JPS58214652A - 複合冷却ロケツト燃焼器 - Google Patents

複合冷却ロケツト燃焼器

Info

Publication number
JPS58214652A
JPS58214652A JP57098356A JP9835682A JPS58214652A JP S58214652 A JPS58214652 A JP S58214652A JP 57098356 A JP57098356 A JP 57098356A JP 9835682 A JP9835682 A JP 9835682A JP S58214652 A JPS58214652 A JP S58214652A
Authority
JP
Japan
Prior art keywords
cooling
combustion chamber
perspiration
coolant
throat
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.)
Granted
Application number
JP57098356A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6132495B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html
Inventor
Masayuki Shinno
正之 新野
Nobuyuki Yatsuyanagi
八柳　信之
Akinaga Kumakawa
彰長 熊川
Akio Suzuki
昭夫 鈴木
Hiromi Gomi
五味　広美
Hiroshi Sakamoto
博 坂本
Masaki Sasaki
正樹 佐々木
Yoshimichi Masuda
増田　良道
Ryuzo Watanabe
渡辺　龍三
Jiyunjirou Takegawa
武川　淳二郎
Etsuo Otsuki
悦夫 大槻
Teru Sagane
砂金　照
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.)
National Aerospace Laboratory of Japan
Original Assignee
National Aerospace Laboratory of Japan
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 National Aerospace Laboratory of Japan filed Critical National Aerospace Laboratory of Japan
Priority to JP57098356A priority Critical patent/JPS58214652A/ja
Priority to DE19833320556 priority patent/DE3320556A1/de
Publication of JPS58214652A publication Critical patent/JPS58214652A/ja
Publication of JPS6132495B2 publication Critical patent/JPS6132495B2/ja
Priority to US07/018,790 priority patent/US4703620A/en
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • 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
    • 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
    • F05D2260/203—Heat transfer, e.g. cooling by transpiration 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00—Power plants
    • Y10S60/909—Reaction motor or component composed of specific material

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Powder Metallurgy (AREA)
JP57098356A 1982-06-08 1982-06-08 複合冷却ロケツト燃焼器 Granted JPS58214652A (ja)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP57098356A JPS58214652A (ja) 1982-06-08 1982-06-08 複合冷却ロケツト燃焼器
DE19833320556 DE3320556A1 (de) 1982-06-08 1983-06-07 Kuehlwand der verbundkuehlart fuer eine raketenbrennkammer und verfahren zu ihrer herstellung
US07/018,790 US4703620A (en) 1982-06-08 1987-02-24 Rocket combustion chamber cooling wall of composite cooling type and method of manufacturing the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57098356A JPS58214652A (ja) 1982-06-08 1982-06-08 複合冷却ロケツト燃焼器

Publications (2)

Publication Number Publication Date
JPS58214652A true JPS58214652A (ja) 1983-12-13
JPS6132495B2 JPS6132495B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1986-07-28

Family

ID=14217605

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57098356A Granted JPS58214652A (ja) 1982-06-08 1982-06-08 複合冷却ロケツト燃焼器

Country Status (3)

Country Link
US (1) US4703620A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS58214652A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE3320556A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100717376B1 (ko) 2004-12-29 2007-05-10 한국항공우주연구원 고압액체로켓엔진용 재생냉각 연소실

