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Application of short fiber reinforced composite materials multilevel model for design of ultra-light aerospace structures

机译:短纤维增强复合材料的应用多级模型进行超轻航空结构设计

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A Multilevel approach of modeling the stiffness and strength of ultra-light aerospace structures from short reinforced composite materials is presented. The object of the research is the strength elements of aerospace structures and specifically, the lugs for the transfer of concentrated forces in the gateway of unit places. The material is anisotropic. The properties of this material depend on the organization of the casting process of the plates from which the lugs are cut. The first level of the model is the descriptive model of the casting process of the plate from PEEK material. The casting model of plates is based on the geometry of the gating system and the tool geometry which defines the characteristics of the high-viscosity heat exchange, reinforced during binding with the environment. The preprocessor for the first level of model production is Moldex Designer, with which the geometrical characteristics of the gating system of heat exchange are set. The finite-element mesh for calculation of the hydrodynamic task is constructed. Calculation of casting process of the gate is carried out in Moldex 3D system. The initial data are the finite-element model, the parameters defining the casting mode: temperature, pressure, material volume, and also the parameters of modes of hold pressure and cooling of detail. The orientation of the file of fibers, which is used for the description of the anisotropy of the products considered is the result of casting modeling of the plate. The second level of the model is the model of anisotropic material with the characteristics defined taking the orientation of reinforcing fibers into account, obtained from the results of the casting process in the DIGIMAT system. The possibility of detailing the material characteristics received on the basis of the processing of strength tests of material samples is considered. The third level of model is the finite-element model of the product considering anisotropy of material. The model is constructed in the ANSYS Workbench system. The strength characteristics of the anisotropic material are defined in the model by the DIGIMAT module connected to ANSYS through the material parameter setting DIGIMAT Material. The multilevel model allows calculation of the strain-stress state of products of irregular shape cast from composite materials reinforced by short high-strength fibers. The results of the multilevel model production are verified with field research of the considered products.
机译:提出了一种模拟刚度和超光航空结构的刚度和强度的多级方法。该研究的目的是航空航天结构的强度元素,具体地,凸耳用于在单位位置的网关中传递集中力。该材料是各向异性的。该材料的性质取决于凸耳被切割的板的铸造过程的组织。该模型的第一级是来自PEEK材料板的铸造过程的描述性模型。板的铸造模型基于门控系统的几何形状和刀具几何形状,其定义了高粘度热交换的特性,在与环境结合期间加强。用于第一级模型生产的预处理器是模特设计师,其中设定了热交换的门控系统的几何特性。构建了用于计算流体动力学任务的有限元网。浇口铸造过程的计算在Modex 3D系统中进行。初始数据是有限元模型,参数定义铸造模式:温度,压力,材料体积,以及保持压力模式的参数和细节的冷却。用于描述所考虑的产品的各向异性的纤维文件的方向是板材铸造建模的结果。该模型的第二级是各向异性材料的模型,该特性定义了通过Digimat系统中的铸造过程的结果获得的增强纤维的取向。考虑了详细描述基于材料样品的强度试验的材料特性的可能性。第三级模型是考虑材料各向异性的产品的有限元模型。该模型是在ANSYS Workbench系统中构建的。通过材料参数设定Digimat材料,通过连接到ANSYS的DigiMat模块在模型中定义各向异性材料的强度特性。多级模型允许从高强度纤维增强的复合材料铸造的不规则形状产物的应变应力状态计算。多级模型生产的结果验证了考虑产品的现场研究。

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