CH324836A - Echangeur de chaleur - Google Patents

Echangeur de chaleur

Info

Publication number
CH324836A
CH324836A CH324836DA CH324836A CH 324836 A CH324836 A CH 324836A CH 324836D A CH324836D A CH 324836DA CH 324836 A CH324836 A CH 324836A
Authority
CH
Switzerland
Prior art keywords
heat exchanger
exchanger
heat
Prior art date
Application number
Other languages
English (en)
Inventor
Bernard Halford Frank
Stanley Snell Leonard
Original Assignee
Havilland Engine Company Limit
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
Priority to GB324836X priority Critical
Application filed by Havilland Engine Company Limit filed Critical Havilland Engine Company Limit
Publication of CH324836A publication Critical patent/CH324836A/fr

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
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion or thrust chambers having cooling arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0077Other 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
    • F28D2021/0078Other 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
    • 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
    • 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
    • Y10T29/49826Assembling or joining
    • Y10T29/49879Spaced wall tube or receptacle
CH324836D 1954-08-30 1955-08-30 Echangeur de chaleur CH324836A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB324836X 1954-08-30

Publications (1)

Publication Number Publication Date
CH324836A true CH324836A (fr) 1957-10-15

Family

ID=10339270

Family Applications (1)

Application Number Title Priority Date Filing Date
CH324836D CH324836A (fr) 1954-08-30 1955-08-30 Echangeur de chaleur

Country Status (4)

Country Link
US (1) US2880577A (fr)
CH (1) CH324836A (fr)
FR (1) FR1130311A (fr)
GB (1) GB794660A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2306028A2 (fr) * 1975-04-03 1976-10-29 Messerschmitt Boelkow Blohm Procede de realisation de pieces de revolution, notamment refroidies par un liquide, comme des tuyeres et chambres de combustion pour moteurs-fusees
DE3535779C1 (en) * 1985-10-07 1987-04-09 Messerschmitt Boelkow Blohm Arrangement for the cooling of rocket engine walls
EP0374382A1 (fr) * 1988-12-21 1990-06-27 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Refroidissement pour les organes de propulseurs hypersoniques

