摘要
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 satisfactory mathematical model of K 8 flap spacing mechanism has been set up by the method provided in this paper, so that the reliability of the mechanism can be calculated. On the basis of it, the method of establishing the mathematical model is also suitable for calculating the reliability of motion of plane multi bar linkages by changing the parameters of the model.
出处
《南京航空航天大学学报》
EI
CAS
CSCD
北大核心
1998年第3期319-325,共7页
Journal of Nanjing University of Aeronautics & Astronautics
关键词
可靠性
多杆机构
数学模型
限位机构
襟翼
reliability
multi bar linkages
mathematical model
spacing mechanism
location and gesture matrix
