JPS6082603A - ロケツト燃焼器製作法 - Google Patents

ロケツト燃焼器製作法

Info

Publication number
JPS6082603A
JPS6082603A JP58188805A JP18880583A JPS6082603A JP S6082603 A JPS6082603 A JP S6082603A JP 58188805 A JP58188805 A JP 58188805A JP 18880583 A JP18880583 A JP 18880583A JP S6082603 A JPS6082603 A JP S6082603A
Authority
JP
Japan
Prior art keywords
filler
groove
compression molding
cylinder
point alloy
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
JP58188805A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6324043B2 (en]
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
Masaki Sasaki
正樹 佐々木
Hiromi Gomi
五味 広美
Hiroshi Sakamoto
博 坂本
Yoshimichi Masuda
増田 良道
Kagozou Watanabe
渡辺 龍三
Jiyunjirou Takegawa
武川 淳二郎
Yoshihiko Doi
良彦 土井
Atsushi Kuroishi
黒石 農士
Yoshinobu Takeda
義信 武田
Shigeki Ochi
越智 茂樹
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
Sumitomo Electric Industries Ltd
Original Assignee
National Aerospace Laboratory of Japan
Sumitomo Electric Industries Ltd
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, Sumitomo Electric Industries Ltd filed Critical National Aerospace Laboratory of Japan
Priority to JP58188805A priority Critical patent/JPS6082603A/ja
Priority to US06/653,012 priority patent/US4584171A/en
Priority to DE19843436419 priority patent/DE3436419C2/de
Priority to FR8415406A priority patent/FR2553148B1/fr
Publication of JPS6082603A publication Critical patent/JPS6082603A/ja
Publication of JPS6324043B2 publication Critical patent/JPS6324043B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture 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
    • B22F7/06Manufacture 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
    • 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
    • F02K9/64Combustion or thrust chambers having cooling arrangements
    • 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
    • Y10T29/4981Utilizing transitory attached element or associated separate material

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Powder Metallurgy (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
JP58188805A 1983-10-07 1983-10-07 ロケツト燃焼器製作法 Granted JPS6082603A (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP58188805A JPS6082603A (ja) 1983-10-07 1983-10-07 ロケツト燃焼器製作法
US06/653,012 US4584171A (en) 1983-10-07 1984-09-21 Method of producing rocket combustors
DE19843436419 DE3436419C2 (de) 1983-10-07 1984-10-04 Verfahren zur Herstellung von Raketenbrennkammern
FR8415406A FR2553148B1 (fr) 1983-10-07 1984-10-08 Procede pour realiser des chambres de combustion pour fusees

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58188805A JPS6082603A (ja) 1983-10-07 1983-10-07 ロケツト燃焼器製作法

Publications (2)

Publication Number Publication Date
JPS6082603A true JPS6082603A (ja) 1985-05-10
JPS6324043B2 JPS6324043B2 (en]) 1988-05-19

Family

ID=16230108

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58188805A Granted JPS6082603A (ja) 1983-10-07 1983-10-07 ロケツト燃焼器製作法

Country Status (2)

Country Link
US (1) US4584171A (en])
JP (1) JPS6082603A (en])

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100450699B1 (ko) * 2002-05-06 2004-10-01 주식회사 로템 액체로켓엔진용 연소기 제조 방법
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

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4942653A (en) * 1989-08-25 1990-07-24 Rockwell International Corporation Production method for a channeled wall thrust nozzle
US5075966A (en) * 1990-09-04 1991-12-31 General Electric Company Method for fabricating a hollow component for a rocket engine
US5130084A (en) * 1990-12-24 1992-07-14 United Technologies Corporation Powder forging of hollow articles
US5249357A (en) * 1993-01-27 1993-10-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of fabricating a rocket engine combustion chamber
US5546656A (en) * 1994-11-30 1996-08-20 United Technologies Corporation Fabrication of rocket thrust chambers
US5822853A (en) * 1996-06-24 1998-10-20 General Electric Company Method for making cylindrical structures with cooling channels
US5802842A (en) * 1996-07-29 1998-09-08 Trw Inc. Dimensionally stable throat insert for rocket thrusters
US6321449B2 (en) * 1998-11-12 2001-11-27 General Electric Company Method of forming hollow channels within a component
US6131280A (en) * 1998-11-30 2000-10-17 United Technologies Corporation Method of repairing a rocket thrust chamber
US6134782A (en) * 1998-11-30 2000-10-24 United Technologies Corporation Method of forming a rocket thrust chamber
US6042780A (en) * 1998-12-15 2000-03-28 Huang; Xiaodi Method for manufacturing high performance components
US6582542B1 (en) 1999-07-07 2003-06-24 Mark C. Russell Method of producing a channeled wall fluid control apparatus
DE60226309T2 (de) * 2001-01-11 2009-05-20 Volvo Aero Corp. Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds
KR100433244B1 (ko) * 2001-03-28 2004-05-24 대한소결금속 주식회사 압축기용 플랜지의 제조 방법
JP2004156131A (ja) * 2002-09-13 2004-06-03 Honda Motor Co Ltd 金属成形体の製造方法
US7213392B2 (en) * 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
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
US20160102862A1 (en) * 2014-10-08 2016-04-14 Solar Turbines Incorporated Method for manufacturing a machine component
CN113787307B (zh) * 2021-09-09 2022-07-26 西安远航真空钎焊技术有限公司 一种收扩管段工件的加工方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB491416A (en) * 1936-12-15 1938-09-01 Wuppertaler Metallverarbeitung A method of uniting a porous metal layer with a metal body
US3103885A (en) * 1959-08-31 1963-09-17 Mclauchlan James Charles Sweat cooled articles
SU149226A1 (ru) * 1961-05-25 1961-11-30 А.П. Малин Способ изготовлени деталей машин
GB1079734A (en) * 1963-10-14 1967-08-16 Kobe Steel Ltd Method of forming metal coatings
US3531848A (en) * 1966-01-10 1970-10-06 Battelle Development Corp Fabrication of integral structures
US3549357A (en) * 1968-06-24 1970-12-22 Allegheny Ludlum Steel Dry impact coating of powder metal parts
US4431449A (en) * 1977-09-26 1984-02-14 Minnesota Mining And Manufacturing Company Infiltrated molded articles of spherical non-refractory metal powders
JPS58217605A (ja) * 1982-06-08 1983-12-17 Natl Aerospace Lab ロケツト燃焼器製作法

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100450699B1 (ko) * 2002-05-06 2004-10-01 주식회사 로템 액체로켓엔진용 연소기 제조 방법
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

Also Published As

Publication number Publication date
US4584171A (en) 1986-04-22
JPS6324043B2 (en]) 1988-05-19

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