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AN INVESTIGATION OF TROOP SEAT TESTING METHODOLOGY USING MADYMO MODELS

机译:使用MADYMO模型调查部队座椅测试方法

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Energy-absorbing troop seats can save lives and mitigate injury in many military aircraft mishaps. Several designs are currently in the field and research continues to provide additional improvements. When it comes to evaluating performance, however, troop seats raise some issues that normally do not occur for pilot seats. Pilots have hand and foot controls that dictate the logical position for manikins in laboratory tests. The same cannot be said for troop seats, but positional variations can have significant effects on some test results. The first part of this study uses computer modeling with the Mathematical Dynamic Model (MADYMO) simulation program to examine the sensitivity of test outcome to troop seat occupant position. The vertical component of the lumbar load, a key performance parameter for troop seats, serves as the principal variable in case comparisons. For some types of seat energy absorbers (Eas), it is shown that changes in arm and leg position can produce lumbar load differences which exceed those that might be expected from normal test-to-test variability. These results point to a need for standardization so that tests of a given seat design, as well as tests of differing designs, can be compared directly. The second part of this paper considers an issue that arises in the testing of both troop and pilot seats: the method chosen to deliver the crash impulse. The two most common methods are a drop tower (DT) test and a horizontal accelerator (HA) test. In the latter, the seat is rotated 90o to vertical so that the seat's Z-axis is aligned with the laboratory X-axis. This leads to questions about the influence of gravity on the test results. Once again, MADYMO simulations are employed to study test result sensitivity, and to determine whether gravity compensation is called for in the form of an HA pulse adjustment or a small forward pitch of the HA seat. The results indicate that the compensation required depends on the test configuration and the relative importance of the measurements taken.
机译:能量吸收的部队座椅可以挽救生命和减轻许多军用飞机的伤害。目前在该领域的几种设计,研究继续提供额外的改进。然而,当涉及评估性能时,部队席位会提出一定的问题,通常不会发生用于试点座位。飞行员有手和脚控制,对实验室测试中的Manikins逻辑位置决定了。对于部队座椅,不能说同样的座位,但位置变化可能对一些测试结果产生显着影响。本研究的第一部分使用计算机建模与数学动态模型(MADYMO)仿真程序,以检查测试结果对部队座位占用位置的敏感性。腰部负荷的垂直分量,部队座椅的关键性能参数,是在比较中的主要变量。对于某些类型的座椅能量吸收器(EA),示出了臂和腿部位置的变化可以产生腰部负载差异,这些载荷差异超过正常测试变异性可能预期的那些。这些结果指出了对标准化的需求,以便直接比较给定座椅设计的测试以及不同设计的测试。本文的第二部分考虑了在队伍和飞行员座椅测试中出现的问题:选择碰撞冲击的方法。两个最常见的方法是滴塔(DT)测试和水平加速器(HA)测试。在后者中,座椅旋转90o至垂直,使得座椅的Z轴与实验室X轴对齐。这导致关于重力对测试结果的影响的问题。再次,MADYMO模拟用于研究测试结果灵敏度,并确定是否以HA脉冲调节的形式或HA座位的小向前间距调用重力补偿。结果表明所需的补偿取决于测试配置和测量所采取的测量的相对重要性。

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