Of remotely piloted helicopter rotor head and remote control helicopter

摘要

The present invention is a conventional R / C helicopter based on the knowledge of the position of appearance of gyro precession are different, to improve the operability by more stable flight behavior of the R / C helicopter. The A coaxial inversion formula on R / C helicopter rotor head, smaller than the gyro precession of each of the main rotor as an output the top and bottom of the main rotor MR is with respect to the operation input SI from the swash plate is 90 degrees to correspond to appear that in the range, the main mast 13a to attach the top and bottom of the main rotor for each of the input position of the cyclic control of the up-down of the swashplate up and down of the main rotor, than 90 degrees 13b around is provided in the small angle and constitutes the upper and lower main rotor top and bottom of the swash plate is connected by a link mechanism. [Selection Figure 7