FR1237054A - Revêtement armé, en particulier pour l'aviation - Google Patents
Revêtement armé, en particulier pour l'aviationInfo
- Publication number
- FR1237054A FR1237054A FR806876A FR806876A FR1237054A FR 1237054 A FR1237054 A FR 1237054A FR 806876 A FR806876 A FR 806876A FR 806876 A FR806876 A FR 806876A FR 1237054 A FR1237054 A FR 1237054A
- Authority
- FR
- France
- Prior art keywords
- aviation
- armored coating
- armored
- coating
- 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
- 239000011248 coating agent Substances 0.000 title 1
- 238000000576 coating method Methods 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
- E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1237054X | 1958-10-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1237054A true FR1237054A (fr) | 1960-07-22 |
Family
ID=10884934
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR806876A Expired FR1237054A (fr) | 1958-10-06 | 1959-10-06 | Revêtement armé, en particulier pour l'aviation |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1237054A (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2177640A1 (fr) * | 1972-03-31 | 1973-11-09 | Dassault Avions | |
FR2180508A1 (en) * | 1972-04-19 | 1973-11-30 | Dassault Avions | Composite sandwich panels - having resin sealed cellular metal cores to inhibit liquid pick up |
-
1959
- 1959-10-06 FR FR806876A patent/FR1237054A/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2177640A1 (fr) * | 1972-03-31 | 1973-11-09 | Dassault Avions | |
FR2180508A1 (en) * | 1972-04-19 | 1973-11-30 | Dassault Avions | Composite sandwich panels - having resin sealed cellular metal cores to inhibit liquid pick up |
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