Hearon B F, Brinkley J W, Raddin J H
Aviat Space Environ Med. 1983 Nov;54(11):977-87.
An experiment to assess the influence of changes in restraint harness configuration, fore-aft headrest position, and upper extremity bracing technique on human response to impact was conducted using the AFAMRL Vertical Deceleration Tower. A total of 201 tests was performed with volunteer subjects in 11 test conditions to evaluate 3 restraint harnesses, 3 arm bracing conditions, and 4 seat adjustment configurations. The test fixture, restraint harness, and subject were instrumented to obtain pertinent objective data during each experiment. Measured parameters included acceleration of the impact carriage and test seat, velocity of the carriage, loads reacted at the seat, loads measured at the restraint harness attachment points, triaxial translational accelerations at the head and chest of the subject, and body segment displacements. The mean peak carriage acceleration for the 161 experimental level tests was 10.5 G (S.D. = 0.18) and the mean carriage velocity change was 7.89 m/s (S.D. = 0.05). Resultant head and chest accelerations were increased in a proposed, modified F/FB-111 restraint system compared to the operational F/FB-111 restraint system. These findings contributed to the decision not to implement the proposed modification. Also, the arms crossed bracing position for F/FB-111 ejectees preparing for landing impact of the crew module was associated with higher seat loads than the arms extended position. With the arms extended and braced on the anterior thighs or knees, loads are transmitted through the extremities to the footrest thereby reducing loading of the vertebral column. Operational use of the arms extended position prior to anticipated vertical impact accelerations may be helpful in reducing the vertebral fracture rate associated with these mechanical force environments.
利用空军航空医学研究实验室垂直减速塔开展了一项实验,以评估约束带配置变化、头枕前后位置以及上肢支撑技术对人体撞击响应的影响。在11种测试条件下,对志愿者受试者进行了总共201次测试,以评估3种约束带、3种手臂支撑条件和4种座椅调整配置。在每次实验过程中,对测试夹具、约束带和受试者进行了仪器安装,以获取相关的客观数据。测量参数包括冲击滑架和测试座椅的加速度、滑架速度、座椅处的反作用力、约束带连接点处测得的力、受试者头部和胸部的三轴平移加速度以及身体各部位的位移。161次实验级测试的平均峰值滑架加速度为10.5G(标准差=0.18),平均滑架速度变化为7.89m/s(标准差=0.05)。与现役F/FB - 111约束系统相比,在一种改进的F/FB - 111约束系统中,头部和胸部的合成加速度有所增加。这些发现促使做出不实施该改进方案的决定。此外,对于准备承受乘员舱着陆冲击的F/FB - 111弹射者来说,双臂交叉支撑姿势比双臂伸展姿势产生的座椅负荷更高。当双臂伸展并支撑在前大腿或膝盖上时,力会通过四肢传递到脚凳,从而减轻脊柱的负荷。在预期垂直冲击加速度之前使用双臂伸展姿势可能有助于降低与这些机械力环境相关的脊椎骨折发生率。