-exchanger structures, particularly regeneratively cooled combustion chambers - Google Patents

Method for the production of soldered heat-exchanger structures, particularly regeneratively cooled combustion chambers

Info

Publication number
AU2003223917A1
AU2003223917A1 AU2003223917A AU2003223917A AU2003223917A1 AU 2003223917 A1 AU2003223917 A1 AU 2003223917A1 AU 2003223917 A AU2003223917 A AU 2003223917A AU 2003223917 A AU2003223917 A AU 2003223917A AU 2003223917 A1 AU2003223917 A1 AU 2003223917A1
Authority
AU
Australia
Prior art keywords
production
combustion chambers
cooled combustion
exchanger structures
regeneratively cooled
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
AU2003223917A
Other languages
English (en)
Inventor
Frank Palm
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.)
Airbus Defence and Space GmbH
Original Assignee
EADS Deutschland 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 EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Publication of AU2003223917A1 publication Critical patent/AU2003223917A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00—Soldering, e.g. brazing, or unsoldering
    • B23K1/0008—Soldering, e.g. brazing, or unsoldering specially adapted for particular articles or work
    • B23K1/0012—Brazing heat exchangers
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/04—Tubular or hollow articles
    • B23K2101/14—Heat exchangers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Ceramic Products (AREA)
AU2003223917A 2002-04-30 2003-04-12 Method for the production of soldered heat-exchanger structures, particularly regeneratively cooled combustion chambers Abandoned AU2003223917A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10219502.1 2002-04-30
DE10219502A DE10219502B4 (de) 2002-04-30 2002-04-30 Verfahren zum Herstellen gelöteter Wärmetauscherstrukturen, insbesondere regenerativ gekühlter Brennkammern
PCT/DE2003/001243 WO2003092946A1 (de) 2002-04-30 2003-04-12 Verfahren zum herstellen gelöteter wärmetauscherstrukturen, insbesondere regenerativ gekühlter brennkammern

Publications (1)

Publication Number Publication Date
AU2003223917A1 true AU2003223917A1 (en) 2003-11-17

Family

ID=29264969

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003223917A Abandoned AU2003223917A1 (en) 2002-04-30 2003-04-12 Method for the production of soldered heat-exchanger structures, particularly regeneratively cooled combustion chambers

Country Status (3)

Country Link
AU (1) AU2003223917A1 (de)
DE (1) DE10219502B4 (de)
WO (1) WO2003092946A1 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008069705A1 (en) 2006-12-06 2008-06-12 Volvo Aero Corporation A liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith
DE102007048527B4 (de) * 2007-10-10 2014-03-27 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Schubtriebwerk
FR2994115B1 (fr) * 2012-08-02 2015-02-20 Aircelle Sa Ensemble d'outillage pour la fabrication d'une piece metallique de revolution et procede de fabrication d'une telle piece
FR3004368B1 (fr) 2013-04-15 2015-09-25 Aircelle Sa Brasage sans outillage

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2406976A1 (de) * 1974-02-14 1975-09-04 Messerschmitt Boelkow Blohm Verfahren zur herstellung von brennkammern und/oder schubduesen fuer fluessigkeitsraketentriebwerke
GB2085785A (en) * 1980-10-22 1982-05-06 Serck Industries Ltd Methods of securing a hollow elongate member in an opening in a further member
US5386628A (en) * 1991-12-23 1995-02-07 United Technologies Corporation Method of making a diffusion bonded rocket chamber
DE19804232C2 (de) * 1998-02-04 2000-06-29 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen
US6065664A (en) * 1998-08-10 2000-05-23 Thermal Corp. Method of installing heat pipes using internal vapor pressure
DE19901422C2 (de) * 1999-01-18 2000-11-16 Daimler Chrysler Ag Brennkammer-Kühlstruktur für ein Raketentriebwerk

Also Published As

Publication number Publication date
WO2003092946B1 (de) 2004-02-19
DE10219502A1 (de) 2003-11-20
DE10219502B4 (de) 2004-09-16
WO2003092946A1 (de) 2003-11-13

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase