SE0001068D0 - Förfarande för tillverkning av en kyld dysa för en raketmotor - Google Patents

Förfarande för tillverkning av en kyld dysa för en raketmotor

Info

Publication number
SE0001068D0
SE0001068D0 SE0001068A SE0001068A SE0001068D0 SE 0001068 D0 SE0001068 D0 SE 0001068D0 SE 0001068 A SE0001068 A SE 0001068A SE 0001068 A SE0001068 A SE 0001068A SE 0001068 D0 SE0001068 D0 SE 0001068D0
Authority
SE
Sweden
Prior art keywords
composite structure
nozzle
rocket engine
manufacturing
fixed
Prior art date
Application number
SE0001068A
Other languages
English (en)
Other versions
SE0001068L (sv
SE520969C2 (sv
Inventor
Joachim Kretschmer
Original Assignee
Daimler Chrysler 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 Daimler Chrysler Ag filed Critical Daimler Chrysler Ag
Publication of SE0001068D0 publication Critical patent/SE0001068D0/sv
Publication of SE0001068L publication Critical patent/SE0001068L/sv
Publication of SE520969C2 publication Critical patent/SE520969C2/sv

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
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/008—Rocket engine parts, e.g. nozzles, combustion chambers
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/40—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
    • F02K9/42—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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/15—Two-dimensional spiral
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/25—Three-dimensional helical
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Moulding By Coating Moulds (AREA)
SE0001068A 1999-04-01 2000-03-27 Förfarande för tillverkning av en kyld dysa för en raketmotor samt en dysa för en raketmotor SE520969C2 (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19915082A DE19915082C1 (de) 1999-04-01 1999-04-01 Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk

Publications (3)

Publication Number Publication Date
SE0001068D0 true SE0001068D0 (sv) 2000-03-27
SE0001068L SE0001068L (sv) 2000-10-02
SE520969C2 SE520969C2 (sv) 2003-09-16

Family

ID=7903388

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0001068A SE520969C2 (sv) 1999-04-01 2000-03-27 Förfarande för tillverkning av en kyld dysa för en raketmotor samt en dysa för en raketmotor

Country Status (5)

Country Link
US (2) US6470671B1 (sv)
JP (1) JP4465485B2 (sv)
DE (1) DE19915082C1 (sv)
FR (1) FR2791589B1 (sv)
SE (1) SE520969C2 (sv)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4537509B2 (ja) * 1998-05-07 2010-09-01 株式会社リコー 画像形成装置
FR2836699B1 (fr) 2002-03-04 2005-02-11 Eads Launch Vehicles Moteur de fusee
US6883220B2 (en) * 2002-07-17 2005-04-26 The Boeing Company Method for forming a tube-walled article
EP1398569A1 (de) * 2002-09-13 2004-03-17 Siemens Aktiengesellschaft Gasturbine
CA2444917A1 (en) * 2002-10-18 2004-04-18 United Technologies Corporation Cold sprayed copper for rocket engine applications
US6802179B2 (en) * 2002-12-02 2004-10-12 Aerojet-General Corporation Nozzle with spiral internal cooling channels
US20070163228A1 (en) * 2006-01-19 2007-07-19 United Technologies Corporation Gas augmented rocket engine
JP4887133B2 (ja) * 2006-12-21 2012-02-29 株式会社リコー 画像形成装置
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
FR2915528B1 (fr) * 2007-04-25 2012-07-06 Astrium Sas Procede et dispositif pour alimenter un moteur de propulsion spatiale en ergols cryogeniques liquides.
DE102010019958B4 (de) * 2010-05-08 2016-05-04 MTU Aero Engines AG Verfahren zur Herstellung eines Einlaufbelags
RU2480610C1 (ru) * 2012-01-11 2013-04-27 Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" Камера жидкостного ракетного двигателя
RU2480611C1 (ru) * 2012-01-11 2013-04-27 Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" Способ изготовления камеры жидкостного ракетного двигателя
JP6289652B2 (ja) 2014-09-25 2018-03-07 合同会社パッチドコニックス 流体を加圧し供給する装置、システム、および方法。
CN105710606A (zh) * 2015-11-25 2016-06-29 沈阳黎明航空发动机(集团)有限责任公司 一种燃气发生器喷嘴头的加工方法
US9835114B1 (en) 2017-06-06 2017-12-05 The United States Of America As Represented By The Administrator Of Nasa Freeform deposition method for coolant channel closeout
US10471542B1 (en) * 2017-06-27 2019-11-12 United States Of America As Represented By The Administrator Of Nasa Cladding and freeform deposition for coolant channel closeout
CN110925114A (zh) * 2019-12-27 2020-03-27 哈尔滨工程大学 一种发动机壳体冷却装置

