ES2143346A1 - Nucleo mecanico desmontable y procedimientos de instalacion. - Google Patents

Nucleo mecanico desmontable y procedimientos de instalacion.

Info

Publication number
ES2143346A1
ES2143346A1 ES009601350A ES9601350A ES2143346A1 ES 2143346 A1 ES2143346 A1 ES 2143346A1 ES 009601350 A ES009601350 A ES 009601350A ES 9601350 A ES9601350 A ES 9601350A ES 2143346 A1 ES2143346 A1 ES 2143346A1
Authority
ES
Spain
Prior art keywords
dismountable mechanical
implementing
procedure
mechanical core
core
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
ES009601350A
Other languages
English (en)
Other versions
ES2143346B1 (es
Inventor
Jean-Francois Tillac
Jean Pierre Houguet
Alain Soulignac
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.)
Safran Ceramics SA
Original Assignee
Societe Nationale des Poudres et Explosifs
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 Societe Nationale des Poudres et Explosifs filed Critical Societe Nationale des Poudres et Explosifs
Publication of ES2143346A1 publication Critical patent/ES2143346A1/es
Application granted granted Critical
Publication of ES2143346B1 publication Critical patent/ES2143346B1/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • F02K9/24Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges
    • 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
    • F05D2230/21Manufacture essentially without removing material by casting
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S425/00Plastic article or earthenware shaping or treating: apparatus
    • Y10S425/043Rocket fuel core

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Lighters Containing Fuel (AREA)
  • Ceramic Products (AREA)
  • Developing Agents For Electrophotography (AREA)

Abstract

Núcleo mecánico desmontable y procedimiento de instalación. La presente invención se refiere.a un núcleo mecánico desmontable (1) que comprende una contra-forma (2) fijada sobre un mandril central (3, 8), debiendo poder ser manipulados a distancia y con total seguridad los elementos de la contra-forma. Estos elementos (10, 11, ...) de contra-forma están ligados y fijados sobre el mandril central (3, 8) mediante unos dispositivos (6) de anclaje de varillas. La presente invención se refiere también a unos procedimientos de ensamblaje y de desensamblaje de dicho núcleo. Este núcleo mecánico desmontable se utiliza fundamentalmente para el modelado de la cavidad interna de carga de propergol sólido.
ES009601350A 1995-08-04 1996-06-18 Nucleo mecanico desmontable y procedimientos de instalacion. Expired - Fee Related ES2143346B1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9509498A FR2737538B1 (fr) 1995-08-04 1995-08-04 Noyau mecanique demontable et procedes de mise en oeuvre

Publications (2)

Publication Number Publication Date
ES2143346A1 true ES2143346A1 (es) 2000-05-01
ES2143346B1 ES2143346B1 (es) 2000-11-01

Family

ID=9481708

Family Applications (1)

Application Number Title Priority Date Filing Date
ES009601350A Expired - Fee Related ES2143346B1 (es) 1995-08-04 1996-06-18 Nucleo mecanico desmontable y procedimientos de instalacion.

Country Status (4)

Country Link
US (1) US5714081A (es)
ES (1) ES2143346B1 (es)
FR (1) FR2737538B1 (es)
IT (1) IT1284719B1 (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITTO20030799A1 (it) * 2003-10-10 2005-04-11 Avio Spa Metodo per la distibuzione di un propellente all'interno
JP6623230B2 (ja) * 2015-03-27 2019-12-18 チェアマン,ディフェンス リサーチ アンド ディヴェロップメント オーガナイゼーション (ディーアールディーオー)Chairman, Defence Research & Development Organisation (Drdo) マンドレル組立体、及びこのマンドレル組立体を用いて固体ロケットの推進薬グレインを製造する方法
FR3035661B1 (fr) * 2015-04-30 2018-11-16 Arianegroup Sas Ensemble pour l'extraction d'au moins un secteur de moule
KR102124070B1 (ko) * 2018-10-10 2020-06-17 주식회사 한화 추진기관용 폼 코어 제거용 장치 및 이를 이용한 추진기관 내 폼 코어 제거 방법
KR102124069B1 (ko) * 2018-10-10 2020-06-17 주식회사 한화 추진기관의 레이디얼 슬롯 제조용 분할형 코어 및 이를 이용한 추진 기관의 추진제 그레인 제조방법
FR3090751B1 (fr) 2018-12-20 2021-01-08 Arianegroup Sas Noyau démontable pour la fabrication d'un chargement de propergol et procédé de mise en oeuvre
CN110230553A (zh) * 2019-07-15 2019-09-13 武汉乾峯智能科技有限公司 自动化取模装置
CN110282533A (zh) * 2019-07-15 2019-09-27 武汉乾峯智能科技有限公司 拾取移动同步平移机构及自动化取模装置
CN112571822B (zh) * 2020-10-29 2023-03-28 上海新力动力设备研究所 适用于带药缠绕的记忆非金属芯模结构及壳体成型方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3270999A (en) * 1963-04-12 1966-09-06 Thiokol Chemical Corp Segmented core for molding a cavity in a cast solid propellant rocket motor
US3345693A (en) * 1965-01-27 1967-10-10 Thiokol Chemical Corp Apparatus for forming ignition surfaces in solid propellant motors
US3567174A (en) * 1968-03-18 1971-03-02 Thiokol Chemical Corp Breakdown core for forming a cavity in a solid propellant grain

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US875097A (en) * 1906-08-16 1907-12-31 George F Mckee Collapsible core.
US3193883A (en) * 1960-09-07 1965-07-13 Jr Joseph G Thibodaux Mandrel for shaping solid propellant rocket fuel into a motor casing
US3952627A (en) * 1962-08-27 1976-04-27 Thiokol Corporation Slot former assembly for use in solid propellant rocket motors
US3983780A (en) * 1962-11-14 1976-10-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Casting propellant in rocket engine
US3237913A (en) * 1963-06-24 1966-03-01 Thiokol Chemical Corp Collapsible mandrel for forming a cavity in solid propellant rocket fuel
US3357189A (en) * 1965-09-08 1967-12-12 Thiokol Chemical Corp A precast hollow core charge for a rocket motor and method for casting same
US3492815A (en) * 1967-03-10 1970-02-03 Thiokol Chemical Corp Means for forming radial slots in solid propellant grains
GB1232923A (es) * 1969-04-03 1971-05-26 Imp Metal Ind Kynoch Ltd
US4761254A (en) * 1986-04-14 1988-08-02 Morton Thiokol, Inc. Method of and apparatus for fabricating a tool to form an asymmetrical constant cross section bore in the propellant in a solid rocket motor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3270999A (en) * 1963-04-12 1966-09-06 Thiokol Chemical Corp Segmented core for molding a cavity in a cast solid propellant rocket motor
US3345693A (en) * 1965-01-27 1967-10-10 Thiokol Chemical Corp Apparatus for forming ignition surfaces in solid propellant motors
US3567174A (en) * 1968-03-18 1971-03-02 Thiokol Chemical Corp Breakdown core for forming a cavity in a solid propellant grain

Also Published As

Publication number Publication date
US5714081A (en) 1998-02-03
IT1284719B1 (it) 1998-05-21
ES2143346B1 (es) 2000-11-01
FR2737538B1 (fr) 1997-08-29
FR2737538A1 (fr) 1997-02-07
ITTO960666A1 (it) 1998-01-31

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