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所采用的建模方法比较完满地解决了Ｋ－８机襟翼限位机构（以下简称限位机构）的建模问题，建立了数学模型，以便进行机构的可靠性计算和设计；并在此基础上通过改变模型参数，使该建模方法同样适用于解决平面多杆机构的运动可靠性问题。
The modeling method used to solve the modeling problem of the K-8 flaps limit mechanism (hereinafter referred to as the limit mechanism) is relatively complete, and a mathematical model is established for the reliability calculation and design of the mechanism. Based on the change of the model parameters, the modeling method is also suitable for solving the problem of the motion reliability of the planar multi-bar mechanism.