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METHOD OF CREATING STRUCTURE ANALYSIS MODEL OF WING AND STRUCTURE ANALYZING METHOD AND APPARATUS

机译:机翼创建结构分析模型的方法及结构分析方法和装置

摘要

PROBLEM TO BE SOLVED: To create a three-dimensional structure analysis model of an actual wing by dividing a line passing measuring points between the front and rear edges of each measuring section into a fixed number of segments, and extending lines passing corresponding division points of each measuring section to defined planes. ;SOLUTION: About a plurality of measuring sections of an actual wing, the positions of a plurality of measuring points are acquired as measuring data, defined sections are set to the end and socket of the wing, and the front and rear end edge of the winding are detected each measuring section, based on the measuring data. About each measuring section, the line passing the measuring points between the front and rear end edges is divided into a fixed number of segments to create division points, and a line passing corresponding division points of each measuring section is extended to each defined plane to create a three-dimensional structure analysis model of the actual wing. This enables the direct structure analysis of the wing and allows the omission of the performance test in the design/development of a wing.;COPYRIGHT: (C)1999,JPO
机译:要解决的问题:通过将通过每个测量部分前后边缘之间的测量点的线划分为固定数量的线段,并通过通过相应测量点的分割线的扩展线,来创建实际机翼的三维结构分析模型每个测量部分都定义了平面。 ;解决方案:关于实际机翼的多个测量区域,获取多个测量点的位置作为测量数据,将定义的区域设置到机翼的末端和承窝,以及机翼的前后边缘根据测量数据在每个测量部分检测绕组。关于每个测量段,将通过前后端点边缘之间的测量点的线划分为固定数量的线段以创建分割点,并且将通过每个测量段的相应分割点的线延伸到每个定义的平面以创建实际机翼的三维结构分析模型。这样就可以对机翼进行直接的结构分析,并且可以省略机翼设计/开发过程中的性能测试。;版权所有:(C)1999,JPO

著录项

  • 公开/公告号JPH11281328A

    专利类型

  • 公开/公告日1999-10-15

    原文格式PDF

  • 申请/专利权人 ISHIKAWAJIMA HARIMA HEAVY IND CO LTD;

    申请/专利号JP19980079899

  • 发明设计人 EHATA KOREICHI;

    申请日1998-03-26

  • 分类号G01B11/03;F01D5/14;G01B11/24;

  • 国家 JP

  • 入库时间 2022-08-22 02:38:01

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