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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
US4928755A (en) * 1988-05-31 1990-05-29 Doty Scientific, Inc. Microtube strip surface exchanger
DE19730674A1 (de) * 1997-07-17 1999-01-21 Deutsch Zentr Luft & Raumfahrt Brennkammer und Verfahren zur Herstellung einer Brennkammer
RU2158840C2 (ru) * 1999-01-21 2000-11-10 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Корпус камеры жидкостного ракетного двигателя
WO2001002131A1 (en) 1999-07-07 2001-01-11 Russell Air-O-Nautical Method of producing channeled wall apparatus
RU2179499C2 (ru) * 1999-08-20 2002-02-20 Федеральное государственное унитарное предприятие Конструкторское бюро химавтоматики Способ получения пористых изделий заданной проницаемости и конфигурации
RU2171388C2 (ru) * 1999-08-20 2001-07-27 Федеральное государственное унитарное предприятие Конструкторское бюро химавтоматики Камера жидкостного ракетного двигателя
US6606851B1 (en) 2000-09-08 2003-08-19 Joseph Roger Herdy, Jr. Transpiration cooling of rocket engines
DE10054333B4 (de) * 2000-11-02 2006-11-30 Eads Space Transportation Gmbh Brennkammer mit erhöhtem Wärmeeintrag in eine Kühleinrichtung
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
KR100433244B1 (ko) * 2001-03-28 2004-05-24 대한소결금속 주식회사 압축기용 플랜지의 제조 방법
FR2836699B1 (fr) * 2002-03-04 2005-02-11 Eads Launch Vehicles Moteur de fusee
RU2287715C2 (ru) * 2002-09-13 2006-11-20 Виталий Алексеевич Алтунин Способ повышения надежности жрд одно- и многоразового использования
US6802179B2 (en) 2002-12-02 2004-10-12 Aerojet-General Corporation Nozzle with spiral internal cooling channels
US7332123B2 (en) * 2002-12-27 2008-02-19 General Electric Company Method for manufacturing composite articles and the articles obtained therefrom
US6799417B2 (en) * 2003-02-05 2004-10-05 Aerojet-General Corporation Diversion of combustion gas within a rocket engine to preheat fuel
US7213392B2 (en) * 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
US7464537B2 (en) * 2005-04-04 2008-12-16 United Technologies Corporation Heat transfer enhancement features for a tubular wall combustion chamber
DE102005036137A1 (de) * 2005-07-26 2007-02-01 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammer und Verfahren zur Herstellung einer Brennkammer
US8230673B2 (en) * 2006-12-04 2012-07-31 Firestar Engineering, Llc Rocket engine injectorhead with flashback barrier
JP5154568B2 (ja) * 2006-12-04 2013-02-27 ファイアースター エンジニアリング，エルエルシー フラッシュバックバリアを備えた火花一体型推進薬噴射器ヘッド
US8572946B2 (en) 2006-12-04 2013-11-05 Firestar Engineering, Llc Microfluidic flame barrier
JP5711536B2 (ja) * 2007-11-09 2015-05-07 ファイアースター エンジニアリング，エルエルシー 一酸化二窒素と燃料とが混合されて成るモノプロペラント
CN102308077A (zh) * 2008-12-08 2012-01-04 火星工程有限公司 再生冷却式多孔介质护套
RU2391543C1 (ru) * 2008-12-17 2010-06-10 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ подачи газа на турбину турбонасосного агрегата жидкостного ракетного двигателя
RU2391545C1 (ru) * 2008-12-17 2010-06-10 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Жидкостный ракетный двигатель
RU2391542C1 (ru) * 2008-12-17 2010-06-10 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Жидкостный ракетный двигатель
RU2396453C1 (ru) * 2009-01-22 2010-08-10 Открытое акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель
FR2947871B1 (fr) * 2009-07-09 2011-11-25 Snecma Barriere anti-condensation sur circuit regeneratif
RU2410559C1 (ru) * 2009-08-13 2011-01-27 Открытое акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель
WO2011091162A1 (en) * 2010-01-20 2011-07-28 Firestar Engineering, Llc Insulated combustion chamber
WO2011152912A2 (en) * 2010-03-12 2011-12-08 Firestar Engineering, Llc Supersonic combustor rocket nozzle
CN108825406A (zh) * 2018-08-29 2018-11-16 北京航天动力研究所 一种液体火箭发动机推力室身部外壁结构
CN109807338B (zh) * 2019-01-25 2021-04-13 航天材料及工艺研究所 一种铼铌复合喷管的分段式制备方法
DE102021120637A1 (de) * 2021-08-09 2023-02-09 Arianegroup Gmbh Raketentriebwerksabschnitt mit porösem Innenwandteil und Verfahren zum Herstellen eines Raketentriebwerksabschnitts
CN114165362A (zh) * 2021-11-08 2022-03-11 湖北三江航天江北机械工程有限公司 液体火箭发动机燃烧室复合成形方法
CN114233516B (zh) * 2021-12-23 2023-05-09 南京航空航天大学 一种具有再生冷却功能的复合材料爆震发动机燃烧室结构

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US3153320A (en) * 1962-11-08 1964-10-20 Gen Motors Corp Cooled rocket nozzle design
US3516254A (en) * 1967-09-11 1970-06-23 United Aircraft Corp Closed-loop rocket propellant cycle

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100717376B1 (ko) 2004-12-29 2007-05-10 한국항공우주연구원 고압액체로켓엔진용 재생냉각 연소실

Also Published As

Publication number Publication date
DE3320556A1 (de) 1983-12-08
US4703620A (en) 1987-11-03
JPS6132495B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1986-07-28

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