飞机自动布局设计的几何方面

Михаил Юрьевич Куприков, M. Kuprikov, Л. Маркин, L. Markin
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引用次数: 9

摘要

本文考虑了与高布局密度产品(主要是运输工具)布局自动化相关的问题。它已经证明了飞机的几何形状是如何在基础设施和布局约束的基础上形成的。考虑到放置在其中的单元的质量-惯性特性,已经描述了气动和内部布局对飞机几何形状的影响。提出了布局的逆向问题(当所需的布局空间是飞机几何形状在硬基础设施限制下的初始数据时)。将寻找飞机几何形状合理参数的工程任务作为多准则离散优化任务进行了广义描述。已经证明,这项任务可以被表述为搜索设计参数向量,作为设计和工程解决方案的众多可接受变体。本文描述了一种用于自动布局的物理任务公式,作为室内对象分配的限制系统(要求的方向,相互兼容性,可使用性等)。本文还描述了作为优化问题的自动布局的数学任务公式。由于分配任务是一个经典的几何问题,有必要建立合适的几何模型来求解。研究表明,这一过程的复杂性是由于现代运输,特别是航空航天运输的布局对象的几何形状信息的计算机表示的复杂性。在本文中,它已经表明,在现代应用几何中使用的大量模型,允许描述任何复杂物体的几何形状,并没有为自动布局任务提供任何解决方案。现代软件的可能性也已显示,并证明了不允许在自动布局任务中直接使用它的原因。将布局任务的数学表达式描述为一个优化问题,明确了其目标函数、限制条件和效率准则。已经证明了一种方法(受体方法和标准方程装置),允许在为自动布局创建几何模型时,从布局对象分配的穷举选择到自动分配的智能算法。正如本文所示,分形理论是研究刚体表面几何形状和影响获得表面结构的机理的良好数学工具。
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Geometric Aspects of Aircraft Automated Layout Design
In this paper have been considered questions related to automation of the layout for products with high layout density (primarily means of transport). It has been demonstrated how an aircraft’s geometric shape is formed on the basis of infrastructural and layout constraints. Influences of aerodynamic and internal layouts on the aircraft’s geometric shape have been described, taking into account mass-inertia characteristics of units placed in it. The layout’s reverse problem (when a required layout space is initial data for the aircraft’s geometric shape under hard infrastructure restrictions) has been presented. A project task of finding the rational parameters for the aircraft’s geometric shape as the task of multi-criterion discrete optimization has been described in a generalized form. It has been demonstrated that this task can be formulated as a search for the vector of design parameters as a multitude of admissible variants for design-and-engineering solutions. In the paper has been described a physical task formulation for automated layout as a system of restrictions on objects allocation indoor (required orientation, mutual compatibility, serviceability etc.). Mathematical task formulation for automated layout as the optimization problem has been described too. Since the allocation task is a classical geometric problem, it is necessary to develop appropriate geometric models for its solving. It has been shown that this process’s complexity is due to the complexity related to computer representation of information about geometric shape for layout objects of modern transport, especially the aerospace one. In this paper it has been shown that the abundance of models used in modern applied geometry and allowing describe geometric shapes for objects of any complexity, does not provide any solution for automated layout tasks. Possibilities of modern software have been also shown, and the reasons not allowing its direct use in the tasks of automated layout have been proved. The layout task’s mathematical formulation has been described as an optimization problem, specifying its objective function, limitations and efficiency criteria. Has been justified an approach (receptor methods and apparatus of normal equations) allowing, while creating geometric models for the automated layout, go from exhaustive options for allocation of layout objects to intellectual algorithms for automated allocation As has been shown in the paper, fractal theory is a good mathematical tool for study of rigid bodies’ surface geometry and mechanisms influencing on the obtaining surface structure.
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