SE512942C2 - Förfarande för tillverkning av utloppsmunstycken för raketmotorer - Google Patents

Förfarande för tillverkning av utloppsmunstycken för raketmotorer

Info

Publication number
SE512942C2
SE512942C2 SE9803387A SE9803387A SE512942C2 SE 512942 C2 SE512942 C2 SE 512942C2 SE 9803387 A SE9803387 A SE 9803387A SE 9803387 A SE9803387 A SE 9803387A SE 512942 C2 SE512942 C2 SE 512942C2
Authority
SE
Sweden
Prior art keywords
wall
outlet nozzle
spacer element
cooling
rocket engine
Prior art date
Application number
SE9803387A
Other languages
English (en)
Swedish (sv)
Other versions
SE9803387L (sv
SE9803387D0 (sv
Inventor
Jan Lundgren
Original Assignee
Volvo Aero Corp
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 Volvo Aero Corp filed Critical Volvo Aero Corp
Priority to SE9803387A priority Critical patent/SE512942C2/sv
Publication of SE9803387D0 publication Critical patent/SE9803387D0/xx
Priority to US09/806,607 priority patent/US6591499B1/en
Priority to JP2000574828A priority patent/JP3890195B2/ja
Priority to RU2001111830/06A priority patent/RU2209994C2/ru
Priority to PCT/SE1999/001727 priority patent/WO2000020749A1/en
Priority to EP99970150A priority patent/EP1117918B1/de
Priority to DE69918452T priority patent/DE69918452T2/de
Priority to CN99811689A priority patent/CN1107164C/zh
Publication of SE9803387L publication Critical patent/SE9803387L/
Publication of SE512942C2 publication Critical patent/SE512942C2/sv
Priority to US10/370,536 priority patent/US6907662B2/en
Priority to US10/872,667 priority patent/US6945032B2/en

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
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20—Bonding
    • B23K26/21—Bonding by welding
    • B23K26/24—Seam welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20—Bonding
    • B23K26/21—Bonding by welding
    • B23K26/24—Seam welding
    • B23K26/28—Seam welding of curved planar seams
    • B23K26/282—Seam welding of curved planar seams of tube sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/04—Tubular or hollow articles
    • B23K2101/045—Hollow panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/04—Tubular or hollow articles
    • B23K2101/14—Heat exchangers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/18—Sheet panels
    • 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
    • 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
    • Y10T29/49995—Shaping one-piece blank by removing material

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Mechanical Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Laser Beam Processing (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
SE9803387A 1998-10-02 1998-10-02 Förfarande för tillverkning av utloppsmunstycken för raketmotorer SE512942C2 (sv)

Priority Applications (10)

Application Number Priority Date Filing Date Title
SE9803387A SE512942C2 (sv) 1998-10-02 1998-10-02 Förfarande för tillverkning av utloppsmunstycken för raketmotorer
CN99811689A CN1107164C (zh) 1998-10-02 1999-09-29 火箭发动机出口喷嘴的制造方法
PCT/SE1999/001727 WO2000020749A1 (en) 1998-10-02 1999-09-29 Method for manufacturing outlet nozzles for rocket engines
JP2000574828A JP3890195B2 (ja) 1998-10-02 1999-09-29 ロケットエンジンのための出口ノズルを製造するための方法
RU2001111830/06A RU2209994C2 (ru) 1998-10-02 1999-09-29 Способ изготовления выходных сопел для ракетных двигателей
US09/806,607 US6591499B1 (en) 1998-10-02 1999-09-29 Method for manufacturing outlet nozzles for rocket engines
EP99970150A EP1117918B1 (de) 1998-10-02 1999-09-29 Verfahren zur herstellung von auslassdüsen von raketenmotoren
DE69918452T DE69918452T2 (de) 1998-10-02 1999-09-29 Verfahren zur herstellung von auslassdüsen von raketenmotoren
US10/370,536 US6907662B2 (en) 1998-10-02 2003-02-20 Method for manufacturing outlet nozzles for rocket engines
US10/872,667 US6945032B2 (en) 1998-10-02 2004-06-21 Method for manufacturing outlet nozzles for rocket engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE9803387A SE512942C2 (sv) 1998-10-02 1998-10-02 Förfarande för tillverkning av utloppsmunstycken för raketmotorer

Publications (3)

Publication Number Publication Date
SE9803387D0 SE9803387D0 (sv) 1998-10-02
SE9803387L SE9803387L (sv) 2000-04-03
SE512942C2 true SE512942C2 (sv) 2000-06-12

Family

ID=20412837

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9803387A SE512942C2 (sv) 1998-10-02 1998-10-02 Förfarande för tillverkning av utloppsmunstycken för raketmotorer

