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FR2556650B1 - PROCESS AND DEVICE FOR MANUFACTURING HOLLOW STRUCTURAL BODY OF COMPOSITE MATERIAL, ESPECIALLY FOR MISSILES - Google Patents

PROCESS AND DEVICE FOR MANUFACTURING HOLLOW STRUCTURAL BODY OF COMPOSITE MATERIAL, ESPECIALLY FOR MISSILES

Info

Publication number
FR2556650B1
FR2556650B1 FR8320047A FR8320047A FR2556650B1 FR 2556650 B1 FR2556650 B1 FR 2556650B1 FR 8320047 A FR8320047 A FR 8320047A FR 8320047 A FR8320047 A FR 8320047A FR 2556650 B1 FR2556650 B1 FR 2556650B1
Authority
FR
France
Prior art keywords
missiles
composite material
structural body
hollow structural
manufacturing hollow
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
Application number
FR8320047A
Other languages
French (fr)
Other versions
FR2556650A1 (en
Inventor
Michel Rouillot
Jean-Michel Lesprit
Daniel Jordan
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.)
Societe des Telephones Ericsson SA
Original Assignee
Societe des Telephones Ericsson SA
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 des Telephones Ericsson SA filed Critical Societe des Telephones Ericsson SA
Priority to FR8320047A priority Critical patent/FR2556650B1/en
Publication of FR2556650A1 publication Critical patent/FR2556650A1/en
Application granted granted Critical
Publication of FR2556650B1 publication Critical patent/FR2556650B1/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00—Producing articles with hollow walls
    • B29D24/001—Producing articles with hollow walls formed of hollow ridges or ribs, e.g. separate ridges; continuous corrugated structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail fins
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2023/00—Tubular articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3097—Cosmonautical vehicles; Rockets

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
FR8320047A 1983-12-14 1983-12-14 PROCESS AND DEVICE FOR MANUFACTURING HOLLOW STRUCTURAL BODY OF COMPOSITE MATERIAL, ESPECIALLY FOR MISSILES Expired FR2556650B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8320047A FR2556650B1 (en) 1983-12-14 1983-12-14 PROCESS AND DEVICE FOR MANUFACTURING HOLLOW STRUCTURAL BODY OF COMPOSITE MATERIAL, ESPECIALLY FOR MISSILES

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8320047A FR2556650B1 (en) 1983-12-14 1983-12-14 PROCESS AND DEVICE FOR MANUFACTURING HOLLOW STRUCTURAL BODY OF COMPOSITE MATERIAL, ESPECIALLY FOR MISSILES

Publications (2)

Publication Number Publication Date
FR2556650A1 FR2556650A1 (en) 1985-06-21
FR2556650B1 true FR2556650B1 (en) 1986-05-23

Family

ID=9295182

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8320047A Expired FR2556650B1 (en) 1983-12-14 1983-12-14 PROCESS AND DEVICE FOR MANUFACTURING HOLLOW STRUCTURAL BODY OF COMPOSITE MATERIAL, ESPECIALLY FOR MISSILES

Country Status (1)

Country Link
FR (1) FR2556650B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2630502B1 (en) * 1988-04-25 1990-08-31 Europ Propulsion COMPOSITE PROPELLER WITH INTEGRATED COMPOSITE WINGS AND MANUFACTURING METHOD THEREOF
DE3927798A1 (en) * 1989-08-23 1991-03-14 Rheinmetall Gmbh Stable missile tail unit - consists of aluminium or steel with low resistance or relatively high wt.
FR2707552B1 (en) * 1993-06-30 1995-10-13 Aerospatiale Method of manufacturing a part made of composite material, a central body and fins and missile body thus obtained.
FR2879496B1 (en) * 2004-12-16 2008-12-12 Eurocopter France METHOD AND DEVICE FOR MANUFACTURING A HELICOPTER ROTOR CARENE, AND CARENE OBTAINED
CN104897009B (en) * 2015-05-04 2017-03-01 晋西工业集团有限责任公司 A kind of interlayer of resistance to ablation complex structure empennage and its processing method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US337235A (en) * 1886-03-02 John h
FR1169030A (en) * 1955-12-22 1958-12-19 Bristol Aeroplane Co Ltd Improvements in the fabrication and construction of resin-bonded fibrous hollow bodies
GB1202340A (en) * 1968-12-23 1970-08-12 Parsons Corp Method of making helicopter rotor spars
FR2490993A3 (en) * 1980-10-01 1982-04-02 Aerospatiale Reusable mould for making complex hollow reinforced profiles - using an inflatable core in split rigid external mould

Also Published As

Publication number Publication date
FR2556650A1 (en) 1985-06-21

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Legal Events

Date Code Title Description
ST Notification of lapse