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TEST RIG FOR FATIGUE TESTS OF SPECIMENS FOR COMBINED AXIAL LOADING AND BENDING

机译:组合轴向载荷和弯曲试样疲劳试验的试验台

摘要

the display u0434u043bu00a0 u0443u0441u0442u0430u043bu043eu0441u0442u043du044bu0445 test samples for joint axial u043du0430u0433u0440u0443u0436u0435u043du0438u0435 and curve. the purpose of u0438u0437u043eu0431u0440u0435u0442u0435u043du0438u00a0 - approximation conditions of testing sample for u0443u0441u043bu043eu0432u0438u00a0u043c exploitation of aircraft structures in the u043du0430u0433u0440u0443u0436u0435u043du0438u0438 axis and from u0433u0438u0431u043du043eu0439 at u0433u0440u0443u0437u043au0430u043cu0438 by u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 u0432u0430u0440u044cu0438u0440u043eu0432u0430u043du0438u00a0 square of different loads.the device u0434u043bu00a0 console u043au0440u0435u043fu043bu0435u043du0438u00a0 sample on the bed is u0448u0430u0440u043du0438u0440u043du043e the body hole, two sides of which u043du0430u043au043bu043eu043du0435u043du044b under one corner to e the axis. there are two in the liner with the counter tilt rods u043fu043eu0432u0435u0440u0445u043du043eu0441u0442u00a0u043cu0438. u0434u0440u0443u0433u0430u00a0 surface of each liner has u043du0430u0441u0435u0447u043au0443 and designed u0434u043bu00a0 u0432u0437u0430u0438u043cu043eu0434u0435u0439u0441u0442u0432u0438u00a0 with the outside end of the sample.liner has a plate, u043au043eu0442u043eu0440u0430u00a0 through lining and elastic gasket cooperates with the external surface of the sample at the station, adjacent to the u043au043eu043du0446u0435u0432u044bu043c with u043fu0440u0438u0436 u0438u043cu043du044bu0445 core elements located in the u043eu0442u0432u0435u0440u0441u0442u0438u00a0u0445 u043fu043bu0430u0441u0442u0438u043d.4 il. (/
机译:显示器 u0434 u043b u00a0 u0443 u0441 u0442 u0430 u043b u043e u0441 u0442 u043d u044b u0445用于关节轴向 u043d u0430 u04330 u0433 u0440 u0443 u0436 u0435 u043d u0438 u0435和曲线。 u0438 u0437 u043e u0431 u0440 u0435 u0442 u0435 u043d u0438 u00a0的目的- u0443 u0441 u043b u043e u043e u0432 u0438 u00a0 u043c的测试样本近似条件 u043d u0430 u0433 u0440 u0443 u0436 u0435 u043d u0438 u0438轴上的飞机结构,并且从 u0433 u0438 u0431 u043d u043d u043e u0439处的飞机结构位于 u0433 u0440 u0443 u0437 u043a u0430 u043c u0438 by u043e u0431 u0435 u0441 u043f u0435 u0447 u0435 u043d u0438 u00a0 u0432 u0430 u0440 u044c u0438 u04438 u0440 u043e u0432 u0430 u043d u0438 u00a0正方形的不同负载。设备 u0434 u043b u00a0控制台 u043a u0440 u0435 u043f u043b u0435 u043d u043d u0438 u00a0床上的样本为 u0448 u0430 u0440 u0440 u043d u0438 u0440 u043d u043e主体孔,其中两个边在轴的一个角下位于 u043d u0430 u043a u043b u043e u043d u0435 u043d u044b。衬管中有两个带有反向倾斜杆 u043f u043e u0432 u0435 u0440 u0445 u043d u043e u0441 u0442 u00a0 u043c u0438。 u0434 u0440 u0443 u0433 u0430 u00a0每个衬里的表面都有 u043d u0430 u0441 u0435 u0447 u043a u0443并设计为 u0434 u043b u00a0 u0432 u0437 u0430 u0438 u043c u043e u0434 u0435 u0439 u0441 u0442 u0432 u0438 u00a0带有样品的外端。衬板有一个衬板,通过衬里和弹性垫圈配合在一起。 u043a u043e u0442 u0432 u043e u0440 u0430样品的外表面在工作站上,与 u043a u043e u043d u0446 u0435 u0432 u044b u043c相邻,并且具有 u043f u0440 u0438 u0436 u0438 u043c u043d u043d u043b u0445位于 u043e u0442 u0432 u0435 u0440 u0441 u0442 u0438 u00a0 u0445 u043f u043b u0430 u0441 u0442 u0438 u043d.4上的元素。 ( /

著录项

  • 公开/公告号SU1758488A1

    专利类型

  • 公开/公告日1992-08-30

    原文格式PDF

  • 申请/专利权人 MO VERTOLETNYJ ZAVOD IM.M.L.MILYA;

    申请/专利号SU19904821147

  • 发明设计人 SHELKOVNIKOV PETR SSU;

    申请日1990-05-03

  • 分类号G01N3/32;

  • 国家 SU

  • 入库时间 2022-08-22 05:26:53

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