Country Status (8)

Country Link
US (3) US6591499B1 (de)
EP (1) EP1117918B1 (de)
JP (1) JP3890195B2 (de)
CN (1) CN1107164C (de)
DE (1) DE69918452T2 (de)
RU (1) RU2209994C2 (de)
SE (1) SE512942C2 (de)
WO (1) WO2000020749A1 (de)

Families Citing this family (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE512942C2 (sv) * 1998-10-02 2000-06-12 Volvo Aero Corp Förfarande för tillverkning av utloppsmunstycken för raketmotorer
ES2305238T3 (es) * 2001-01-11 2008-11-01 Volvo Aero Corporation Procedimiento de fabricacion de boquillas de salida para motores de cohetes.
WO2002055864A1 (en) * 2001-01-11 2002-07-18 Volvo Aero Corporation Rocket engine member and a method for manufacturing a rocket engine member
JP2002303207A (ja) * 2001-04-02 2002-10-18 Advanced Space Technology Kk 液体ロケットエンジンにおける燃焼室の製造方法
SE519781C2 (sv) * 2001-08-29 2003-04-08 Volvo Aero Corp Förfarande för framställning av en stator-eller rotorkomponent
JP4452919B2 (ja) * 2001-12-18 2010-04-21 ボルボ エアロ コーポレイション 動作中に高い熱負荷を受ける構成部品及びそのような構成部品を製造する方法
US7188417B2 (en) * 2002-06-28 2007-03-13 United Technologies Corporation Advanced L-channel welded nozzle design
DE60313782T2 (de) * 2002-08-14 2008-01-24 Volvo Aero Corp. Verfahren zur herstellung eines stator- oder rotorteils
US7121481B2 (en) * 2002-10-10 2006-10-17 Volvo Aero Corporation Fuel injector
US6953509B2 (en) * 2003-06-03 2005-10-11 The Boeing Company Method for preparing pre-coated, metallic components and components prepared thereby
DE10340826A1 (de) * 2003-09-04 2005-03-31 Rolls-Royce Deutschland Ltd & Co Kg Homogene Gemischbildung durch verdrallte Einspritzung des Kraftstoffs
US20050210820A1 (en) * 2004-03-24 2005-09-29 Shinmaywa Industries, Ltd. Frame and method for fabricating the same
US6998570B1 (en) * 2004-11-04 2006-02-14 United Technologies Corporation Beam welding apparatus and methods
US7370469B2 (en) * 2004-12-13 2008-05-13 United Technologies Corporation Rocket chamber heat exchanger
US7596940B2 (en) * 2005-03-22 2009-10-06 Pratt & Whitney Rocketdyne, Inc. Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing
US8002168B2 (en) * 2005-09-06 2011-08-23 Volvo Aero Corporation Method of producing an engine wall structure
EP1926904A4 (de) * 2005-09-06 2013-04-10 Volvo Aero Corp Motorwandstruktur und verfahren zur herstellung einer motorwandstruktur
WO2008010748A1 (en) * 2006-07-19 2008-01-24 Volvo Aero Corporation Method for manufacturing a wall structure
EP2094430A4 (de) * 2006-12-18 2010-07-28 Volvo Aero Corp Verfahren zur verbindung von metallmaterialteilchen und schweissvorrichtung
EP2094964A4 (de) * 2006-12-19 2013-05-01 Volvo Aero Corp Wand eines raketenmotors
EP2094420A4 (de) * 2006-12-19 2012-08-22 Volvo Aero Corp Verfahren zur herstellung einer wandstruktur und werkzeugmaschine
EP2122148B1 (de) * 2007-02-13 2013-08-28 GKN Aerospace Sweden AB Zur beaufschlagung mit einer hohen wärmelast im betrieb konfiguriertes bauteil
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
SE531857C2 (sv) * 2007-12-21 2009-08-25 Volvo Aero Corp En komponent avsedd att utsättas för hög termisk last vid drift
CN100570147C (zh) * 2008-01-17 2009-12-16 清华大学 一种利用强吸热反应的层板发汗冷却结构
DE102010007272B4 (de) * 2010-02-08 2016-09-15 Astrium Gmbh Verfahren zur Herstellung einer regenerativ gekühlten Düsenerweiterung einer Raketenbrennkammer und Düsenerweiterung
US20120227408A1 (en) * 2011-03-10 2012-09-13 Delavan Inc. Systems and methods of pressure drop control in fluid circuits through swirling flow mitigation
US9409251B2 (en) * 2011-10-12 2016-08-09 Asml Netherlands B.V. Radiation beam welding method, body and lithographic apparatus
CN102974926B (zh) * 2012-11-02 2014-12-17 首都航天机械公司 火箭发动机喷管的偏芯tig焊接方法
RU2536653C1 (ru) * 2013-06-19 2014-12-27 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") Способ изготовления сопла жидкостного ракетного двигателя оживальной формы (варианты)
CN105268799B (zh) * 2014-07-21 2018-03-16 北京航天动力研究所 一种净成型整体加强外套
JP5823069B1 (ja) * 2015-01-23 2015-11-25 三菱重工業株式会社 ロケットエンジンの燃焼器の製造方法、ロケットエンジンの燃焼器、および、ロケットエンジン
JP6481978B2 (ja) 2015-03-10 2019-03-13 三菱重工業株式会社 燃焼室の冷却機構、冷却機構を備えるロケットエンジン、及び、冷却機構の製造方法
FR3052502B1 (fr) * 2016-06-13 2018-06-29 Snecma Chambre de combustion de moteur fusee avec ailettes a composition variable
WO2018045327A1 (en) * 2016-09-01 2018-03-08 Additive Rocket Corporation Structural heat exchanger
CN106423597A (zh) * 2016-10-28 2017-02-22 北京航天动力研究所 一种铣槽扩散焊喷嘴
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
EP3466601B1 (de) 2017-10-04 2024-06-12 Saint-Gobain Ecophon AB Verfahren zur herstellung eines profilelements
RU2679032C1 (ru) * 2018-01-30 2019-02-05 Федеральное государственное бюджетное образовательное учреждение высшего образования "Тверской государственный технический университет" Способ изготовления наплавленного биметаллического сопла
US20190329355A1 (en) * 2018-04-27 2019-10-31 United States Of America As Represented By The Administrator Of Nasa Method for Fabricating Seal-Free Multi-Metallic Thrust Chamber Liner
CN109079322A (zh) * 2018-07-11 2018-12-25 陕西蓝箭航天技术有限公司 航天运载器的发动机喷管制备方法
CN112638570B (zh) * 2018-08-30 2023-07-07 Ipg光子公司 背面焊接系统和方法
JP7324096B2 (ja) * 2019-09-13 2023-08-09 三菱重工業株式会社 冷却流路構造、バーナー及び熱交換器
RU194928U1 (ru) * 2019-10-08 2019-12-30 Федеральное государственное бюджетное образовательное учреждение высшего образования "Омский государственный технический университет"(ОмГТУ) Внутренняя оболочка сопла камеры жидкостного ракетного двигателя
CN111531334A (zh) * 2020-05-23 2020-08-14 北京普惠三航科技有限公司 三层点阵结构件及其加工方法
DE102020133967A1 (de) 2020-12-17 2022-06-23 Arianegroup Gmbh Brennkammer, Verfahren zur Herstellung einer Brennkammer und Triebwerk
CN112832930B (zh) * 2021-03-05 2022-02-25 中国科学院力学研究所 一种用于火箭发动机的等水力直径的冷却通道设计方法
CN114439652B (zh) * 2021-12-29 2023-03-10 北京航天动力研究所 一种热防护增强型3d打印喷管延伸段
WO2025085463A1 (en) * 2023-10-20 2025-04-24 Dm3D Technology, Llc Direct printing of cooling channel walls for rocket engines

