DE69812253D1 - Herstellung eines Raketenmotors mit einem Verbindungsstück zwischen Verbrennungskammer und Injektor - Google Patents

Herstellung eines Raketenmotors mit einem Verbindungsstück zwischen Verbrennungskammer und Injektor

Info

Publication number
DE69812253D1
DE69812253D1 DE69812253T DE69812253T DE69812253D1 DE 69812253 D1 DE69812253 D1 DE 69812253D1 DE 69812253 T DE69812253 T DE 69812253T DE 69812253 T DE69812253 T DE 69812253T DE 69812253 D1 DE69812253 D1 DE 69812253D1
Authority
DE
Germany
Prior art keywords
injector
connector
manufacture
combustion chamber
rocket engine
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
DE69812253T
Other languages
English (en)
Other versions
DE69812253T2 (de
Inventor
Kurt B Kreiner
Carl R Stechmann
Joel Neiderman
David Bronson
Peter Woll
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics 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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Application granted granted Critical
Publication of DE69812253D1 publication Critical patent/DE69812253D1/de
Publication of DE69812253T2 publication Critical patent/DE69812253T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/008Rocket engine parts, e.g. nozzles, combustion chambers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K31/00Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
    • B23K31/02Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups relating to soldering or welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/34Casings; Combustion chambers; Liners thereof
    • F02K9/343Joints, connections, seals therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/68Decomposition chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K33/00Specially-profiled edge portions of workpieces for making soldering or welding connections; Filling the seams formed thereby
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49346Rocket or jet device making
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)
DE69812253T 1997-08-29 1998-08-27 Herstellung eines Raketenmotors mit einem Verbindungsstück zwischen Verbrennungskammer und Injektor Expired - Lifetime DE69812253T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US5736897P 1997-08-29 1997-08-29
US57368P 1997-08-29

Publications (2)

Publication Number Publication Date
DE69812253D1 true DE69812253D1 (de) 2003-04-24
DE69812253T2 DE69812253T2 (de) 2004-02-05

Family

ID=22010145

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69812253T Expired - Lifetime DE69812253T2 (de) 1997-08-29 1998-08-27 Herstellung eines Raketenmotors mit einem Verbindungsstück zwischen Verbrennungskammer und Injektor

Country Status (4)

Country Link
US (1) US6249967B1 (de)
EP (1) EP0899448B1 (de)
JP (1) JP3023348B2 (de)
DE (1) DE69812253T2 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0899449B1 (de) * 1997-08-29 2003-03-12 Hughes Electronics Corporation Raketenmotor mit einem Verbindungsstück zwischen Verbrennungskammer und Injektor
CA2250599A1 (en) * 1998-10-16 2000-04-16 Jobst Ulrich Gellert Apparatus and method of making an injection molding nozzle with tip insert
RU2158666C2 (ru) * 1999-02-04 2000-11-10 Открытое акционерное общество НПО Энергомаш им. акад. В.П. Глушко Способ изготовления сварно-паяной конструкции
RU2158667C1 (ru) * 1999-03-01 2000-11-10 Открытое акционерное общество НПО Энергомаш им. акад. В.П. Глушко Способ изготовления сварно-паяной конструкции газогенератора
DE19927734C2 (de) * 1999-06-17 2002-04-11 Astrium Gmbh Schubkammer eines Antriebstriebwerks für Satelliten und Transportgeräte für Raumfahrtanwendungen
US7199338B2 (en) * 2004-11-19 2007-04-03 General Electric Company Method and system for applying an isolation layer to a brazed end of a generator armature winding bar
US9404441B2 (en) * 2008-08-18 2016-08-02 Aerojet Rocketdyne Of De, Inc. Low velocity injector manifold for hypergolic rocket engine
CN102049623B (zh) * 2010-10-21 2012-09-12 航天材料及工艺研究所 一种不同厚度镍铜组件与无氧铜基体的组合焊接方法
CN102922229A (zh) * 2012-10-24 2013-02-13 哈尔滨东安发动机(集团)有限公司 机匣的组合加工方法
JP6273175B2 (ja) * 2014-07-25 2018-01-31 三菱重工業株式会社 部材接合方法及び部材接合システム
CN106862746B (zh) * 2017-03-08 2019-05-10 西北工业大学 一种高温钛合金薄壁铸件电子束焊接方法
RU2664746C1 (ru) * 2017-10-11 2018-08-22 Федеральное государственное унитарное предприятие "Научно-исследовательский институт Научно-производственное объединение "ЛУЧ" (ФГУП "НИИ НПО "ЛУЧ") Способ электронно-лучевой сварки тонкостенных труб из молибденовых сплавов
CN111922577B (zh) * 2020-05-29 2022-07-29 西安航天精密机电研究所 基于六轴机器人的封接体极针与桥带焊接机械手
CN112628021B (zh) * 2020-12-01 2021-11-16 蓝箭航天空间科技股份有限公司 一种推力室端部的封焊方法及火箭发动机推力室
CN113352062B (zh) * 2021-08-11 2021-11-19 西安远航真空钎焊技术有限公司 燃烧室筒体的制备方法
CN113814511B (zh) * 2021-09-17 2023-02-17 西安航天发动机有限公司 火箭发动机钎焊身部气保护真空钎焊工艺装置及使用方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4785748A (en) 1987-08-24 1988-11-22 The Marquardt Company Method sudden expansion (SUE) incinerator for destroying hazardous materials & wastes
US4915938A (en) 1987-11-13 1990-04-10 Zawadzki Mary E Hair treating composition
US4936091A (en) * 1988-03-24 1990-06-26 Aerojet General Corporation Two stage rocket combustor
US4882904A (en) * 1988-03-24 1989-11-28 Aerojet-General Corporation Two stage rocket combustor
US6079101A (en) * 1998-05-11 2000-06-27 Hughes Electronics Corporation Rocket engine with one-piece combustion chamber step structure, and its fabrication
RU2158666C2 (ru) * 1999-02-04 2000-11-10 Открытое акционерное общество НПО Энергомаш им. акад. В.П. Глушко Способ изготовления сварно-паяной конструкции

Also Published As

Publication number Publication date
DE69812253T2 (de) 2004-02-05
EP0899448B1 (de) 2003-03-19
US6249967B1 (en) 2001-06-26
JP3023348B2 (ja) 2000-03-21
EP0899448A3 (de) 2000-06-14
EP0899448A2 (de) 1999-03-03
JPH11132108A (ja) 1999-05-18

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: WITTE, WELLER & PARTNER, 70178 STUTTGART