FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to flying vehicles heavier than air. Fuselage structure comprises transverse and lengthwise bearing elements made up of fuselage frames 17-25 and lengthwise walls 26-29. Set of lengthwise walls 26-29 extends through fuselage midpoint 3 and tail 57 Centre wing section 12 is arranged in the plane of wing maximum overall height and made up of frames 17-25. Fuselage bottom has large-size lengthwise openings for cargo compartments 10, 14. Cutout bearing structure comprises lengthwise walls 26 jointed with central wing section frames.
EFFECT: redistribution of strains resulting from external loads due to optimum arrangement of structural elements.
4 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRFRAME OF MULTIMODE MONOPLANE | 1997 |
|
RU2173654C2 |
| MULTIFUNCTIONAL SUPERSONIC SINGLE-ENGINE AIRCRAFT | 2021 |
|
RU2770885C1 |
| MULTIMODE HIGH MANEUVERABILITY AIRCRAFT OF INTEGRAL AERODYNAMIC CONFIGURATION | 2009 |
|
RU2400402C1 |
| STRUCTURAL POWER LAYOUT OF AN AIRFRAME OF A STEALTH SINGLE-ENGINE AIRCRAFT | 2022 |
|
RU2798303C1 |
| MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS | 1996 |
|
RU2207968C2 |
| AIRCRAFT IN INTEGRAL AERODYNAMIC CONFIGURATION | 2010 |
|
RU2440916C1 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| HIGH-PERFORMANCE AIRCRAFT | 2022 |
|
RU2800101C1 |
| HIGH-CAPACITY AIRCRAFT | 2007 |
|
RU2335430C1 |
| MULTI-FUNCTIONAL TWO-SEAT STEALTH AIRCRAFT | 2023 |
|
RU2807624C1 |
