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A process architecture for increased parameterization in the solid modeling and design of aircraft wing and empennage structural assemblies and parts

机译:在飞机机翼和尾翼结构组件和零件的实体建模和设计中增加参数化的过程架构

摘要

pA Process Architecture for Increased Parameterization in the Solid Modeling and Design of Aircraft Wing and Empennage structural assemblies and parts. Abstract Design involves human effort, often demanding the incorporation of changes. So this human effort plus the changes result in another considerable effort. But if the Design is represented by a set of parameters then the change merely means changing the values of the parameters. So the proposed method keeps the Design heritage intact and lets the Design intent alone do the talking. In the process, meanwhile, a human element (in the guise of parameters) is lent to an otherwise complex scenario: which can be further utilized in the selection, change and optimization of the system. THE METHODOLOGY The topology is divided into two spaces: Top Design (TD) & Detail Design (DD). Further, there is an identity element (ID) made common to the both. The novelty comes with the idea of a further classification inside the spaces of TD and DD. Three kinds of objects were defined: (1)Elements Xj (which are nothing but the lines and curves in the Sketcher), (2)Relations fj (which are constraints between the x,'s forced by the Designer), and (3)Analysis objects kr (typically objects with full 3-D data). The parameterization is achieved by an implementation of the relation: f(x) = k, ...fj being commutative and associative. This means, the operations on x/s are not dependent on the sequence of their creation, unlike the feature based modeling where the sequence of the features is important. In this way, new x( 's can be added or deleted at any later time, or the fj's values be changed, without any difficulty. This in practical terms means rapid incorporation of design changes. All design decisions are represented by fj's, whereas the kr's are derived from x/s and f/s by the use of features such as extrude, trim, revolve, booleans, etc, without invoking any design decision on the part of the Designer. For example, in the 'extrude' operation the parameters are: 'start-value' and 'end-value'; but here these values are not important and can be put a sufficiently large number (in the feature based modeling, however, these two parameters are usually design driven parameters). Further, the ID file contains relevant kr's from the TD. The ID (the 'node') makes these objects available to the DD files by the use of proper file-structure. In this way the TD drives top-down changes into the DD. Moreover, at the TD or DD level, the presence of all parameters in the Sketcher alone, makes it easy to identify and change the relevant parameters./p
机译:>在飞机机翼和尾翼结构组件和零件的实体建模和设计中增加参数化的过程体系结构。抽象设计涉及人类的努力,通常要求将变更纳入其中。因此,这种人为的努力加上变化导致了另一项相当大的努力。但是,如果设计由一组参数表示,则更改仅意味着更改参数的值。因此,所提出的方法可以保持设计遗产的完整,并让设计意图独自进行讨论。同时,在此过程中,人为因素(以参数的形式)被用于其他复杂的场景:可以在系统的选择,更改和优化中进一步利用。方法论拓扑分为两个空间:顶部设计(TD)和详细设计(DD)。此外,存在两者共同的身份元素(ID)。新颖性在于在TD和DD空间内进行进一步分类的想法。定义了三种对象:(1)元素Xj(除了草绘器中的直线和曲线外),(2)关系fj(它们是设计器强制执行的x之间的约束)和(3 )分析对象kr(通常是具有完整3D数据的对象)。通过以下关系的实现来实现参数化:f(x)=> k,... fj是可交换的和关联的。这意味着,对x / s的操作不依赖于其创建的顺序,这与基于特征的建模不同,在特征建模中,特征的顺序很重要。这样,可以在以后的任何时间添加或删除新的x(,或更改fj的值,没有任何困难。这实际上意味着快速合并设计更改。所有设计决策都由fj表示,而kr是通过使用诸如拉伸,修剪,旋转,布尔值等功能从x / s和f / s推导而来的,而无需设计器方面的任何设计决定,例如,在“拉伸”操作中参数是:“开始值”和“结束值”;但是这里这些值并不重要,可以放足够大的数量(但是在基于特征的建模中,这两个参数通常是设计驱动的参数)。此外,ID文件包含来自TD的相关kr。ID(“节点”)通过使用适当的文件结构使这些对象可用于DD文件,这样TD将自顶向下的更改驱动到DD中。此外,在TD或DD级别,仅草绘器中所有参数的存在都会使易于识别和更改相关参数。

著录项

  • 公开/公告号IN2013CH05275A

    专利类型

  • 公开/公告日2015-05-29

    原文格式PDF

  • 申请/专利权人 HINDUSTAN AERONAUTICS LTD;

    申请/专利号IN2013CHE5275

  • 发明设计人 AMIT KUMAR PANDEY;GURURAJ B KULKARNI;

    申请日2013-11-18

  • 分类号B64C3;

  • 国家 IN

  • 入库时间 2022-08-21 15:14:10

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