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1.飞机的操纵面副翼,用于绕飞机纵轴作横滚运动的横向操纵(见图左上A);升降舵,用于绕飞机横轴作俯仰运动的俯仰操纵(见图左中B);方向舵,用于绕飞机立轴作偏航运动的航向操纵(见图左下C)。每个操纵面都通过操纵系统与驾驶舱中的驾驶杆或脚蹬相连.由驾驶员操纵其编转。操纵面偏转的主要作用不是推动整架飞机,而是使其绕飞机的某个轴转动。例如,当驾驶员侧压(向左或向右)驾驶杆时,左右机翼的副翼就会分别向上和向下偏转,从而产生一个绕纵轴的转动力短,左右机器就会相应
1. The airplane’s control ailerons are used for lateral maneuvers that roll around the longitudinal axis of the aircraft (see figure A, left); elevators, pitch controls for pitch movements around the abscissa of the aircraft (see figure B, middle left) ; Rudder, used for yawing around the vertical axis of the aircraft (see chart below C). Each control surface is connected to the cockpit or pedal in the cockpit via a maneuvering system, which is manipulated by the driver. Instead of pushing the entire aircraft, the primary effect of the control surface deflection is to rotate it about an axis of the aircraft. For example, when the driver presses the steering column sideways (leftward or rightward), the ailerons of the left and right wings will deflect upward and downward, respectively, resulting in a short rotational force about the longitudinal axis, and the left and right machines will respond accordingly