... 安定配平状态 stable-trim conditions 飞机配平状态 airplane trim 俯仰配平状态 state of pitch-trim ...
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trim of airplane 飞机配平
Pitch axis - Horizontal or lateral axis, passes through the airplane from one side to the other - nose up and nose down control is by elevators (and stabilizer for trim).
俯仰轴—又称水平轴或横轴。由飞机的一侧通向另一侧。飞机绕此轴转动即造成机首的俯与仰。俯仰控制是由升降舵来达成的,水平安定面则为配平之用。
Horizontal or lateral axis, passes through the airplane from one side to the other - nose up and nose down control is by elevators (and stabilizer for trim).
从飞机一侧通向另一侧的水平轴或横轴。升降舵控制机头绕此轴作上下的运动。(水平安定面则用以配平。)
When the autopilot is disengaged, the control wheels and ailerons move to the (possibly undesired) neutral point and the airplane will roll proportional to the amount of trim input.
一旦自动驾驶被脱开,操纵盘和副翼就移向新的(可能是不需要的)中立点,并且,飞机将与配平输入量成比例地滚转。
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