最后，针对某型飞机升降舵操纵机构进行了应用研究。

At last, the software scheme of the mechanism reliability simulation is defined, and a case of an elevator control mechanism is presented.

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升降舵，铰连在水平安定面后缘上的可动部件。用以操纵飞机的俯仰运动(机头朝上及朝下)。

ELEVATOR, a hinged moveable part on the trailing edge of the horizontal stabilizer for airplane pitch (nose up and nose down) control.

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飞机尾部的水平稳定器和升降舵。

The horizontal stabilizer and elevator in the tail assembly of an aircraft.

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