ATE323224T1 - Abgabedüse und verfahren zur herstellung einer abgabedüse - Google Patents

Abgabedüse und verfahren zur herstellung einer abgabedüse

Info

Publication number
ATE323224T1
ATE323224T1 AT02729602T AT02729602T ATE323224T1 AT E323224 T1 ATE323224 T1 AT E323224T1 AT 02729602 T AT02729602 T AT 02729602T AT 02729602 T AT02729602 T AT 02729602T AT E323224 T1 ATE323224 T1 AT E323224T1
Authority
AT
Austria
Prior art keywords
nozzle
section
dispensing nozzle
revolution
axis
Prior art date
Application number
AT02729602T
Other languages
English (en)
Inventor
Jan Haeggander
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
Priority claimed from SE0100076A external-priority patent/SE518258C2/sv
Application filed filed Critical
Application granted granted Critical
Publication of ATE323224T1 publication Critical patent/ATE323224T1/de

Links

Classifications

    • 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
    • F02K9/42—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
    • 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
    • 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
    • F05D2250/30—Arrangement of components
    • F05D2250/33—Arrangement of components symmetrical
    • 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
    • F05D2250/30—Arrangement of components
    • F05D2250/35—Arrangement of components rotated
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Orthopedics, Nursing, And Contraception (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Laser Beam Processing (AREA)
  • Testing Of Engines (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
AT02729602T 2001-01-11 2002-01-09 Abgabedüse und verfahren zur herstellung einer abgabedüse ATE323224T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US26104501P 2001-01-11 2001-01-11
SE0100076A SE518258C2 (sv) 2001-01-11 2001-01-11 Utloppsmunstycke och förfarande för framställning av detta

Publications (1)

Publication Number Publication Date
ATE323224T1 true ATE323224T1 (de) 2006-04-15

Family

ID=26655368

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02729602T ATE323224T1 (de) 2001-01-11 2002-01-09 Abgabedüse und verfahren zur herstellung einer abgabedüse

Country Status (8)

Country Link
US (1) US20040103640A1 (de)
EP (1) EP1352166B1 (de)
JP (1) JP4019215B2 (de)
AT (1) ATE323224T1 (de)
DE (1) DE60210578T2 (de)
ES (1) ES2261667T3 (de)
RU (1) RU2278294C2 (de)
WO (1) WO2002055860A1 (de)

Families Citing this family (12)

* 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
RU2325545C1 (ru) * 2006-11-07 2008-05-27 Федеральное государственное унитарное предприятие "Воронежский механический завод" Внутренняя оболочка сопла камеры жидкостного ракетного двигателя
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)
CN104439945B (zh) * 2014-11-11 2016-08-24 沈阳黎明航空发动机(集团)有限责任公司 一种航空发动机主喷口类零件的数控加工方法
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
DE102016212399B4 (de) * 2016-07-07 2022-04-28 Arianegroup Gmbh Raketentriebwerk
CN107322246B (zh) * 2017-08-23 2019-05-14 湖北三江航天江北机械工程有限公司 固体火箭发动机大喷管粘接压配工艺
CN109676326B (zh) * 2019-01-14 2020-02-18 蓝箭航天空间科技股份有限公司 航天发动机喷管零件的成型方法
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
CN110761916A (zh) * 2019-10-29 2020-02-07 北京星际荣耀空间科技有限公司 一种再生冷却结构
RU2757798C1 (ru) * 2020-12-26 2021-10-21 Владимир Александрович Вьюрков Сопло двигателя с истечением масс
WO2023163616A1 (ru) * 2022-02-28 2023-08-31 Акционерное общество "ЗЕНТОРН" Сопло с истечением масс и прямовыходящим потоком

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2523011A (en) * 1947-11-01 1950-09-19 Daniel And Florence Guggenheim Cooling and feeding means for rotating combustion chambers
US3154914A (en) * 1959-12-12 1964-11-03 Bolkow Entwicklungen Kg Rocket engine construction
US3605412A (en) * 1968-07-09 1971-09-20 Bolkow Gmbh Fluid cooled thrust nozzle for a rocket
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
DE3436419C2 (de) * 1983-10-07 1990-11-15 Yoshimichi Chigasaki Kanagawa Masuda Verfahren zur Herstellung von Raketenbrennkammern
DE3618038A1 (de) * 1986-05-28 1987-12-03 Messerschmitt Boelkow Blohm Stuetzstruktur fuer fluessigkeitsgekuehlte expansionsduesen
JPH0659502B2 (ja) * 1987-03-26 1994-08-10 宇宙科学研究所長 ロケット用高圧燃焼器の燃焼室及びその製造方法
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
US6164060A (en) * 1997-08-18 2000-12-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Combustion chamber/nozzle assembly and fabrication process therefor
RU2139439C1 (ru) * 1998-05-20 1999-10-10 Федеральное государственное унитарное предприятие "Конструкторское бюро химавтоматики" Сопло камеры жидкостного ракетного двигателя
JP4271866B2 (ja) * 1998-11-27 2009-06-03 ボルボ エアロ コーポレイション 冷却されるノズル壁を有するロケットノズルのノズル構造

Also Published As

Publication number Publication date
JP4019215B2 (ja) 2007-12-12
RU2278294C2 (ru) 2006-06-20
DE60210578D1 (de) 2006-05-24
ES2261667T3 (es) 2006-11-16
EP1352166B1 (de) 2006-04-12
WO2002055860A1 (en) 2002-07-18
US20040103640A1 (en) 2004-06-03
RU2003123787A (ru) 2005-02-27
JP2004518057A (ja) 2004-06-17
EP1352166A1 (de) 2003-10-15
DE60210578T2 (de) 2006-12-14

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Legal Events

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