首页> 外国专利> GEOMETRIC FORMS OF COMPOSITE SAMPLES, FACILITATING THEIR DESTRUCTION IN AREA UNDER STUDY IN FATIGUE TESTS

GEOMETRIC FORMS OF COMPOSITE SAMPLES, FACILITATING THEIR DESTRUCTION IN AREA UNDER STUDY IN FATIGUE TESTS

机译:疲劳试验研究中复合样品的几何形式,有助于其在区域内的破坏

摘要

FIELD: testing equipment.;SUBSTANCE: pre-fabricated structure of the test piece (10) comprises of a plurality of layers, made of a fiber-reinforced polymer material, co-forming a laminated material of constant thickness. The laminated material has a geometry including the first and second trapezoidal portions (16, 18) connected through the area under study, in which said sample has a minimum width. The first trapezoidal part, the second trapezoidal part and the area under study form the corresponding parts of the front surface and the corresponding parts of the rear surface of the test specimen. Each of the front and rear surfaces has a profile with a shape similar to a "bow-tie" shape and is made parallel to the specified layers. The first and second projections, glued to the first trapezoidal part on the respective first portions of the front and rear surfaces. The third and fourth protrusions, glued to the second trapezoidal part on the respective second portions of the front and rear surfaces. Each of the first, second, third and fourth protrusions is made of a fiber-reinforced polymer material and has a trapezoidal profile. The test specimen has a minimum width in the test area (20) and a constant thickness. The first trapezoidal part (16) has the first and second rectilinear bevelled sides (12a and 12b). The second trapezoidal part (18) has the third and fourth rectilinear bevelled sides (12c and 12d). The area under study (20) comprises of the first and second radial sides (14a and 14b). The first radial side (14A) is connected to the first and third rectilinear bevelled sides (12a and 12 c), and the second radial side (14b) is connected with the second and fourth rectilinear bevelled sides (12b and 12d). The height of said first radial portion does not exceed 3% of said height of the test specimen (10).;EFFECT: guaranteed destruction in the area under study in fatigue tests.;6 cl, 7 dwg
机译:技术领域:测试设备;物质:试件(10)的预制结构包括由纤维增强的聚合物材料制成的多层,共同形成恒定厚度的层压材料。层压材料具有包括通过研究区域连接的第一和第二梯形部分(16、18)的几何形状,其中所述样品具有最小宽度。第一梯形部分,第二梯形部分和研究区域形成试样的前表面的相应部分和后表面的相应部分。每个前表面和后表面均具有类似于“领结”形状的轮廓,并且使其平行于指定层。在前表面和后表面的相应的第一部分上粘接到第一梯形部分的第一和第二突起。第三和第四突起在前表面和后表面的相应第二部分上胶粘到第二梯形部分。第一,第二,第三和第四突起中的每一个都由纤维增强的聚合物材料制成并且具有梯形轮廓。测试样品在测试区域(20)的最小宽度和恒定的厚度。第一梯形部分(16)具有第一和第二直线斜面(12a和12b)。第二梯形部分(18)具有第三和第四直线斜面(12c和12d)。研究区域(20)包括第一和第二径向侧面(14a和14b)。第一径向侧面(14A)连接到第一和第三直线斜面(12a和12c),第二径向侧面(14b)连接到第二和第四直线斜面(12b和12d)。所述第一径向部分的高度不超过所述试样(10)的所述高度的3%。效果:在疲劳测试中保证研究区域内的破坏; 6cl,7dwg

著录项

  • 公开/公告号RU2640776C2

    专利类型

  • 公开/公告日2018-01-11

    原文格式PDF

  • 申请/专利权人 ZE BOING KOMPANI;

    申请/专利号RU20140104698

  • 申请日2014-02-11

  • 分类号G01N3/02;G01N3/32;

  • 国家 RU

  • 入库时间 2022-08-21 12:35:53

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