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 MISSILESInfo
- 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
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)
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)
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)
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 |
-
1983
- 1983-12-14 FR FR8320047A patent/FR2556650B1/en not_active Expired
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 |