FIELD: vibration equipment.
SUBSTANCE: invention can be used in design of reactive convertible rotary-wing aircraft. Unmanned Attack Aircraft Helicopter (UAAH) has fuselage, weapon system on launching devices, wing with control elements, power plant engine, on-board control system providing telemechanical control from command post (CP) of carrier vehicle. UAAH comprises asymmetrically variable sweep wing (AVSW) and on its consoles two double-blade rotors (DBR), inverted V-shaped fins and in stern nacelle free power turbines, driving DBR and/or remote fan, creating at vertical and short take-off and landing (VTOL and STOL) lifting force and sustainer jet with operating/autorotating transverse DBR or their fixed blades-wings asymmetrically variable sweep angle χ=±30° to AVSW front edge with swept angle χ=±60° during horizontal flight in configuration of jet rotorcraft/winged gyroplane or transonic aircraft.
EFFECT: higher speed and range of flight, higher probability of destruction of underwater or surface target located at long range.
4 cl, 3 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| UNMANNED AIRCRAFT-HELICOPTER-MISSILE CARRIER | 2019 |
|
RU2708782C1 |
| AIRCRAFT-MISSILE STRIKE SYSTEM | 2019 |
|
RU2721803C1 |
| MULTIPURPOSE MISSILE AVIATION SYSTEM | 2019 |
|
RU2738224C2 |
| AIR MISSILE SYSTEM WITH AN UNMANNED PERCUSSIVE AIRCRAFT HELICOPTER | 2018 |
|
RU2710317C1 |
| ADAPTIVE AIRBORNE MISSILE SYSTEM | 2019 |
|
RU2720592C1 |
| UNMANNED TRANSONIC AIRCRAFT-HELICOPTER | 2018 |
|
RU2711451C1 |
| ADAPTIVE AVIATION-MISSILE SYSTEM | 2019 |
|
RU2720569C1 |
| STEALTHY ROCKET AND AIRCRAFT COMPLEX | 2019 |
|
RU2722609C1 |
| HYBRID JET PLANE-HELICOPTER | 2019 |
|
RU2706430C1 |
| AIRCRAFT IMPACT MISSILE SYSTEM | 2019 |
|
RU2722520C1 |
