FIELD: aircraft engineering.
SUBSTANCE: claimed multicopter comprises the platform of propeller sets composed of lengthwise load-bearing beams, the frames, arranged in the flight direction. Crosswise structural beams are secured to said frames to support the motors with propellers, one at the end of every crosswise beam. Freight-and-passenger cabin with packs of storage batteries is attached from behind to said platform. The number of propeller units should allow the required airlift but cannot be less than 9 pairs (18 propeller groups) for reliable landing at the fault of 4 motors at a time.
EFFECT: variety of lift and purposes, higher flight safety.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL | 2018 |
|
RU2711633C2 |
| SMALL-SIZED VERTICAL TAKE-OFF/LANDING AIRCRAFT WITH AN INCREASED FLIGHT DISTANCE | 2017 |
|
RU2681464C1 |
| MULTICOPTER WITH COMBINED PROPELLERS AND HYBRID PROPELLER OF POWER PLANTS | 2022 |
|
RU2803214C1 |
| MULTICOPTER FRAME (OPTIONS) | 2017 |
|
RU2657650C1 |
| MULTICOPTER WITH FULL-TURN RUDDER, HYBRID PROPULSION SYSTEM AND COMBINED ENGINE-PROPELLER GROUPS | 2023 |
|
RU2831361C1 |
| AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING AND/OR VERTICAL TAKEOFF AND LANDING WITH SHORTENED RUN | 2021 |
|
RU2764311C1 |
| GYROPLANE | 2018 |
|
RU2673933C1 |
| MULTICOPTER WITH TWO-TIER ARRANGEMENT OF PROPELLER-DRIVEN GROUPS | 2021 |
|
RU2766284C1 |
| CONVERTIPLANE (VERSIONS) | 2010 |
|
RU2446078C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ADDITIONAL CARGO MODULES AND RETRACTABLE PROPELLERS | 2021 |
|
RU2759061C1 |
