FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, particularly to combined aircraft. Proposed combined aircraft comprises elongated airframe, rotor with blades to generate lift and wings extending aside of airframe on its both sides. Every wing is arranged on airframe to turn about its lengthwise axis. Aforesaid rotor incorporates casing to accommodate slip-in/out-blades.
EFFECT: smooth control in changing from propelled flight to gliding flight.
7 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2742496C2 |
| COMBINED AIRCRAFT | 2014 |
|
RU2581110C1 |
| ZERO FLIGHT AIRCRAFT | 2018 |
|
RU2746025C2 |
| HYBRID AIRCRAFT | 1996 |
|
RU2160689C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH AUXILIARY AIR PROPELLERS FOR FLIGHT CONTROL | 2021 |
|
RU2762441C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2021 |
|
RU2805888C2 |
| UNMANNED AERIAL VEHICLE FOR VERTICAL TAKE-OFF AND LANDING | 2023 |
|
RU2799426C1 |
| FAST-SPEED COMBINED HELICOPTER | 2016 |
|
RU2610326C1 |
| HIGH-SPEED TURBOFAN COMBINED HELICOPTER | 2016 |
|
RU2629475C1 |
| CONVERTIPLANE | 2019 |
|
RU2723516C1 |
