| 摘要 |
PURPOSE: An apparatus for compensating a P-factor is provided to automatically compensate the P-factor with minimum mechanical devices added according to engine power, attack angle, and equivalent airspeed. CONSTITUTION: An apparatus for compensating a P-factor comprises a first adjusting part (130), an attack angle- airspeed integrated probe, a second adjusting part, and a final adjusting part (320). The first adjusting part applies force to the final adjusting part through a first steel wire (140) in proportion to the opening degree of a throttle measured by a throttle control lever (120). The attack angle-airspeed integrated probe mechanically measures attack angle and equivalent airspeed. The second adjusting part applies force to the final adjusting part through a second steel wire (240) in proportion to an attack angle known from the rotation of the attack angle-airspeed integrated probe and in inverse proportion to an indicated airspeed known from the longitudinal movement of an aircraft of the attach-airspeed integrated probe. The final adjusting part transfers force for rotating a rudder (400) to right side in proportion to the force receiving from the first and second adjusting parts.
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