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Comparing Fixed-Base and Shaker Table Model Correlation Methods Using Jim Beam

机译:使用JIM梁比较固定基础和振动台模型相关方法

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The key to any dynamic model correlation is an understanding of how the boundary conditions of the test article interact with the test data. Due to budget and schedule constraints, some spacecraft programs opt to correlate the spacecraft dynamic model during the Environmental Qualification Test, conducted on a large shaker table. While this saves cost to the spacecraft program, the base-drive analysis of the dynamic model incorrectly assumes the boundary condition between the shaker and the spacecraft to be completely fixed, except for the prescribed force input. This paper follows-up research published in IMAC 36, "Comparing Free-Free and Shaker Table Model Correlation Methods using Jim Beam." In that study a free-free impact modal test, a "fixed" base impact modal test on top of the shaker, and a base-drive vibration test were used to assess Finite Element Model (FEM) correlation using different boundary conditions. The NAVCON Jim Beam, a simple and well characterized structure featured in the round robin tests of IMAC 27, was chosen as the test article. Conclusions showed that due to the non-linear compliance of the shaker table, most time would be spent accounting for the boundary condition in the correlation, rather than correlating the test article itself. Previous testing was conducted with the Jim Beam flush mounted to the shaker table, which restricted the motion of the bending and shear modes. To mitigate this constraint, this paper included the use of "donut" force gauges inserted between the shaker table and the Jim Beam. Not only was the direct force input of the vibration test measured, but the gauges acted as spacers which relieved the constraint on mode shapes caused by contact with the shaker table. This constraint was a source of error in the previous modal data. The premise of this follow-on study is the same as before; to compare test data of the same structure with identical instrumentation across different boundary conditions. First, a fixed base modal impact test of the Jim Beam was conducted on a slip table to approximate a modal plate. During this test the Jim Beam was mounted on four disconnected force gauges to simulate the same bolted interface as the shaker table. Second, the Jim Beam was transferred to a large shaker table and a vibration test was conducted. Results of the two tests were compared to investigate the validity of using environmental test data alone to correlate a dynamic model.
机译:任何动态模型相关的关键是了解测试文章的边界条件如何与测试数据交互。由于预算和安排限制,一些航天器计划选择在大型振动筛表中进行环境资格测试期间的航天器动态模型。虽然这节省了航天器计划,但动态模型的基本驱动分析错误地假设振动器和航天器之间的边界条件完全固定,除了规定的力输入。本文在IMAC 36发布的研究后续研究,“使用Jim Beam比较自由和振动筛表模型相关方法。”在该研究中,可以使用自由影响模态测试,在振动器顶部的“固定”基础冲击模态测试,以及使用不同边界条件评估有限元模型(FEM)相关性的基础驱动振动试验。 IMAC 27的循环罗宾测试中的简单且特征在于IMAC 27的循环试验中的简单且良好的结构结构。结论表明,由于振动筛表的非线性顺应性,大多数时间都将花费占相关性的边界条件,而不是将测试物品本身相关联。先前的测试用安装在振动台的吉姆梁冲洗,限制了弯曲和剪切模式的运动。为了减轻这种约束,本文包括使用插入振动台和吉姆梁之间的“甜甜圈”力量仪。不仅测量了振动试验的直接力输入,而且仪表用作垫片,该间隔物可缓解由与振动台接触引起的模式形状的约束。此约束是前一个模态数据中的错误源。这种后续研究的前提是与以前相同的;将相同结构的测试数据与不同边界条件的相同仪器进行比较。首先,在滑动台上进行吉姆梁的固定基础模态冲击试验,以近似模态板。在此测试期间,Jim梁安装在四个断开的力量表上,以模拟与振动台相同的螺栓接口。其次,将Jim梁转移到大振荡器台,并进行振动试验。比较两种测试的结果,以研究单独使用环境测试数据的有效性来关联动态模型。

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