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3235947A (en) 1961-12-22 1966-02-22 Bolkow Gmbh Method for making a combustion chamber
FR2012723A1 (de) * 1968-07-11 1970-03-20 Messerschmitt Boelkow Blohm
US3832290A (en) * 1972-09-14 1974-08-27 Nasa Method of electroforming a rocket chamber
RU2027053C1 (ru) * 1989-05-23 1995-01-20 Конников Герман Германович Комбинированное сопло реактивного двигателя
RU1725598C (ru) * 1989-11-09 1994-12-15 Байсиев Хаджи-Мурат Хасанович Ракетный двигатель твердого топлива байсиева
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.
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
US5501011A (en) * 1992-05-18 1996-03-26 Societe Europeenne De Propulsion Method of manufacture of an enclosure containing hot gases cooled by transportation, in particular the thrust chamber of a rocket engine
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
US5588268A (en) 1993-06-23 1996-12-31 Jos. L. Meyer Werft Gmbh & Co. Plate element for a building panel assembly
US5874015A (en) * 1996-06-06 1999-02-23 Alliedsignal Inc. Method for making a rhenium rocket nozzle
US5822853A (en) * 1996-06-24 1998-10-20 General Electric Company Method for making cylindrical structures with cooling channels
SE512942C2 (sv) * 1998-10-02 2000-06-12 Volvo Aero Corp Förfarande för tillverkning av utloppsmunstycken för raketmotorer
JP2000158257A (ja) * 1998-11-19 2000-06-13 Showa Aircraft Ind Co Ltd チタンハニカムの製造方法
US6134782A (en) * 1998-11-30 2000-10-24 United Technologies Corporation Method of forming a rocket thrust chamber
RU2158666C2 (ru) * 1999-02-04 2000-11-10 Открытое акционерное общество НПО Энергомаш им. акад. В.П. Глушко Способ изготовления сварно-паяной конструкции
US6205661B1 (en) * 1999-04-15 2001-03-27 Peter John Ring Method of making a rocket thrust chamber
SE516046C2 (sv) * 2000-03-17 2001-11-12 Volvo Aero Corp Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp
ES2305238T3 (es) * 2001-01-11 2008-11-01 Volvo Aero Corporation Procedimiento de fabricacion de boquillas de salida para motores de cohetes.
EP1352168B1 (de) * 2001-01-11 2006-06-21 Volvo Aero Corporation Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds
ATE323224T1 (de) * 2001-01-11 2006-04-15 Abgabedüse und verfahren zur herstellung einer abgabedüse
WO2002055864A1 (en) * 2001-01-11 2002-07-18 Volvo Aero Corporation Rocket engine member and a method for manufacturing a rocket engine member
US6783824B2 (en) * 2001-01-25 2004-08-31 Hyper-Therm High-Temperature Composites, Inc. Actively-cooled fiber-reinforced ceramic matrix composite rocket propulsion thrust chamber and method of producing the same
ATE360752T1 (de) * 2002-05-28 2007-05-15 Volvo Aero Corp Wandkonstruktion

