| K-8 机襟翼限位机构可靠性建模及求解方法 |
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| 引用本文： | 李立杰,王珉,欧阳祖行,尹明德. K-8 机襟翼限位机构可靠性建模及求解方法[J]. 南京航空航天大学学报, 1998, 0(3) |
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| 作者姓名： | 李立杰 王珉 欧阳祖行 尹明德 |
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| 作者单位： | 南京航空航天大学机电工程学院 |
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| 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。
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| 关 键 词： | 可靠性；多杆机构；数学模型；限位机构；位姿矩阵 |
Establishing and Calculating the Reliability Mathematical Model of K 8 Flap's Spacing Mechanism |
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| Li Lijie Wang Min Ouyang Zuxing Yin Mingde. Establishing and Calculating the Reliability Mathematical Model of K 8 Flap's Spacing Mechanism[J]. Journal of Nanjing University of Aeronautics & Astronautics, 1998, 0(3) |
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| Authors: | Li Lijie Wang Min Ouyang Zuxing Yin Mingde |
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| Abstract: | 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. |
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| Keywords: | reliability multi bar linkages mathematical model spacing mechanism location and gesture matrix |
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