FIELD: process engineering.
SUBSTANCE: invention relates to structural composite, particularly, to laminar structure with integrity protection element and to method of its fabrication. It includes light composite filler arranged between laminar composite linings. Said filler consists of section connected at buts with built-in elements for protection of integrity of lining. Retaining means composed by composite straps, plates covering the filler edges and sections located between filler and every lining are arranged between filler and every lining.
EFFECT: higher duration, higher strength of filler, its resistance to cracking, fracturing.
10 cl, 17 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FUSELAGE COMPOSITE SECTIONS JUNCTION ALONG WINDOW ZONE | 2013 |
|
RU2628262C2 |
| STRUCTURE OF LOAD-CARRYING AERODYNAMIC SURFACE OF AIRCRAFT | 0 |
|
SU572983A1 |
| METHOD OF RECONDITIONING THE HIGHLY CHARGED THREE-LAYER STRUCTURES MADE OF COMPOSITE MATERIAL | 1992 |
|
RU2039655C1 |
| AIRCRAFT WING AND OUTER WING JOINT ASSEMBLY | 2012 |
|
RU2481243C1 |
| REINFORCED STIFFNESS ELEMENTS AND METHODS OF THEIR PRODUCTION | 2009 |
|
RU2514747C2 |
| CIRCUMFERENTIAL BUTT JOINT FOR SKIN STRUCTURES | 2013 |
|
RU2658211C2 |
| BUTT JOINT OF LAMINATED PANELS OF ENCLOSURE STRUCTURES | 0 |
|
SU979593A1 |
| BUTT JOINT OF LAMINATED PANELS OF FENCING STRUCTURES | 0 |
|
SU894094A1 |
| LAMINATED CELLULAR PANEL | 0 |
|
SU973750A1 |
| COMPOSITE RADIUS AGGREGATES AND METHODS OF THEIR MANUFACTURE | 2013 |
|
RU2636494C2 |
