FIELD: aviation; fuselages, wings and other structural members. SUBSTANCE: skin has boundaries of front and rear sides in cross section. Boundary line at boundary of front and/or rear side and/or at one of vertices of section is made in form of fragment and/or combination of fragments of oblique taper section of right circular cone. EFFECT: improved strength characteristics under vibration conditions; Localizing and excluding cracking and intermittent and/or alternating loads. 21 cl, 18 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LAMINATED SKIN OF FLYING VEHICLE | 1999 |
|
RU2144482C1 |
| FLYING VEHICLE HATCH COVER | 1999 |
|
RU2144483C1 |
| FLYING VEHICLE LAMINATED HATCH COVER | 1999 |
|
RU2144484C1 |
| SHIP'S LAMINATED SKIN | 1999 |
|
RU2143363C1 |
| SHIP'S SKIN | 1999 |
|
RU2143362C1 |
| SHIP'S HATCH COVER | 1999 |
|
RU2143366C1 |
| LAMINATED COVER FOR SHIP'S HATCH | 1999 |
|
RU2143367C1 |
| FLYING VEHICLE RIB | 1999 |
|
RU2144485C1 |
| FLYING VEHICLE SPAR | 1999 |
|
RU2144488C1 |
| GLASS | 1999 |
|
RU2145552C1 |