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB809844A (en) * 1956-07-05 1959-03-04 Armstrong Siddeley Motors Ltd Improvements in and relating to rocket motors
US3105522A (en) * 1956-12-10 1963-10-01 Robert C Veit Tube of uniform depth and variable width
US2976679A (en) * 1956-12-10 1961-03-28 Robert C Veit Tubular rocket combustion chamber
US2977754A (en) * 1958-01-29 1961-04-04 Thiokol Chemical Corp Rocket chamber with multi-pass axial flow coolant passageways
US3024606A (en) * 1958-07-10 1962-03-13 Curtiss Wright Corp Liquid cooling system for jet engines
US3043103A (en) * 1958-10-10 1962-07-10 Gen Motors Corp Liquid cooled wall
US2943442A (en) * 1959-01-09 1960-07-05 Edward F Baehr Rocket thrust chamber construction
US3064947A (en) * 1959-02-20 1962-11-20 United Aircraft Corp Involute flat tube and plate fin radiator
US3069850A (en) * 1959-05-18 1962-12-25 United Aircraft Corp Rocket nozzle with directional control
DE1118539B (de) * 1959-05-25 1961-11-30 United Aircraft Corp Raketenbrennkammer
US3086358A (en) * 1959-05-25 1963-04-23 United Aircraft Corp Rocket nozzle construction
US3066702A (en) * 1959-05-28 1962-12-04 United Aircraft Corp Cooled nozzle structure
US3004386A (en) * 1959-06-23 1961-10-17 United Aircraft Corp Rocket nozzle tube construction
US3001726A (en) * 1959-06-23 1961-09-26 United Aircraft Corp Manifold attachment
US3127667A (en) * 1959-06-23 1964-04-07 United Aircraft Corp Double thickness wall construction for rockets
US3062566A (en) * 1959-06-25 1962-11-06 United Aircraft Corp Manifold attachment to tubular wall
DE1135405B (de) * 1959-10-02 1962-08-30 Boelkow Entwicklungen Kg Verfahren zum Herstellen von fluessigkeitsgekuehlten Raketenbrennkammern
DE1164753B (de) * 1959-12-12 1964-03-05 Boelkow Entwicklungen Kg Raketentriebwerk fuer fluessige Treibstoffe
US3131535A (en) * 1960-04-07 1964-05-05 Pneumo Dynamics Corp Rocket nozzle
US3176464A (en) * 1960-05-24 1965-04-06 Martin Marietta Corp Ducted rocket engine
US3170286A (en) * 1962-03-26 1965-02-23 Stein Samuel Injector-valve device
US3289943A (en) * 1962-08-17 1966-12-06 Westinghouse Electric Corp Thermal barrier for thrust vehicle nozzle
US3534908A (en) * 1967-11-02 1970-10-20 North American Rockwell Variable geometry nozzle
US4148121A (en) * 1974-06-12 1979-04-10 Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung Method and apparatus for manufacturing rotationally symmetrical constructional parts such as nozzles and combination chambers of rocket engines
US4107919A (en) * 1975-03-19 1978-08-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Heat exchanger
DE2706715C3 (fr) * 1977-02-17 1981-07-16 M.A.N. Maschinenfabrik Augsburg-Nuernberg Ag, 8000 Muenchen, De
US4786015A (en) * 1986-12-31 1988-11-22 Sundstrand Corporation Structural cooling unit
DE4315256A1 (de) * 1993-05-07 1994-11-10 Mtu Muenchen Gmbh Einrichtung zur Verteilung sowie Zu- und Abführung eines Kühlmittels an einer Wand eines Turbo-, insbesondere Turbo-Staustrahltriebwerks
DE19915082C1 (de) 1999-04-01 2000-07-13 Daimler Chrysler Ag Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk
US6802179B2 (en) * 2002-12-02 2004-10-12 Aerojet-General Corporation Nozzle with spiral internal cooling channels
US20060016551A1 (en) * 2004-07-23 2006-01-26 Christensen Donald J Phenolic lamination process for hot gas components
JP4333587B2 (ja) * 2005-01-14 2009-09-16 三菱電機株式会社 ヒートシンクおよび冷却ユニット
SE531857C2 (sv) * 2007-12-21 2009-08-25 Volvo Aero Corp A component designed to be exposed to high thermal load during operation
US20190093602A1 (en) * 2017-09-25 2019-03-28 Shapefidelity, Inc. Rocket engine combustion chamber liner

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1655086A (en) * 1926-03-26 1928-01-03 Robert L Blanding Heat exchanger
US1935659A (en) * 1930-09-01 1933-11-21 Bbc Brown Boveri & Cie Pressureproof combustion chamber
DE716175C (de) * 1935-02-09 1942-01-14 Eugen Saenger Dr Ing Raketenmotor
US2520751A (en) * 1944-02-19 1950-08-29 Aerojet Engineering Corp Reaction motor with fluid cooling means
US2540594A (en) * 1946-08-23 1951-02-06 Lockheed Aircraft Corp Ram jet engine having variable area inlets

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2306028A2 (fr) * 1975-04-03 1976-10-29 Messerschmitt Boelkow Blohm Procede de realisation de pieces de revolution, notamment refroidies par un liquide, comme des tuyeres et chambres de combustion pour moteurs-fusees
DE3535779C1 (en) * 1985-10-07 1987-04-09 Messerschmitt Boelkow Blohm Arrangement for the cooling of rocket engine walls
EP0374382A1 (fr) * 1988-12-21 1990-06-27 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Refroidissement pour les organes de propulseurs hypersoniques

Also Published As

Publication number Publication date
US2880577A (en) 1959-04-07
GB794660A (en) 1958-05-07
FR1130311A (fr) 1957-02-04

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