结构载荷 meaning in Chinese
structural load
Examples
- For smaller vehicles with high acceleration the wind may be little concern with structural loads .
对于具有高加速度的小型飞行器，风与结构载荷的关系可能不大。 - The tested results showed that the collecting ring could be used for the dynamic stress test successfully and the experimental data would be used for determining load spectrum and analyzing fatigue life of spoke plate
结果表明，动态测试过程稳定，所设计和制造的集流环完全满足试验要求，测试数据可以用于结构载荷谱的编制和疲劳寿命分析。 - Taking into account of the structure distortion , the theory and method of load calculation is researched from the perspective of engineering and airworthiness in this paper . the presented theory and method of load calculation is suitable for all kinds of civil aircraft . the load conditions and the initial parameters appropriated to the load calculation are determined according to the requirement of airworthiness
本文从工程应用和适航性角度出发，对民用飞机结构载荷计算的理论与方法做了详细的研究，研究了考虑结构变形的载荷计算方法，按照适航要求确定了飞机各部件载荷计算的设计情况和原始参数。 - Firstly , itis explained that the application research of smart layer . to laod detecting and simulative damage for the model of wing - box , fbg fiber smart layer and pzt smart layer are designed , and manufactured . so , those are surface - mounted respectively on the stiffened skin of aluminum alloy and carbon fiber reinforced . data acquisition system based on different signal processing technique are designed
针对机翼盒段试件结构载荷识别和模拟损伤监测的功能要求,结合智能夹层的设计制作工艺,设计制作了基于fbg传感器的光纤和压电两种智能夹层,并分别安装在机翼盒段试件上的铝合金和碳纤维制蒙皮上。 - Because of above demands , the program of simulation of response of the impact load is generated by fepg , deeply analysis to the program shows the meanings of parameters , function of subroutines and interface files , and compared with the result of experimentation , which indicate the difference is small enough , so can generate the computing source program of the grid structure . as the beginning research of the load identification , this thesis discusses the recognisation of cantilever beam by ga , and the result is well , but the program is limit by number of the parameters . finally show the path of accuracy improvement
基于上述要求,本文利用fepg对格栅结构在冲击载荷作用下的响应进行了数值模拟,生成了计算源程序,并对源程序做了详细而细致的分析,对内部各程序中的变量含义、子程序功能和文件接口做了详细说明,并将模拟结果与实验结果作了比较,结果表明, fepg在格栅结构的计算结果与实验结果相差较少,可以用来生成计算源程序,为下一步的格栅结构载荷重构研究提供参考。