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FR2268166A1 - - Google Patents

Info

Publication number
FR2268166A1
FR2268166A1 FR7509545A FR7509545A FR2268166A1 FR 2268166 A1 FR2268166 A1 FR 2268166A1 FR 7509545 A FR7509545 A FR 7509545A FR 7509545 A FR7509545 A FR 7509545A FR 2268166 A1 FR2268166 A1 FR 2268166A1
Authority
FR
France
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.)
Granted
Application number
FR7509545A
Other versions
FR2268166B3 (fr
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
Messerschmitt Bolkow Blohm 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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2268166A1 publication Critical patent/FR2268166A1/fr
Application granted granted Critical
Publication of FR2268166B3 publication Critical patent/FR2268166B3/fr
Expired 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F13/18—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by applying coatings, e.g. radiation-absorbing, radiation-reflecting; by surface treatment, e.g. polishing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0077—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for tempering, e.g. with cooling or heating circuits for temperature control of elements
    • F28D2021/0078—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for tempering, e.g. with cooling or heating circuits for temperature control of elements in the form of cooling walls

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Electroplating Methods And Accessories (AREA)
FR7509545A 1974-04-19 1975-03-26 Expired FR2268166B3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742418889 DE2418889A1 (de) 1974-04-19 1974-04-19 Thermisch und mechanisch hochbelastbare waermetauscher

Publications (2)

Publication Number Publication Date
FR2268166A1 true FR2268166A1 (fr) 1975-11-14
FR2268166B3 FR2268166B3 (fr) 1977-12-02

Family

ID=5913323

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7509545A Expired FR2268166B3 (fr) 1974-04-19 1975-03-26

Country Status (6)

Country Link
JP (1) JPS50140717A (fr)
DE (1) DE2418889A1 (fr)
FR (1) FR2268166B3 (fr)
GB (1) GB1490641A (fr)
IN (1) IN144883B (fr)
IT (1) IT1037358B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0943795A1 (fr) * 1998-03-20 1999-09-22 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Procédé de fabrication d'un circuit régénératif à fort flux thermique, notamment pour chambre de combustion de moteur-fusée

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4015204C1 (fr) * 1990-05-11 1991-10-17 Mtu Muenchen Gmbh
DE4137638C2 (de) * 1991-11-15 1994-08-11 Mtu Muenchen Gmbh Bauteil mit einer vor thermischer Belastung zu schützenden Wand
DE102004047533A1 (de) * 2004-09-30 2006-04-06 Carl Zeiss Smt Ag Vorrichtung zur Temperierung von Elementen
DE102005059502A1 (de) * 2005-12-06 2007-06-14 Deutsches Zentrum für Luft- und Raumfahrt e.V. Heißkammer
DE102008011502A1 (de) * 2008-02-25 2009-09-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Düsenerweiterung und Verfahren zur Herstellung einer Düsenerweiterung

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0943795A1 (fr) * 1998-03-20 1999-09-22 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Procédé de fabrication d'un circuit régénératif à fort flux thermique, notamment pour chambre de combustion de moteur-fusée
FR2776215A1 (fr) * 1998-03-20 1999-09-24 Snecma Procede de fabrication d'un circuit regeneratif a fort flux thermique, notamment pour chambre de combustion de moteur-fusee
US6209199B1 (en) 1998-03-20 2001-04-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation- S.N.E.C.M.A. Method of manufacturing a high heat flux regenerative circuit, in particular for the combustion chamber of a rocket engine
US6516872B1 (en) 1998-03-20 2003-02-11 Societe Nationale D'etude Et De Construction De Moteurs D'aviation -S.N.E.C.M.A. High heat flux regenerative circuit, in particular for the combustion chamber of a rocket engine

Also Published As

Publication number Publication date
FR2268166B3 (fr) 1977-12-02
DE2418889A1 (de) 1975-11-20
JPS50140717A (fr) 1975-11-12
IT1037358B (it) 1979-11-10
IN144883B (fr) 1978-07-22
GB1490641A (en) 1977-11-02

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Legal Events

Date Code Title Description
ST Notification of lapse