DE60226574D1 - Verfahren zur herstellung von austrittsdüsen für raketentriebwerke - Google Patents

Verfahren zur herstellung von austrittsdüsen für raketentriebwerke

Info

Publication number
DE60226574D1
DE60226574D1 DE60226574T DE60226574T DE60226574D1 DE 60226574 D1 DE60226574 D1 DE 60226574D1 DE 60226574 T DE60226574 T DE 60226574T DE 60226574 T DE60226574 T DE 60226574T DE 60226574 D1 DE60226574 D1 DE 60226574D1
Authority
DE
Germany
Prior art keywords
nozzle
flanges
revolution
web
axis
Prior art date
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.)
Expired - Lifetime
Application number
DE60226574T
Other languages
English (en)
Inventor
Jan Haeggander
Jan Lundgren
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GKN Aerospace Sweden AB
Original Assignee
Volvo Aero AB
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 SE0100077A external-priority patent/SE520261C2/sv
Application filed by Volvo Aero AB filed Critical Volvo Aero AB
Application granted granted Critical
Publication of DE60226574D1 publication Critical patent/DE60226574D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F02K9/42—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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • 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
    • F05D2250/19—Two-dimensional machined; miscellaneous
    • 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
    • F05D2250/29—Three-dimensional machined; miscellaneous
    • F05D2250/292—Three-dimensional machined; miscellaneous tapered
    • 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
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • 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
    • 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
    • Y10T29/49826—Assembling or joining
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
DE60226574T 2001-01-11 2002-01-09 Verfahren zur herstellung von austrittsdüsen für raketentriebwerke Expired - Lifetime DE60226574D1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US26104901P 2001-01-11 2001-01-11
SE0100077A SE520261C2 (sv) 2001-01-11 2001-01-11 Förfarande för tillverkning av utloppsmunstycke
PCT/SE2002/000024 WO2002055861A1 (en) 2001-01-11 2002-01-09 Method for manufacturing outlet nozzles for rocket engines

Publications (1)

Publication Number Publication Date
DE60226574D1 true DE60226574D1 (de) 2008-06-26

Family

ID=26655369

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60226574T Expired - Lifetime DE60226574D1 (de) 2001-01-11 2002-01-09 Verfahren zur herstellung von austrittsdüsen für raketentriebwerke

Country Status (8)

Country Link
US (1) US6789316B2 (de)
EP (1) EP1352167B1 (de)
JP (1) JP4019216B2 (de)
AT (1) ATE395508T1 (de)
DE (1) DE60226574D1 (de)
ES (1) ES2305238T3 (de)
RU (1) RU2274762C2 (de)
WO (1) WO2002055861A1 (de)

Families Citing this family (18)

* 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
SE527732C2 (sv) * 2004-10-07 2006-05-23 Volvo Aero Corp Ett hölje för omslutande av en gasturbinkomponent
WO2008076007A1 (en) * 2006-12-19 2008-06-26 Volvo Aero Corporation A method of manufacturing a wall structure and a machining tool
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
DE102010007272B4 (de) 2010-02-08 2016-09-15 Astrium Gmbh Verfahren zur Herstellung einer regenerativ gekühlten Düsenerweiterung einer Raketenbrennkammer und Düsenerweiterung
US8966759B1 (en) * 2010-06-25 2015-03-03 Maxq Technology, Llc Method of making a fluid cooled assembly
WO2014126899A1 (en) * 2013-02-17 2014-08-21 United Technologies Corporation Exhaust liner flange cooling
DE102013224982A1 (de) * 2013-12-05 2015-06-11 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbine mit einem Kern-Triebwerksgehäuse mit Kühlluftröhren
CN105772812B (zh) * 2016-04-21 2017-10-27 上海航天设备制造总厂 整体成形箱底五轴镜像铣数控加工方法
CN106050474B (zh) * 2016-05-23 2017-12-15 上海空间推进研究所 一种火箭发动机头部和再生冷却身部的新型连接结构
DE102016212314B4 (de) * 2016-07-06 2022-05-12 Arianegroup Gmbh Verfahren zur Herstellung einer Brennkammer
US10414521B1 (en) 2018-04-17 2019-09-17 Hardy Engineering & Manufacturing, Inc. Nuclear rocket engine with pebble fuel source
US10414520B1 (en) 2018-04-17 2019-09-17 Hardy Engineering & Manufacturing, Inc. Fuel retention reactor for nuclear rocket engine
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
CN113787305B (zh) * 2021-09-01 2022-07-22 西安远航真空钎焊技术有限公司 一种空气加热器喷注器的加工方法
CN114131223A (zh) * 2021-10-29 2022-03-04 首都航天机械有限公司 一种激光焊接管束式喷管的接头状态调整装置
CN114427507B (zh) * 2022-04-06 2022-07-15 西安航天动力研究所 一种冷却路射流均匀性检测导流结构及检测装置

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB843923A (en) * 1957-01-17 1960-08-10 Havilland Engine Co Ltd Apparatus in which heat exchange takes place between fluids
US3267559A (en) * 1961-12-01 1966-08-23 Martin Marietta Corp Multi-contoured structures and process
US3521345A (en) * 1965-02-11 1970-07-21 Mb Assoc Method of making a rocket nozzle
US3521344A (en) * 1965-02-11 1970-07-21 Mb Assoc Method of making a rocket nozzle
US3418707A (en) * 1965-04-19 1968-12-31 Rohr Corp Integrated and match machined rocket nozzle and process of making same
US3537646A (en) * 1965-04-19 1970-11-03 Rohr Corp Rocket nozzle structure
US3481543A (en) * 1967-12-18 1969-12-02 Thiokol Chemical Corp Rocket thrust nozzle
DE1751180A1 (de) * 1968-04-18 1971-04-29 Messerschmitt Boelkow Blohm Ausbildung und Anordnung eines Zulaufringes oder Ablaufsammelringes fuer Schubduesen oder Brennkammern von Raketentriebwerken,insbesondere Fluessigkeitsraketentriebwerken
US3630449A (en) * 1970-05-11 1971-12-28 Us Air Force Nozzle for rocket engine
SE512942C2 (sv) * 1998-10-02 2000-06-12 Volvo Aero Corp Förfarande för tillverkning av utloppsmunstycken för raketmotorer
US7017333B2 (en) * 2002-05-28 2006-03-28 Volvo Aero Corporation Wall structure

Also Published As

Publication number Publication date
US6789316B2 (en) 2004-09-14
JP4019216B2 (ja) 2007-12-12
RU2274762C2 (ru) 2006-04-20
ATE395508T1 (de) 2008-05-15
EP1352167B1 (de) 2008-05-14
WO2002055861A1 (en) 2002-07-18
EP1352167A1 (de) 2003-10-15
US20040123460A1 (en) 2004-07-01
ES2305238T3 (es) 2008-11-01
RU2003123783A (ru) 2005-02-27
JP2004518058A (ja) 2004-06-17

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