A blade actuation system comprises at least one motor coupled to a rotor blade for changing the pitch angle of the rotor blade. The motor is configured to wirelessly communicate with at least one flight control computer to modulate the pitch angle. At least one generator may be mounted on a...
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14. A helicopter, comprising: a rotor shaft; a rotor hub fixedly connectable to the rotor shaft; a plurality of rotor blades connectable to the rotor hub; a plurality of generators configured to rotate with the rotor shaft for generating power; a plurality of motors operatively coupled to the...
Ganguli R, Jehnert B, Wolfram J, et al. Optimal location of centre of gravity for swashplateless helicopter UAV and MAV. Aircr Eng Aerosp Technol 2007; 79: 335-345.Optimal location of centre of gravity for swashplateless helicopter UAV and MAV[J] . Ranjan Ganguli,Beatrix Jehnert,Jens ...
Shen, J., Chopra, I., and Johnson, W., "Performance of Swashplateless Helicopter with Trailing-Edge Flaps for Primary Flight Control," Journal of the American Helicopter Society, Vol. 55, (4), October 2010.Shen, J., Chopra, I., and ...
Significant hub forces and moments are produced as well.;For a production swashplateless helicopter, it may be prudent to eliminate the pitch links by reducing the blade structural stiffness. A novel wire sensor system network is proposed in order to measure blade elastic flap bending, lead-lag ...
Chao, Development of swashplateless helicopter blade pitch control system using the limited angle direct-drive motor (LADDM), Chinese Journal of Aeronautics, vol. 28, no. 5, pp. 1416-1425, 2015;Development of swashplateless helicopter blade pitch control system using the limited angle direct-...
Chopra, "Swashplateless helicopter rotor with trailing-edge flaps," Journal of Aircraft, vol. 41, no. 2, pp. 208- 214, 2004.Shen Jinwei,Chopra I.Swashplateless helicopter rotor with trailing-edge flaps. Journal of Aircraft . 2004Shen, J., and Chopra, I., "Swashplateless Helicopter Rotor...
Chao, Development of swashplateless helicopter blade pitch control system using the limited angle direct-drive motor (LADDM), Chinese Journal of Aeronautics, vol. 28, no. 5, pp. 1416-1425, 2015;Development of swashplateless helicopter blade pitch control system using the limited angle direct-...
A blade actuation system comprises at least one motor coupled to a rotor blade for changing the pitch angle of the rotor blade. The motor is configured to wirelessly communicate with at least one flight control computer to modulate the pitch angle. At least one generator may be mounted on a...