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3190070A (en) * 1950-04-05 1965-06-22 Thiokol Chemical Corp Reaction motor construction
GB794660A (en) * 1954-08-30 1958-05-07 Havilland Engine Co Ltd Heat exchangers
US3241311A (en) * 1957-04-05 1966-03-22 United Aircraft Corp Turbofan engine
US3099909A (en) * 1959-05-21 1963-08-06 United Aircraft Corp Nozzle construction
US3170286A (en) * 1962-03-26 1965-02-23 Stein Samuel Injector-valve device
US3349464A (en) * 1962-06-29 1967-10-31 Aerojet General Co Method of making rocket combustion chamber
US3289943A (en) * 1962-08-17 1966-12-06 Westinghouse Electric Corp Thermal barrier for thrust vehicle nozzle
US3224678A (en) * 1962-10-04 1965-12-21 Marquardt Corp Modular thrust chamber
US3170266A (en) 1962-11-07 1965-02-23 Reynolds Metals Co Soffit systems
US3267664A (en) * 1963-03-19 1966-08-23 North American Aviation Inc Method of and device for cooling
DE1264160B (de) * 1966-12-15 1968-03-21 Boelkow Gmbh Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
US3460759A (en) * 1967-03-07 1969-08-12 Nasa Combustion chamber
US3692637A (en) * 1969-11-24 1972-09-19 Carl Helmut Dederra Method of fabricating a hollow structure having cooling channels
US3897316A (en) * 1972-05-17 1975-07-29 Us Air Force Method for manufacturing a composite wall for a regeneratively cooled thrust chamber of a liquid propellant rocket engine
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
DE2522681C2 (de) * 1975-05-22 1983-04-14 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorrichtung zur Montage von spiralförmig gebogenen Rohren zur Herstellung von rotationssymmetrischen Bauteilen
US4131057A (en) * 1976-09-29 1978-12-26 Phillips Petroleum Company Apparatus for forming a convoluted container sidewall
FR2482666B1 (fr) * 1980-05-19 1985-06-21 Europ Propulsion Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur
DE3942022A1 (de) * 1989-12-20 1991-06-27 Mtu Muenchen Gmbh Verfahren und vorrichtung zur kuehlung eines flugtriebwerkes
US5221045A (en) * 1991-09-23 1993-06-22 The Babcock & Wilcox Company Bulge formed cooling channels with a variable lead helix on a hollow body of revolution
DE4301041C1 (de) * 1993-01-16 1994-04-28 Deutsche Aerospace Verfahren zur Herstellung einer fluidgekühlten Wand in Röhrchenverbundbauweise
DE4326338C2 (de) * 1993-08-05 1996-07-18 Daimler Benz Aerospace Ag Schweißroboter
US5546656A (en) * 1994-11-30 1996-08-20 United Technologies Corporation Fabrication of rocket thrust chambers
DE19520885C2 (de) * 1995-06-08 1999-05-20 Daimler Benz Ag Verfahren zum thermischen Spritzen von Schichten aus Metallegierungen oder Metallen und seine Verwendung

Also Published As

Publication number Publication date
JP4465485B2 (ja) 2010-05-19
US20020056762A1 (en) 2002-05-16
JP2000320404A (ja) 2000-11-21
US6543135B2 (en) 2003-04-08
SE0001068L (sv) 2000-10-02
US6470671B1 (en) 2002-10-29
FR2791589B1 (fr) 2001-11-16
SE520969C2 (sv) 2003-09-16
DE19915082C1 (de) 2000-07-13
FR2791589A1 (fr) 2000-10-06

Similar Documents

Publication Publication Date Title
SE0001068D0 (sv) Förfarande för tillverkning av en kyld dysa för en raketmotor
JP3947519B2 (ja) 複合壁の製造方法
US5231833A (en) Gas turbine engine fuel manifold
US4827588A (en) Method of making a turbine nozzle
RU2330162C2 (ru) Высокотемпературная слоистая система для теплоотвода и способ для ее изготовления (варианты)
RU2141564C1 (ru) Воздушная турбина, в частности, небольшого диаметра из термоконструкционного композиционного материала и способ ее изготовления
US9840925B2 (en) Axial turbomachine compressor outer casing
ATE303866T1 (de) Mehrschichtiger katalysator und dessen herstellungsverfahren
CA2379218A1 (en) Pilot nozzle for a gas turbine combustor and supply path converter
RU2003133393A (ru) Камера сгорания реактивного двигателя со сборными образующими ее горловину конфорными несущими облицовку элементами
RU2004136269A (ru) Использование напыленного покрытия для достижения неравномерных уплотненных зазоров в турбомашинах
JP2004093125A5 (sv)
JPS6151123B2 (sv)
US6134782A (en) Method of forming a rocket thrust chamber
EP1319823A3 (en) Method of producing an insultated rocket engine casing and insulated casing produced in this way
US3773593A (en) Method of making hot gas manifold
US3035333A (en) Method of making a regeneratively cooled combustion chamber
JPS6064129A (ja) 燃焼タービンの燃焼器
EP1352166B1 (en) An outlet nozzle and a method for manufacturing an outlet nozzle
ATE356288T1 (de) Brennkammerstruktur und verfahren zu deren herstellung
EP3663563A1 (en) Casing with integral cavity
US20200377428A1 (en) Solid Rocket Motor Propellant Manufacture and Configurations
US3189500A (en) Method of making a composite multiwalled pressure vessel
US7234294B1 (en) Outlet nozzle and a method for manufacturing an outlet nozzle
RU2007607C1 (ru) Кольцевое сопло ракетного двигателя твердого топлива