GB1490641A - Heat exchangers for use under conditions of high thermal and mechanical loading - Google Patents

Heat exchangers for use under conditions of high thermal and mechanical loading

Info

Publication number
GB1490641A
GB1490641A GB1305175A GB1305175A GB1490641A GB 1490641 A GB1490641 A GB 1490641A GB 1305175 A GB1305175 A GB 1305175A GB 1305175 A GB1305175 A GB 1305175A GB 1490641 A GB1490641 A GB 1490641A
Authority
GB
United Kingdom
Prior art keywords
under conditions
heat exchangers
high thermal
use under
mechanical loading
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
Application number
GB1305175A
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 GB1490641A publication Critical patent/GB1490641A/en
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)

Abstract

1490641 Rocket combustion chambers MESSERSCHMITT-BOLKOW-BLOHM GmbH 27 March 1975 [19 April 1974] 13051/75 Headings F1J and F1L A regeneratively cooled rocket combustion chamber and thrust nozzle comprises inner and outer walls 1, 5 formed by an electro-plating process and defining cooling passages 2 therebetween, the inner wall at least being of dispersion-hardened metal, e.g. copper. The dispersoids used are specified. The walls of the coolant channels are coated with steel or aluminium or with a precious metal, e.g. gold. An intermediate layer 4 of gold or aluminium is galvanically deposited.
GB1305175A 1974-04-19 1975-03-27 Heat exchangers for use under conditions of high thermal and mechanical loading Expired GB1490641A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742418889 DE2418889A1 (en) 1974-04-19 1974-04-19 THERMALLY AND MECHANICALLY HEAT EXCHANGERS

Publications (1)

Publication Number Publication Date
GB1490641A true GB1490641A (en) 1977-11-02

Family

ID=5913323

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1305175A Expired GB1490641A (en) 1974-04-19 1975-03-27 Heat exchangers for use under conditions of high thermal and mechanical loading

Country Status (6)

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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2249141A (en) * 1990-05-11 1992-04-29 Mtu Muenchen Gmbh Thrust nozzle wall construction.
WO2006037494A2 (en) * 2004-09-30 2006-04-13 Carl Zeiss Smt Ag Device for adjusting the temperature of elements
EP2093409A3 (en) * 2008-02-25 2013-12-18 Deutsches Zentrum für Luft- und Raumfahrt e. V. Nozzle extension and method for manufacturing same

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4137638C2 (en) * 1991-11-15 1994-08-11 Mtu Muenchen Gmbh Component with a wall to be protected against thermal stress
FR2776215B1 (en) 1998-03-20 2000-06-16 Snecma PROCESS FOR MANUFACTURING A HIGH-THERMAL FLOW REGENERATIVE CIRCUIT, IN PARTICULAR FOR A FIREPLACE COMBUSTION CHAMBER
DE102005059502A1 (en) * 2005-12-06 2007-06-14 Deutsches Zentrum für Luft- und Raumfahrt e.V. hot chamber

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2249141A (en) * 1990-05-11 1992-04-29 Mtu Muenchen Gmbh Thrust nozzle wall construction.
GB2249141B (en) * 1990-05-11 1994-06-15 Mtu Muenchen Gmbh A thrust nozzle wall
WO2006037494A2 (en) * 2004-09-30 2006-04-13 Carl Zeiss Smt Ag Device for adjusting the temperature of elements
WO2006037494A3 (en) * 2004-09-30 2006-07-20 Zeiss Carl Smt Ag Device for adjusting the temperature of elements
EP2093409A3 (en) * 2008-02-25 2013-12-18 Deutsches Zentrum für Luft- und Raumfahrt e. V. Nozzle extension and method for manufacturing same

Also Published As

Publication number Publication date
DE2418889A1 (en) 1975-11-20
FR2268166A1 (en) 1975-11-14
FR2268166B3 (en) 1977-12-02
IT1037358B (en) 1979-11-10
IN144883B (en) 1978-07-22
JPS50140717A (en) 1975-11-12

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee