SE9803387D0 - Förfarande för tillverkning av utloppsmunstycken för raketmotorer - Google Patents
Förfarande för tillverkning av utloppsmunstycken för raketmotorerInfo
- Publication number
- SE9803387D0 SE9803387D0 SE9803387A SE9803387A SE9803387D0 SE 9803387 D0 SE9803387 D0 SE 9803387D0 SE 9803387 A SE9803387 A SE 9803387A SE 9803387 A SE9803387 A SE 9803387A SE 9803387 D0 SE9803387 D0 SE 9803387D0
- Authority
- SE
- Sweden
- Prior art keywords
- spacers
- outlet nozzles
- procedure
- rocket engine
- engine outlet
- Prior art date
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)
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 |
EP99970150A EP1117918B1 (en) | 1998-10-02 | 1999-09-29 | Method for manufacturing outlet nozzles for rocket engines |
RU2001111830/06A RU2209994C2 (ru) | 1998-10-02 | 1999-09-29 | Способ изготовления выходных сопел для ракетных двигателей |
PCT/SE1999/001727 WO2000020749A1 (en) | 1998-10-02 | 1999-09-29 | Method for manufacturing outlet nozzles for rocket engines |
DE69918452T DE69918452T2 (de) | 1998-10-02 | 1999-09-29 | Verfahren zur herstellung von auslassdüsen von raketenmotoren |
CN99811689A CN1107164C (zh) | 1998-10-02 | 1999-09-29 | 火箭发动机出口喷嘴的制造方法 |
US09/806,607 US6591499B1 (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 |
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 true SE9803387D0 (sv) | 1998-10-02 |
SE9803387L SE9803387L (sv) | 2000-04-03 |
SE512942C2 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 (sv) |
EP (1) | EP1117918B1 (sv) |
JP (1) | JP3890195B2 (sv) |
CN (1) | CN1107164C (sv) |
DE (1) | DE69918452T2 (sv) |
RU (1) | RU2209994C2 (sv) |
SE (1) | SE512942C2 (sv) |
WO (1) | WO2000020749A1 (sv) |
Families Citing this family (48)
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 |
DE60212069T2 (de) * | 2001-01-11 | 2006-12-21 | Volvo Aero Corp. | Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds |
ES2305238T3 (es) | 2001-01-11 | 2008-11-01 | Volvo Aero Corporation | Procedimiento de fabricacion de boquillas de salida para motores de cohetes. |
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 |
WO2003052255A1 (en) * | 2001-12-18 | 2003-06-26 | Volvo Aero Corporation | A component for being subjected to high thermal load during operation and a method for manufacturing such a component |
US7188417B2 (en) * | 2002-06-28 | 2007-03-13 | United Technologies Corporation | Advanced L-channel welded nozzle design |
ATE362037T1 (de) * | 2002-08-14 | 2007-06-15 | 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 |
EP1926904A4 (en) * | 2005-09-06 | 2013-04-10 | Volvo Aero Corp | MOTOR WALL STRUCTURE AND METHODS FOR GENERATING THE WALL STRUCTURE OF THE ENGINE |
EP1929147B1 (en) * | 2005-09-06 | 2010-08-25 | Volvo Aero Corporation | A method of producing an engine wall structure |
WO2008010748A1 (en) * | 2006-07-19 | 2008-01-24 | Volvo Aero Corporation | Method for manufacturing a wall structure |
US20100116792A1 (en) * | 2006-12-18 | 2010-05-13 | Volvo Aero Corporation | Method of joining pieces of metal material and a welding device |
US20100229565A1 (en) * | 2006-12-19 | 2010-09-16 | Arne Boman | Wall of a rocket engine |
US8448335B2 (en) | 2006-12-19 | 2013-05-28 | Volvo Aero Corporation | Method of manufacturing a wall structure and a machining tool |
WO2008100186A1 (en) * | 2007-02-13 | 2008-08-21 | Volvo Aero Corporation | A component configured for being subjected to high thermal load during operation |
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 |
NL2009446A (en) * | 2011-10-12 | 2013-04-15 | Asml Netherlands Bv | 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 |
EP3507558A4 (en) * | 2016-09-01 | 2020-04-22 | 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 (en) | 2017-10-04 | 2024-06-12 | Saint-Gobain Ecophon AB | Method for manufacturing of a profile member |
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 |
CA3110516A1 (en) * | 2018-08-30 | 2020-03-05 | Ipg Photonics Corporation | Backside surface welding system and method |
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 |
Family Cites Families (22)
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 (sv) * | 1968-07-11 | 1970-03-20 | Messerschmitt Boelkow Blohm | |
US3832290A (en) * | 1972-09-14 | 1974-08-27 | Nasa | Method of electroforming a rocket chamber |
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 |
JPH08501361A (ja) | 1993-06-23 | 1996-02-13 | ヨーゼフ エル マイヤー ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー | 板部材 |
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 |
ATE331133T1 (de) * | 2001-01-11 | 2006-07-15 | Volvo Aero Corp | Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglieds |
ES2305238T3 (es) * | 2001-01-11 | 2008-11-01 | Volvo Aero Corporation | Procedimiento de fabricacion de boquillas de salida para motores de cohetes. |
DE60210578T2 (de) * | 2001-01-11 | 2006-12-14 | Volvo Aero Corp. | Abgabedüse und verfahren zur herstellung einer abgabedüse |
DE60212069T2 (de) * | 2001-01-11 | 2006-12-21 | Volvo Aero Corp. | Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds |
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 |
JP4405382B2 (ja) * | 2002-05-28 | 2010-01-27 | ボルボ エアロ コーポレイション | 壁構造 |
-
1998
- 1998-10-02 SE SE9803387A patent/SE512942C2/sv not_active IP Right Cessation
-
1999
- 1999-09-29 RU RU2001111830/06A patent/RU2209994C2/ru not_active IP Right Cessation
- 1999-09-29 DE DE69918452T patent/DE69918452T2/de not_active Expired - Lifetime
- 1999-09-29 US US09/806,607 patent/US6591499B1/en not_active Expired - Lifetime
- 1999-09-29 CN CN99811689A patent/CN1107164C/zh not_active Expired - Fee Related
- 1999-09-29 WO PCT/SE1999/001727 patent/WO2000020749A1/en active IP Right Grant
- 1999-09-29 JP JP2000574828A patent/JP3890195B2/ja not_active Expired - Fee Related
- 1999-09-29 EP EP99970150A patent/EP1117918B1/en not_active Expired - Lifetime
-
2003
- 2003-02-20 US US10/370,536 patent/US6907662B2/en not_active Expired - Lifetime
-
2004
- 2004-06-21 US US10/872,667 patent/US6945032B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP3890195B2 (ja) | 2007-03-07 |
US20040237533A1 (en) | 2004-12-02 |
RU2209994C2 (ru) | 2003-08-10 |
CN1107164C (zh) | 2003-04-30 |
US6907662B2 (en) | 2005-06-21 |
EP1117918A1 (en) | 2001-07-25 |
SE9803387L (sv) | 2000-04-03 |
US6591499B1 (en) | 2003-07-15 |
US20030183606A1 (en) | 2003-10-02 |
JP2002526715A (ja) | 2002-08-20 |
US6945032B2 (en) | 2005-09-20 |
DE69918452D1 (de) | 2004-08-05 |
DE69918452T2 (de) | 2005-07-28 |
WO2000020749A1 (en) | 2000-04-13 |
SE512942C2 (sv) | 2000-06-12 |
CN1321219A (zh) | 2001-11-07 |
EP1117918B1 (en) | 2004-06-30 |
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Date | Code | Title | Description |
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NUG | Patent has lapsed |