FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering. Fuselage caisson consists of U-shaped upper and lower panels made of carrier layers of polymer composite material and aggregate. Fuselage side panels are integrated into the top panel. Height of the bottom panel placeholder exceeds the height of the top panel placeholder. Upper and lower panels of the fuselage box can be interconnected along the entire length of the flanges by a glue-and-bolt connection made with anchor nuts and fasteners.
EFFECT: invention is aimed at increasing the resource.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CAISSON OF WING DETACHABLE PART | 2017 |
|
RU2690300C1 |
| METHOD TO ASSEMBLE WING FROM POLYMER COMPOSITE MATERIAL | 2016 |
|
RU2613661C1 |
| METHOD FOR MANUFACTURING AN ADAPTIVE WING WITH FLEXIBLE GAPLESS MECHANIZATION | 2022 |
|
RU2784223C1 |
| STRUCTURE MADE OF COMPOSITE MATERIALS, AIRCRAFT MAIN WING AND BODY CONTAINING SAID STRUCTURE | 2010 |
|
RU2518927C2 |
| SUPPORT UNIT FOR THREE-LAYER PANEL | 2006 |
|
RU2322354C1 |
| HELICOPTER FUSELAGE | 1993 |
|
RU2090450C1 |
| AIRCRAFT WING AND OUTER WING JOINT ASSEMBLY | 2012 |
|
RU2481243C1 |
| AIRCRAFT FUSELAGE STRUCTURE AND MANUFACTURING METHOD | 2007 |
|
RU2435703C2 |
| AIRCRAFT WING | 2014 |
|
RU2557638C1 |
| MOVABLE TAILPLANE FOR AIRCRAFT | 1997 |
|
RU2166460C2 |
