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DE69525518D1 - Herstellung von Raketenkammern - Google Patents

Herstellung von Raketenkammern

Info

Publication number
DE69525518D1
DE69525518D1 DE69525518T DE69525518T DE69525518D1 DE 69525518 D1 DE69525518 D1 DE 69525518D1 DE 69525518 T DE69525518 T DE 69525518T DE 69525518 T DE69525518 T DE 69525518T DE 69525518 D1 DE69525518 D1 DE 69525518D1
Authority
DE
Germany
Prior art keywords
manufacture
rocket chambers
rocket
chambers
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
DE69525518T
Other languages
English (en)
Other versions
DE69525518T2 (de
Inventor
Mark L Hartman
Russell J Melnick
Daniel A Bales
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69525518D1 publication Critical patent/DE69525518D1/de
Application granted granted Critical
Publication of DE69525518T2 publication Critical patent/DE69525518T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion or thrust chambers having cooling arrangements
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49346Rocket or jet device making
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4935Heat exchanger or boiler making
    • Y10T29/49364Tube joined to flat sheet longitudinally, i.e., tube sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
DE69525518T 1994-11-30 1995-11-27 Herstellung von Raketenkammern Expired - Lifetime DE69525518T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/346,646 US5546656A (en) 1994-11-30 1994-11-30 Fabrication of rocket thrust chambers

Publications (2)

Publication Number Publication Date
DE69525518D1 true DE69525518D1 (de) 2002-03-28
DE69525518T2 DE69525518T2 (de) 2002-11-28

Family

ID=23360381

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69525518T Expired - Lifetime DE69525518T2 (de) 1994-11-30 1995-11-27 Herstellung von Raketenkammern

Country Status (4)

Country Link
US (1) US5546656A (de)
EP (1) EP0720876B1 (de)
JP (1) JP3702376B2 (de)
DE (1) DE69525518T2 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2733581B1 (fr) * 1995-04-27 1997-07-18 Europ Propulsion Enceinte de combustion avec refroidissement par transpiration
DE19845336A1 (de) 1998-10-01 2000-04-06 Behr Gmbh & Co Mehrkanal-Flachrohr
US6134782A (en) * 1998-11-30 2000-10-24 United Technologies Corporation Method of forming a rocket thrust chamber
US6131280A (en) * 1998-11-30 2000-10-17 United Technologies Corporation Method of repairing a rocket thrust chamber
DE19915082C1 (de) * 1999-04-01 2000-07-13 Daimler Chrysler Ag Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk
US6421998B1 (en) * 2000-06-13 2002-07-23 The Boeing Company Thruster device responsive to solar radiation
EP1352169B1 (de) * 2001-01-11 2008-04-30 Volvo Aero Corporation Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds
US7213392B2 (en) 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
US7219505B2 (en) * 2004-10-22 2007-05-22 York International Corporation Control stability system for moist air dehumidification units and method of operation
EP3717768B1 (de) * 2017-12-02 2022-12-14 Aerojet Rocketdyne, Inc. Kupferlegierungbrennkammer, die an der einspritzdüse durch einen nicht-kupfer-schweissübergangsring befestigt ist
CN109604436B (zh) * 2018-11-29 2020-11-03 湖北三江航天江北机械工程有限公司 液体火箭发动机推力室身部变截面异形单管的成形方法
DE102020124542A1 (de) * 2020-09-21 2022-03-24 Arianegroup Gmbh Brennkammer mit schwingungsdämpfender Innenwandform und Verfahren zum Herstellen eines Brennkammerabschnitts
CN114233516B (zh) * 2021-12-23 2023-05-09 南京航空航天大学 一种具有再生冷却功能的复合材料爆震发动机燃烧室结构

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968918A (en) * 1949-08-22 1961-01-24 California Inst Res Found Rocket motor shell construction
US3190070A (en) 1950-04-05 1965-06-22 Thiokol Chemical Corp Reaction motor construction
US3208132A (en) 1962-04-13 1965-09-28 William J D Escher Method of making a multi-walled chamber
US3349464A (en) * 1962-06-29 1967-10-31 Aerojet General Co Method of making rocket combustion chamber
DE1911642A1 (de) * 1968-03-15 1969-10-16 Man Turbo Gmbh Verfahren zur Herstellung der Brennkammer und/oder der Schubduese eines Raketentriebwerkes
FR2012723A1 (de) 1968-07-11 1970-03-20 Messerschmitt Boelkow Blohm
US3897316A (en) * 1972-05-17 1975-07-29 Us Air Force Method for manufacturing a composite wall for a regeneratively cooled thrust chamber of a liquid propellant rocket engine
JPS6082602A (ja) * 1983-10-07 1985-05-10 Natl Aerospace Lab ロケツト燃焼器外筒製作法
JPS6082603A (ja) * 1983-10-07 1985-05-10 Natl Aerospace Lab ロケツト燃焼器製作法
US4942653A (en) * 1989-08-25 1990-07-24 Rockwell International Corporation Production method for a channeled wall thrust nozzle
FR2669966B1 (fr) * 1990-11-30 1993-03-26 Europ Propulsion Procede de fabrication de paroi de chambre de combustion, notamment pour moteur-fusee, et chambre de combustion obtenue par ce procede.
US5386628A (en) * 1991-12-23 1995-02-07 United Technologies Corporation Method of making a diffusion bonded rocket chamber
US5371945A (en) * 1991-12-23 1994-12-13 United Technologies Corporation Method of making a tubular combustion chamber construction
US5375325A (en) * 1992-05-26 1994-12-27 United Technologies Corporation Method of making a rocket chamber construction
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

Also Published As

Publication number Publication date
EP0720876A2 (de) 1996-07-10
EP0720876B1 (de) 2002-02-20
JP3702376B2 (ja) 2005-10-05
EP0720876A3 (de) 1996-12-04
JPH08210184A (ja) 1996-08-20
US5546656A (en) 1996-08-20
DE69525518T2 (de) 2002-11-28

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition