Chinese translation for "复合材料机匣"

composite casing

Related Translations:

整套复合材料:  whole series of bonded materials

先进复合材料:  acm advanced composite materials

复合材料基体:  matrices of composite material

复合材料直升机:  helicopter; composite

取向复合材料:  aligned composite materialoriented composite material

复合材料试样:  composite test specimen

高级复合材料:  advanced composite materials (acm)advanced composites

复合材料力学:  compound material mechanicsmechanics of complex materialsmechanics of composite materialsmechanics of composites

纳米复合材料:  nano composite materialsnanocomposite

混合复合材料:  hybrid composite

Example Sentences:

	1.	3 , analyzing the stress field of the aero - engine case under the given loads , the fatigue life of the case is predicted through the presented fatigue model and the method of " nominal stress " 用该模型对孔径为5mm层合板的s ? n曲线进行疲劳寿命预测及试验验证。 3 、首次对某型发动机t300 kh - 304复合材料机匣的主铺层在给定工况下的疲劳寿命进行预测。
	2.	4 , using the finite element method , the buckling of the case is studied under the loads including the axial force torsion and pressure . the results will be benefit for aero - engine design in the future . the buckling characteristics of the two new kinds of composite ( t300 / kh - 304 and t300 / bmp - 316 ) is studied under the same boundary conditions sizes and plies , the anti - buckling ability of t300 / kh - 304 composite laminate is better than that of t300 / bmp - 316 composite plates 4 、首次用有限元法和圆柱壳体耦合理论分析了t300 bmp - 316复合材料机匣分别在轴向力、扭矩和内压等单独作用以及耦合作用下的屈曲特性，为进一步研究打下了基础；运用有限元法分析了t300 kh - 304和t300 bmp - 316两种复合材料层合板的屈曲特性，讨论了铺层方式、尺寸、位移边界条件等参数对屈曲特性的影响。
	3.	Composite laminate shells have been applied more and more widely in aerospace structures . in order to increase thrust to weight ratio and improve the comprehensive performance of airplane , optimization design must be carried out . this thesis brings forward utilizing the method of aga - fem , which combines adaptive genetic algorithm ( aga ) and finite element method ( fem ) , to optimize fibre - reinforced composite shells 本文提出采用自适应遗传算法( adaptivegeneticalgorithm )和有限元方法( finiteelementmethod , fem )结合即aga - fem方法进行纤维增强型复合材料层合壳结构的优化设计，并对某航空发动机复合材料机匣进行优化设计分析，取得了很好的效果。

Similar Words：

"复合材料发动机机匣" Chinese translation, "复合材料分类" Chinese translation, "复合材料风管" Chinese translation, "复合材料隔热层" Chinese translation, "复合材料基体" Chinese translation, "复合材料集装箱" Chinese translation, "复合材料结构" Chinese translation, "复合材料结构力学" Chinese translation, "复合材料绝缘系统" Chinese translation, "复合材料力学" Chinese translation