DE2015024A1 - - Google Patents

Info

Publication number
DE2015024A1
DE2015024A1 DE19702015024 DE2015024A DE2015024A1 DE 2015024 A1 DE2015024 A1 DE 2015024A1 DE 19702015024 DE19702015024 DE 19702015024 DE 2015024 A DE2015024 A DE 2015024A DE 2015024 A1 DE2015024 A1 DE 2015024A1
Authority
DE
Germany
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.)
Withdrawn
Application number
DE19702015024
Other versions
DE2015024B2 (de
DE2015024C (de
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 filed Critical
Priority to DE19702015024 priority Critical patent/DE2015024B2/de
Priority to JP12194370A priority patent/JPS4918904B1/ja
Priority to FR7106516A priority patent/FR2083964A5/fr
Priority to US00123535A priority patent/US3738916A/en
Priority to GB2490671*A priority patent/GB1343064A/en
Publication of DE2015024A1 publication Critical patent/DE2015024A1/de
Publication of DE2015024B2 publication Critical patent/DE2015024B2/de
Priority to US00341361A priority patent/US3835644A/en
Withdrawn legal-status Critical Current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
DE19702015024 1970-03-28 1970-03-28 Verfahren zur herstellung von regenerativ gekuehlten brenn kammern und oder schubduesen Withdrawn DE2015024B2 (de)

Priority Applications (6)

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
JP12194370A JPS4918904B1 (de) 1970-03-28 1970-12-29
FR7106516A FR2083964A5 (de) 1970-03-28 1971-02-25
US00123535A US3738916A (en) 1970-03-28 1971-03-12 Process for the production of regeneratively cooled rocket combustionchambers and thrust nozzle assemblies
GB2490671*A 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
US00341361A US3835644A (en) 1970-03-28 1973-03-15 Regeneratively cooled rocket combustion chamber and thrust novel assembly

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 (2)

Publication Number Publication Date
DE2015024A1 true DE2015024A1 (de) 1971-10-14
DE2015024B2 DE2015024B2 (de) 1971-10-14

Family

ID=27182498

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19702015024 Withdrawn DE2015024B2 (de) 1970-03-28 1970-03-28 Verfahren zur herstellung von regenerativ gekuehlten brenn kammern und oder schubduesen

Country Status (4)

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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3436419A1 (de) * 1983-10-07 1985-05-02 Yoshimichi Chigasaki Kanagawa Masuda Verfahren zur herstellung von raketenbrennkammern
US5233755A (en) * 1990-11-30 1993-08-10 Societe Europeenne De Propulsion Method of manufacturing the wall of a combustion chamber, in particular for a rocket engine, and a combustion chamber obtained by the method
EP2093409A2 (de) 2008-02-25 2009-08-26 Deutches Zentrum für Luft- und Ramfahrt e. V. Düsenerweiterung und Verfahren zur Herstellung einer Düsenerweiterung

Families Citing this family (16)

* 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
DE2550951C3 (de) * 1975-11-13 1981-12-17 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Leichtbauteil
DE2550952C3 (de) * 1975-11-13 1982-01-14 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zur galvanoplastischen Serienherstellung von Raketenbrennkammer- oder -schubdüsenteilen
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
US4707225A (en) * 1986-01-06 1987-11-17 Rockwell International Corporation Fluid-cooled channel construction
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
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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3436419A1 (de) * 1983-10-07 1985-05-02 Yoshimichi Chigasaki Kanagawa Masuda Verfahren zur herstellung von raketenbrennkammern
US5233755A (en) * 1990-11-30 1993-08-10 Societe Europeenne De Propulsion Method of manufacturing the wall of a combustion chamber, in particular for a rocket engine, and a combustion chamber obtained by the method
EP2093409A2 (de) 2008-02-25 2009-08-26 Deutches Zentrum für Luft- und Ramfahrt e. V. Düsenerweiterung und Verfahren zur Herstellung einer Düsenerweiterung

Also Published As

Publication number Publication date
FR2083964A5 (de) 1971-12-17
US3835644A (en) 1974-09-17
DE2015024B2 (de) 1971-10-14
US3738916A (en) 1973-06-12
GB1343064A (en) 1974-01-10

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Legal Events

Date Code Title Description
E77 Valid patent as to the heymanns-index 1977
8339 Ceased/non-payment of the annual fee