FIELD: aeronautics.
SUBSTANCE: connection of wing with the fuselage, in which wing (2), located at the top of the fuselage (1), is connected to the fuselage (1) through several connecting elements (3, 4, 5, 6), and the connecting elements (3, 4, 5, 6) are provided for the perception of strength in different directions, and each of them has a maximum load capacity, designed primarily for the nominal load during flight and landing or nominal emergency loads. According to the invention, the ability to bear a load of separate connecting elements (3, 4, 5, 6) of the wing and their direction of forces perception are aligned so that the failure of one of the connecting elements (3, 4, 5, 6) the maximum ability to withstand the load of remaining connecting elements (3, 4, 5, 6) is sufficient to secure the normal flight mode.
EFFECT: improved load bearing.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR RETAINING TANK IN AIRCRAFT | 2014 |
|
RU2662588C2 |
| AIRCRAFT ENGINE ASSEMBLY WITH ANNULAR BEARING STRUCTURE COVERING TURBOJET CENTRAL HOUSING | 2009 |
|
RU2487058C2 |
| AIRCRAFT ENGINE SUPPORT COMPRISING TWO TIE RODS WITH TRANSVERSE JOINTING ELEMENT | 2007 |
|
RU2433068C2 |
| AIRCRAFT TAIL AND METHOD OF ITS ASSEMBLY | 2009 |
|
RU2501711C2 |
| AIRCRAFT WITH FOLDING WING AND WING FOLDING DEVICE | 2019 |
|
RU2727896C1 |
| METHOD FOR TESTING CENTRAL PART OF FUSELAGE OF LIGHT HELICOPTER | 2023 |
|
RU2816120C1 |
| DEVICE TO SECURE LIFT CREATING MEMBER ON AIRCRAFT FUSELAGE | 2008 |
|
RU2415774C1 |
| AIRCRAFT WITH FIN ASSEMBLY OF "CODFISH TAIL" TYPE AND WITH REAR-MOUNTED ENGINE | 2010 |
|
RU2522539C2 |
| AIRFRAME OF MULTIPURPOSE CLASS VI AIRCRAFT | 2010 |
|
RU2462395C2 |
| AIRFRAME OF MULTIMODE MONOPLANE | 1997 |
|
RU2173654C2 |
