GB1343064A - Process for the production of a combustion chamber and/or thrust nozzle provided with cooling channels by a galvano- plastic process - Google Patents

Process for the production of a combustion chamber and/or thrust nozzle provided with cooling channels by a galvano- plastic process

Info

Publication number
GB1343064A
GB1343064A GB2490671*A GB2490671A GB1343064A GB 1343064 A GB1343064 A GB 1343064A GB 2490671 A GB2490671 A GB 2490671A GB 1343064 A GB1343064 A GB 1343064A
Authority
GB
United Kingdom
Prior art keywords
core
cooling channels
galvanizing
wall
galvano
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
GB2490671*A
Other languages
English (en)
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 GB1343064A publication Critical patent/GB1343064A/en
Expired legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D1/00—Electroforming
    • 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
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S29/00—Metal working
    • Y10S29/012—Method or apparatus with electroplating
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device making

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Electrochemistry (AREA)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Testing Of Engines (AREA)
GB2490671*A 1970-03-28 1971-04-19 Process for the production of a combustion chamber and/or thrust nozzle provided with cooling channels by a galvano- plastic process Expired GB1343064A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19702015024 DE2015024B2 (de) 1970-03-28 1970-03-28 Verfahren zur herstellung von regenerativ gekuehlten brenn kammern und oder schubduesen
US12353571A 1971-03-12 1971-03-12
US00341361A US3835644A (en) 1970-03-28 1973-03-15 Regeneratively cooled rocket combustion chamber and thrust novel assembly

Publications (1)

Publication Number Publication Date
GB1343064A true GB1343064A (en) 1974-01-10

Family

ID=27182498

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2490671*A Expired GB1343064A (en) 1970-03-28 1971-04-19 Process for the production of a combustion chamber and/or thrust nozzle provided with cooling channels by a galvano- plastic process

Country Status (4)

Country Link
US (2) US3738916A (enExample)
DE (1) DE2015024B2 (enExample)
FR (1) FR2083964A5 (enExample)
GB (1) GB1343064A (enExample)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2406976A1 (de) * 1974-02-14 1975-09-04 Messerschmitt Boelkow Blohm Verfahren zur herstellung von brennkammern und/oder schubduesen fuer fluessigkeitsraketentriebwerke
DE2550952C3 (de) * 1975-11-13 1982-01-14 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zur galvanoplastischen Serienherstellung von Raketenbrennkammer- oder -schubdüsenteilen
DE2550951C3 (de) * 1975-11-13 1981-12-17 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Leichtbauteil
DE2657474A1 (de) * 1976-12-18 1978-06-22 Messerschmitt Boelkow Blohm Verfahren zum herstellen von regenerativ gekuehlten raketenbrennkammern und/oder schubduesen
JPS54152766A (en) * 1978-05-24 1979-12-01 Yamatake Honeywell Co Ltd Fluid circuit device
DE2828993C2 (de) * 1978-07-01 1984-04-12 Kernforschungszentrum Karlsruhe Gmbh, 7500 Karlsruhe Verfahren zur galvanoplastischen Herstellung eines Düsenkörpers
DE3011282C2 (de) * 1980-03-24 1985-08-08 Kernforschungsanlage Juelich Gmbh, 5170 Juelich Wärmeabsorber, insbesondere Plasmastrahlenabsorber
DE3017515A1 (de) * 1980-05-07 1981-11-12 Rudolf Ing. Mutters Zlotek sen. Waermetauscher
DE3029499A1 (de) * 1980-08-04 1982-03-04 Dieter Dipl.-Ing. 8013 Haar Hayn Herstellungsverfahren fuer miniatur-lavalduesen mit definierter geometrie im halsbereich
DE3436419C2 (de) * 1983-10-07 1990-11-15 Yoshimichi Chigasaki Kanagawa Masuda Verfahren zur Herstellung von Raketenbrennkammern
US4707225A (en) * 1986-01-06 1987-11-17 Rockwell International Corporation Fluid-cooled channel construction
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.
US5557928A (en) * 1994-08-16 1996-09-24 United Technologies Corporation Tube rocket thrust chamber construction and method
US5832719A (en) * 1995-12-18 1998-11-10 United Technologies Corporation Rocket thrust chamber
DE19901422C2 (de) 1999-01-18 2000-11-16 Daimler Chrysler Ag Brennkammer-Kühlstruktur für ein Raketentriebwerk
EP1398569A1 (de) * 2002-09-13 2004-03-17 Siemens Aktiengesellschaft Gasturbine
US7464537B2 (en) * 2005-04-04 2008-12-16 United Technologies Corporation Heat transfer enhancement features for a tubular wall combustion chamber
DE102008011502A1 (de) 2008-02-25 2009-09-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Düsenerweiterung und Verfahren zur Herstellung einer Düsenerweiterung
EP3945245B1 (en) * 2020-07-27 2024-02-07 Ansaldo Energia Switzerland AG Hot gas path component for a gas turbine with built-in heat exchanger
CN114483382B (zh) * 2021-12-29 2023-07-14 北京航天动力研究所 一种3d打印一体化喷管延伸段

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3022230A (en) * 1959-06-16 1962-02-20 Camin Lab Inc Process for electroforming grooved and channeled bodies
US3445348A (en) * 1965-05-12 1969-05-20 Honeywell Inc Cellular structure and method of manufacture
US3467583A (en) * 1966-05-16 1969-09-16 Camin Lab Process for making a hollow body with protective inner layer for high-temperature applications
US3520357A (en) * 1967-07-03 1970-07-14 North American Rockwell Open core sandwich-structure
US3686081A (en) * 1969-01-31 1972-08-22 Messerschmitt Boelkow Blohm Method for incorporating strength increasing filler materials in a matrix
US3692637A (en) * 1969-11-24 1972-09-19 Carl Helmut Dederra Method of fabricating a hollow structure having cooling channels

Also Published As

Publication number Publication date
DE2015024B2 (de) 1971-10-14
FR2083964A5 (enExample) 1971-12-17
DE2015024A1 (enExample) 1971-10-14
US3738916A (en) 1973-06-12
US3835644A (en) 1974-09-17

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee