FR2744174B1 - Agencement de paroi pour des parois de propulseurs refroidies par circulation de propergols - Google Patents

Agencement de paroi pour des parois de propulseurs refroidies par circulation de propergols

Info

Publication number
FR2744174B1
FR2744174B1 FR9700656A FR9700656A FR2744174B1 FR 2744174 B1 FR2744174 B1 FR 2744174B1 FR 9700656 A FR9700656 A FR 9700656A FR 9700656 A FR9700656 A FR 9700656A FR 2744174 B1 FR2744174 B1 FR 2744174B1
Authority
FR
France
Prior art keywords
propergols
propeller
circulation
wall arrangement
cooled walls
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
FR9700656A
Other languages
English (en)
Other versions
FR2744174A1 (fr
Inventor
Gunther Schmidt
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
Daimler Benz Aerospace AG
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 Daimler Benz Aerospace AG filed Critical Daimler Benz Aerospace AG
Publication of FR2744174A1 publication Critical patent/FR2744174A1/fr
Application granted granted Critical
Publication of FR2744174B1 publication Critical patent/FR2744174B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)
FR9700656A 1996-01-26 1997-01-23 Agencement de paroi pour des parois de propulseurs refroidies par circulation de propergols Expired - Lifetime FR2744174B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19602731A DE19602731C1 (de) 1996-01-26 1996-01-26 Wandstruktur für treibstoffgekühlte Triebwerkswände

Publications (2)

Publication Number Publication Date
FR2744174A1 FR2744174A1 (fr) 1997-08-01
FR2744174B1 true FR2744174B1 (fr) 1999-12-10

Family

ID=7783722

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9700656A Expired - Lifetime FR2744174B1 (fr) 1996-01-26 1997-01-23 Agencement de paroi pour des parois de propulseurs refroidies par circulation de propergols

Country Status (4)

Country Link
US (1) US5899060A (fr)
JP (1) JP3004930B2 (fr)
DE (1) DE19602731C1 (fr)
FR (1) FR2744174B1 (fr)

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DE19801407C2 (de) * 1998-01-16 1999-12-02 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen
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
DE10126926B4 (de) * 2001-06-01 2015-02-19 Astrium Gmbh Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung
DE10126923B4 (de) 2001-06-01 2006-11-23 Eads Space Transportation Gmbh Raketentriebwerk mit Trennung von Innenmantel und Außenmantel
FR2836698B1 (fr) * 2002-03-04 2005-02-11 Eads Launch Vehicles Chambre de combustion pour statoreacteur et statoreacteur pourvu d'une telle chambre de combustion
RU2303155C2 (ru) * 2002-05-28 2007-07-20 Вольво Аэро Корпорейшн Конструкция стенки и элемент реактивного двигателя космического аппарата
ES2350847T3 (es) * 2005-09-06 2011-01-27 Volvo Aero Corporation Procedimiento para la fabricación de una estructura de pared de un motor.
EP1926904A4 (fr) * 2005-09-06 2013-04-10 Volvo Aero Corp Structure de paroi du moteur et procedes pour produire une structure de paroi du moteur
DE102005059502A1 (de) * 2005-12-06 2007-06-14 Deutsches Zentrum für Luft- und Raumfahrt e.V. Heißkammer
ES2439237T3 (es) 2006-12-06 2014-01-22 Gkn Aerospace Sweden Ab Un revestimiento para una sección de turbina
DE102007048527B4 (de) * 2007-10-10 2014-03-27 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Schubtriebwerk
US8453456B2 (en) * 2009-03-25 2013-06-04 United Technologies Corporation Fuel-cooled flexible heat exchanger with thermoelectric device compression
RU2517949C2 (ru) * 2012-02-02 2014-06-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Камера жидкосного ракетного двигателя
RU2513059C2 (ru) * 2012-02-02 2014-04-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Тракт охлаждения теплонапряженных конструкций
RU2516723C2 (ru) * 2012-02-03 2014-05-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ изготовления тракта регенеративного охлаждения камеры жидкостного ракетного двитателя
RU2515576C2 (ru) * 2012-02-03 2014-05-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Сопло камеры жидкостного ракетного двигателя
RU2516678C2 (ru) * 2012-02-03 2014-05-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Тракт регенеративного охлаждения камеры жидкостного ракетного двигателя
US10471542B1 (en) * 2017-06-27 2019-11-12 United States Of America As Represented By The Administrator Of Nasa Cladding and freeform deposition for coolant channel closeout
JP7324096B2 (ja) * 2019-09-13 2023-08-09 三菱重工業株式会社 冷却流路構造、バーナー及び熱交換器
EP3945245B1 (fr) * 2020-07-27 2024-02-07 Ansaldo Energia Switzerland AG Composant de trajet de gaz chaud pour une turbine à gaz à échangeur de chaleur intégré
CN113389657B (zh) * 2021-07-27 2022-09-30 中国人民解放军国防科技大学 一种高温流体通道

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NL69245C (fr) * 1946-01-09
US3190070A (en) * 1950-04-05 1965-06-22 Thiokol Chemical Corp Reaction motor construction
DE1197689B (de) * 1959-12-12 1965-07-29 Boelkow Gmbh Raketenbrennkammer
US3242670A (en) * 1962-08-27 1966-03-29 United Aircraft Corp Segmented baffle injector design
US3267664A (en) * 1963-03-19 1966-08-23 North American Aviation Inc Method of and device for cooling
US3280850A (en) * 1963-05-06 1966-10-25 North American Aviation Inc Hollow structural elements and methods for fabricating same
US3493177A (en) * 1967-07-26 1970-02-03 Trw Inc Method of and means for cooling the throat wall of rocket engine nozzle
US3798902A (en) * 1968-08-21 1974-03-26 Messerschmitt Boelkow Blohm Arrangement of cooling channels for rocket engine combustion chambers
DE1751938B1 (de) * 1968-08-21 1970-12-03 Messerschmitt Boelkow Blohm Verfahren zur Herstellung der Kuehlkanaele fuer Raketenbrennkammern mit konvergent-divergenter Schubduese
DE2137109C3 (de) * 1971-07-24 1980-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Herstellung einer regenerativ gekühlten Raketenbrennkammer
US3832290A (en) * 1972-09-14 1974-08-27 Nasa Method of electroforming a rocket chamber
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
US4840226A (en) * 1987-08-10 1989-06-20 The United States Of America As Represented By The United States Department Of Energy Corrosive resistant heat exchanger
US5172548A (en) * 1988-09-14 1992-12-22 Societe Europeene De Propulsion Device for tapping off hot gases from a combustion chamber and injector head equipped with such a device
FR2664585B1 (fr) * 1990-07-13 1993-08-06 Europ Propulsion Structures refractaires refroidies et procede pour leur fabrication.
DE4115403A1 (de) * 1991-05-10 1992-11-12 Mtu Muenchen Gmbh Duesenwand
DE4137638C2 (de) * 1991-11-15 1994-08-11 Mtu Muenchen Gmbh Bauteil mit einer vor thermischer Belastung zu schützenden Wand
DE4443864A1 (de) * 1994-12-09 1996-06-13 Abb Management Ag Gek}hltes Wandteil

Also Published As

Publication number Publication date
JP3004930B2 (ja) 2000-01-31
JPH09217654A (ja) 1997-08-19
FR2744174A1 (fr) 1997-08-01
US5899060A (en) 1999-05-04
DE19602731C1 (de) 1997-07-10

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