首页> 外文会议>SAFE Association annual symposium >Whole Body Vibration Exposure for MH-60S Pilots
【24h】

Whole Body Vibration Exposure for MH-60S Pilots

机译:MH-60S飞行员的全身振动暴露

获取原文

摘要

Pilots of the MH-60S helicopter are exposed to continuous whole body vibration (WBV). Pilot fatigue is a growing operational concern due to the increased frequency of extended durations of missions (6-8+hours) in support of Operations Iraqi Freedom and Enduring Freedom. Endurance aspects of the currently used rotary wing seating systems were not optimized for the longer missions and wide range of pilot anthropometric measurements, which is now typical of naval aviation. The current seating systems were designed primarily to meet crashworthiness requirements, not for the wide range of pilot anthropometry or to mitigate WBV. Albeit, an issue, pilot fatigue and reduced mission effectiveness are also critical concerns. Current Hazard Reports (HAZREP) indicated that pain in both pilots' legs and backs begin 2 to 4 hours into the flight and increase with time. Situational awareness also decreases with an increase in flight duration due to the constant distraction of pilots shifting in their seats while trying to get comfortable. Froom (1987) reported a dose-response relationship between the length of military helicopter flights and back discomfort. He also concluded that this pain is typically dull, over the lower back, and its prevalence and intensity are dependent on the total flight hours of exposure. This study evaluated WBV produced in the pilot seating systems onboard the MH-60S. The purpose of the study was to test and compare the effectiveness of three different seat cushions, the current seat cushion versus two anti-vibration seat cushions A and B. The three seat cushions were measured for acceleration levels averaged over five-minute intervals using a triaxial seat pad accelerometer. The recordings were completed for several round-trip straight and level flights. A frequency analysis from 0-80 hertz (Hz) was conducted on all acceleration measurements to determine the dominant axis and frequency of the pilots' vibration exposure. The results were then compared to the applicable Threshold Limit Values (TLVs) established by the American Conference of Governmental Industrial Hygienists (ACGIH) [1] to determine the MH-60S pilots' permissible exposure time for all seat cushions.
机译:MH-60S直升机的飞行员暴露于连续全身振动(WBV)。导频疲劳是由于支撑伊拉克自由和持久自由的延长持续的持续时间(6-8 +时间)的频率增加而越来越多的操作关注。目前使用的旋翼座椅系统的耐力方面对于长长的任务和广泛的试点人体测量测量没有优化,现在是海军航空的典型。目前的座椅系统主要是为了满足耐火性要求,而不是用于广泛的试点人体测量法或减轻WBV。尽管如此,问题,飞行员疲劳和减少的使命效果也是关键问题。目前的危险报告(HAZREP)表明,飞行员的腿和背部的疼痛在飞行中开始2到4个小时,随着时间的推移而增加。由于飞行员在试图舒服的同时,由于飞行员在座位上的不干伤而增加,但情况意识也随着飞行持续时间而减少。上游(1987)报道了军用直升机航班长度与背部不适之间的剂量反应关系。他还得出结论,这种疼痛通常是暗淡的,在腰部上,其流行和强度取决于暴露的总飞行时间。本研究评估了在MH-60S的飞行员座椅系统中产生的WBV。该研究的目的是测试和比较三个不同座垫的有效性,当前座垫与两个抗振座垫A和B。测量三个座垫,用于使用a以上5分钟间隔的加速度水平平均。三轴座椅垫加速度计。录音完成了几次往返直程和水平的航班。在所有加速度测量上进行0-80赫兹(Hz)的频率分析,以确定导频振动曝光的主轴和频率。然后将结果与美国政府工业卫生学家(ACGIH)[1]建立的适用阈值限制值(TLV)进行比较,以确定所有座垫的MH-60S飞行员的允许暴露时间。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号