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).
PARAMOTOR WITH DYNAMIC TORQUE COMPENSATION
06.08.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Numerical investigations of ducted propeller aerodynamics for a mini paramotor UAV
American Institute of Physics | 2018
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