FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Claimed rotor (14) comprises the rotor (30) exploiting the Magnus effect and rotor (32) with transverse direction of airflow and guide (34). Said rotor exploiting the Magnus effect is actuated by the first drive (20) to spin around the shaft (38 and has the closed side surface (36). Said rotor with transverse direction of airflow fitted on the shaft to spin there about has the set (40) of blades (42) extending axially. Said blades are gyrated about the shaft by the drive (22) and fixed relative to tangential angular position (54). Rotor exploiting the Magnus effect is built in the rotor with transverse direction of airflow, the axis of the former extends in direction of rotational axis. Afore said guide has structural segment (56) developing partially the rotor with transverse airflow direction. Note here that said structural element incorporates the mechanism (58) to change the position relative to rotor exploiting the Magnus effect.
EFFECT: decreased weight, higher efficiency of production.
12 cl, 11 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| WIND-POWER HYBRID ROTOR | 2011 |
|
RU2579426C2 |
| AIRCRAFT BASED ON MAGNUS EFFECT | 2024 |
|
RU2827521C1 |
| PROPULSION SYSTEM OF HIGH-SPEED ROTARY-WINGED AIRCRAFT (VERSIONS) | 2015 |
|
RU2629635C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH HYBRID POWER PLANT | 2017 |
|
RU2724940C2 |
| AIRCRAFT | 2016 |
|
RU2682954C1 |
| HYBRID AIRCRAFT | 1996 |
|
RU2160689C2 |
| DEVICE FOR CREATING LIFT FORCE | 1992 |
|
RU2041137C1 |
| AIRCRAFT | 2019 |
|
RU2711768C1 |
| HIGH-SPEED LONG-RANGE HYBRID HELICOPTER WITH OPTIMISED ROTOR | 2008 |
|
RU2445236C2 |
| HIGH-SPEED HYBRID LARGE-RANGE HELICOPTER | 2008 |
|
RU2473454C2 |
