FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering and can be used in design of rotary-wing aircraft. Unmanned aircraft-helicopter-missile carrier (UAHMC) has fuselage with wing and tail unit, engine, onboard control system (OCS), detachable controlled missile. UAHMC has high-lying wing asymmetrically variable sweep and on rounded in plan its tips – two double-bladed rotors (DBR), tail empennage of seagull type and in stern nacelle – free power turbine, leading DBR and portable turbofan. DBR and turbo-fan create, at vertical and short take-off and landing, lifting force and reactive cruise thrust with running/autorotating transverse DBR or fixed by wings with their hollow wing blades of asymmetrically variable sweep to outside from center of weights at horizontal flight in configuration of jet rotary-wing/gyroplane and transonic aircraft, which has aircraft guided missiles in bomb compartment. UAHMC is made with the possibility of folding the blades DBR, wing and tail empennage after landing on carrier ship.
EFFECT: higher speed and range of flight, higher probability of destruction of surface, underwater and air targets located at long range.
5 cl, 3 dwg, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
UNMANNED TRANSONIC AIRCRAFT-HELICOPTER | 2018 |
|
RU2711451C1 |
UNMANNED IMPACT HELICOPTER AIRCRAFT | 2019 |
|
RU2733678C1 |
AIR MISSILE SYSTEM WITH AN UNMANNED PERCUSSIVE AIRCRAFT HELICOPTER | 2018 |
|
RU2710317C1 |
AIRCRAFT-MISSILE STRIKE SYSTEM | 2019 |
|
RU2721803C1 |
ADAPTIVE AIRBORNE MISSILE SYSTEM | 2019 |
|
RU2720592C1 |
MULTIPURPOSE MISSILE AVIATION SYSTEM | 2019 |
|
RU2738224C2 |
ADAPTIVE AVIATION-MISSILE SYSTEM | 2019 |
|
RU2720569C1 |
AIRCRAFT IMPACT MISSILE SYSTEM | 2019 |
|
RU2722520C1 |
HYBRID JET PLANE-HELICOPTER | 2019 |
|
RU2706430C1 |
HIGH-SPEED JET AIRCRAFT-HELICOPTER | 2018 |
|
RU2706294C1 |
Authors
Dates
2019-12-11—Published
2019-01-10—Filed