Also Published As

Publication number Publication date
US6945032B2 (en) 2005-09-20
US6591499B1 (en) 2003-07-15
SE9803387L (sv) 2000-04-03
WO2000020749A1 (en) 2000-04-13
JP2002526715A (ja) 2002-08-20
EP1117918A1 (de) 2001-07-25
SE9803387D0 (sv) 1998-10-02
US6907662B2 (en) 2005-06-21
US20030183606A1 (en) 2003-10-02
JP3890195B2 (ja) 2007-03-07
DE69918452T2 (de) 2005-07-28
US20040237533A1 (en) 2004-12-02
DE69918452D1 (de) 2004-08-05
CN1107164C (zh) 2003-04-30
CN1321219A (zh) 2001-11-07
RU2209994C2 (ru) 2003-08-10
EP1117918B1 (de) 2004-06-30

Similar Documents

Publication Publication Date Title
SE512942C2 (sv) Förfarande för tillverkning av utloppsmunstycken för raketmotorer
CN109798800A (zh) 波形壁热交换器
EP0725214B1 (de) Filmgekühlte Brennkammerwand für Gasturbine und Verfahren zu ihrer Herstellung
JP4586024B2 (ja) 熱交換器及びその使用
EP1352170B1 (de) Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds
US6789316B2 (en) Method for manufacturing outlet nozzles for rocket engines
JP2005513322A (ja) 動作中に高い熱負荷を受ける構成部品及びそのような構成部品を製造する方法
EP1352169B1 (de) Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds
US20090314479A1 (en) Heat exchanger and a method of manufacturing a heat exchanger
JP2007303813A (ja) 自己ブレーキラジエータ側板
US4134195A (en) Method of manifold construction for formed tube-sheet heat exchanger and structure formed thereby
US7895823B2 (en) Heat exchanger for a rocket engine
KR20010101414A (ko) 코일열교환기 및 이를 제조하는 방법
EP1352166B1 (de) Abgabedüse und verfahren zur herstellung einer abgabedüse
US20070000652A1 (en) Heat exchanger with dimpled tube surfaces
JP4729973B2 (ja) 熱交換器およびこれを備えた温水装置
JP2004218954A (ja) 熱交換器およびその製造方法
JP2007225137A (ja) 排気ガス冷却装置用多管式熱交換器および伝熱管
US20240302113A1 (en) Heat recovery member and heat exchanger
JP4923824B2 (ja) 熱交換器および温水装置
JPH1038490A (ja) 高温熱交換器用フィン付き伝熱管
SE520261C2 (sv) Förfarande för tillverkning av utloppsmunstycke
JPH0611281A (ja) 熱交換器及びその伝熱管
SE520268C2 (sv) Del till en raketmotor för flytande bränsle samt förfarande för framställning av en del till en raketmotor

Legal Events

Date Code Title Description
NUG Patent has lapsed