| 摘要 |
Paramotor with dynamic torque compensation includes a frame (1), harness or seat (2), engine and propeller (3) rotating in a cage (4) characterized by one or more surfaces placed on the frame and/or the cage in such a way that when air flows around them aerodynamic forces are generated in the opposite direction to the propeller torque. These surfaces are characterized by an asymetric profile (13), a symetric profile with non-zero angle of attack (14), an asymmetric profile with non-zero angle of attack (15) or in a form of flaps or ailerons with non-zero angle of attack (16). The surfaces may have adjustable angle of attack (17). |
