FIELD: aircraft engineering.
SUBSTANCE: proposed aircraft comprises airframe wherein central part 2 smoothly fairs with backswept outer wings 3, nose part 1 and tail part 6 wherein all-moving vertical tail 4 and horizontal tail 5 are arranged. Canopy 10 is arranged in airframe hose 1. Airframe features greater width in cross section and is made up of aerodynamic profiles with their height allowing accommodating freight compartment between air intakes.
EFFECT: uniform distribution of air load and increased load bearing qualities of airframe.
10 dwg
Title | Year | Author | Number |
---|---|---|---|
MULTI-FUNCTIONAL TWO-SEAT STEALTH AIRCRAFT | 2023 |
|
RU2807624C1 |
AIRCRAFT IN INTEGRAL AERODYNAMIC CONFIGURATION | 2010 |
|
RU2440916C1 |
MULTIFUNCTIONAL SUPERSONIC SINGLE-ENGINE AIRCRAFT | 2021 |
|
RU2770885C1 |
MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
HIGH-PERFORMANCE AIRCRAFT | 2022 |
|
RU2800101C1 |
DRONE | 2023 |
|
RU2818209C1 |
SUPERSONIC MANEUVERABLE AIRCRAFT | 2000 |
|
RU2180309C2 |
SWEPT-FORWARD WING WITH SWIVEL PART OF OUTER WING PANELS | 2005 |
|
RU2296082C1 |
MULTI-MODE AIRCRAFT-BOOSTER FOR AVIATION ROCKET SPACE COMPLEX | 1999 |
|
RU2175934C2 |
MULTIMODE AIRCRAFT OF INTEGRAL AERODYNAMIC CONFIGURATION | 1998 |
|
RU2138423C1 |
Authors
Dates
2010-09-27—Published
2009-09-09—Filed