基于气囊缓冲的某火箭炮着陆冲击分析

目的减小火箭弹着陆冲击加速度。方法基于LS-DYNA瞬态动力学分析软件和冲击动力学理论,采用有限元软件HYPERMESH建立火箭炮-气囊系统有限元模型,采用显式动力学方法对火箭炮-气囊系统的着陆冲击缓冲过程进行仿真。分析火箭炮在正常着陆工况下,火箭弹的着陆冲击响应,得出空投装备速度、加速度变化曲线,以及气囊的体积、压力曲线。结果在正常着陆工况下,火箭弹横向加速度的最大值为122 m/s2,小于安全的横向加速度;火箭弹纵向加速度的最大值为48.3 m/s2,小于安全的纵向加速度;火箭弹的最大轴向力为2640 N,小于安全闭锁力。结论在火箭炮着陆冲击过程中,气囊缓冲装置吸收了大部分冲击能量,起到了良好的缓冲作用,火箭弹的冲击加速度、闭锁力均在安全范围内。采用显式动力学方法对火箭炮的着陆冲击过程进行分析是可行的。     

THOR dummy chest deflection response in oblique and lateral far-side sled tests

Abstract

Objective: The focus of this study is side impact. Though occupant injury assessment and protection in nearside impacts has received considerable attention and safety standards have been promulgated, field studies show that a majority of far-side occupant injuries are focused on the head and thorax. The 50th percentile male Test Device for Human Occupant Restraint (THOR) has been used in oblique and lateral far-side impact sled tests, and regional body accelerations and forces and moments recorded by load cells have been previously reported. The aim of this study is to evaluate the chestband-based deflection responses from these tests.

Methods: The 3-point belt–restrained 50th percentile male THOR dummy was seated upright in a buck consisting of a rigid flat seat, simulated center console, dashboard, far-side side door structure, and armrest. It was designed to conduct pure lateral and oblique impacts. The center console, dashboard, simulated door structure, and armrest were covered with energy-absorbing materials. A center-mounted airbag was mounted to the right side of the seat. Two 59-gage chestbands were routed on the circumference of the thorax, with the upper and lower chestbands at the level of the third and sixth ribs, respectively, following the rib geometry. Oblique and pure lateral far-side impact tests with and without airbags were conducted at 8.3 m/s. Maximum chest deflections were computed by processing temporal contours using custom software and 3 methods: Procedures paralleling human cadaver studies, using the actual anchor point location and actual alignment of the InfraRed Telescoping Rods for the Assessment of Chest Compression (IR-TRACC) in the dummy on each aspect—that is, right or left,—and using the same anchor location of the internal sensor but determining the location of the peak chest deflection on the contour confined to the aspect of the sensor; these were termed the SD, ID, and TD metrics, respectively.

Results: All deformation contours at the upper and lower thorax levels and associated peak deflections are given for all tests. Briefly, the ID metrics were the lowest in magnitude for both pure lateral and oblique modes, regardless of the presence or absence of an airbag. This was followed by the TD metric, and the SD metric produced the greatest deflections.

Conclusion: The chestbands provide a unique opportunity to compute peak deflections that parallel current IR-TRACC-type deflections and allow computation of peak deflections independent of the initial point of attachment to the rib. The differing locations of the peak deflection vectors along the rib contours for different test conditions suggest that a priori attachment is less effective. Further, varying magnitudes of the differences between ID and TD metrics underscore the difficulty in extrapolating ID outputs under different conditions: Pure lateral versus oblique, airbag presence, and thoracic levels. Deflection measurements should, therefore, not be limited to an instrument that can only track from a fixed point. For improved predictions, these results suggest the need to investigate alternative techniques, such as optical methods to improve chest deflection measurements for far-side occupant injury assessment and mitigation.     

高瓦斯工作面隅角柔性气囊安全封堵研究

为解决高瓦斯工作面隅角封堵工人劳动强度大、效率低,封堵效果不佳易造成隅角瓦斯浓度超限等安全问题,研发设计了矿用阻燃内外胆组合结构的轻型柔性隅角封堵气囊,并相应提出了单体液压支柱配合轻型柔性气囊的隅角封堵新方法。通过实验室测试实验和现场工业性试验表明:选用PVC材料和双抗涂覆布材料的气囊质量小、轻便实用,大幅降低了工人的劳动强度,提高了工作效率,减小了传统封堵方式编织袋装碎煤造成的遗煤浪费;该气囊可适应大变形(变形率可达42.5%)、耐冲击(2×104J的冲击能量不破坏),抗撕扯能力强,且具有阻燃特性,重复使用率高,大大节约了隅角封堵的成本;使用气囊封堵后,采空区内瓦斯浓度显著增大,说明气囊封堵的密闭性增加,安全封堵效果十分明显。     

用于大中型救生气囊释放阀的研制

大中型救生气囊广泛运用于航空、航海救生等领域,它要求启动释放装置后能在很短的时间内将气囊充至规定形状,以满足救生功能,同时又要具有很高的可靠性与安全性,本文主要介绍一种用于大中型救生气囊的快速气体释放阀,并阐述其工作原理及应用。     

循环流化床锅炉掺烧高炉煤气的应用

介绍了高炉煤气的主要燃烧特性,分析了高炉煤气在循环流化床锅炉中掺烧时对炉膛换热、过热蒸汽温度、锅炉负荷、热效率、分离装置以及环境的影响,并提出了消除不良影响的相应措施。     

高位巷瓦斯抽采下采空区自燃危险性数值分析及应用

针对大流量高位巷瓦斯抽采可能诱发采空区自燃问题,以南山矿18层5分段综放面为研究背景,构建采空区气体渗流分析模型。利用变渗透系数和Forchheimer方程,求解非线性流与层流并存下采空区三维氧气分布。结果表明:高位巷瓦斯抽采使工作面氧气更易沿漏风方向采空区纵深发展,氧化带总体宽度会随抽放流量的提高而增加。在进风侧氧气分布后移程度较小,而回风侧受抽放负压显著影响,出现明显氧气富集区。上下隅角封堵配合注氮,会降低抽放对氧气渗入的诱导影响。依据研究结论,利用综合防火措施消除了高位巷附近潜在的自燃危险。     

侧开缝对竖通道内旋转热流场影响的实验研究

为了掌握竖通道两侧开缝对于通道内热流场的影响,在一32cm(长)×32cm(宽)×200cm(高)的竖通道内进行了旋转热流场实验研究,对比了在不同热源条件下,竖通道侧开缝宽度为3.0cm和3.5cm时,侧开缝底部5cm高区域被遮挡前后通道内热流场的变化。实验结果表明,与遮挡前相比,遮挡通道侧开缝底部对火焰燃烧和热流场的运动状态都会产生影响。遮挡通道侧开缝底部区域,会在一定程度上限制外界冷空气进入通道内,从而减弱通道内的火焰旋转程度,致使燃料燃尽的耗时更长,平均火焰高度降低,其影响程度随着燃料池增大而减弱;遮挡侧开缝底部区域后,造成通道内下部区域中心轴线处的温度降低,最大影响区域在50cm高度附近,而在150cm高度以上基本没有影响;平均火焰高度与燃料池直径之比的无量纲量H/Φ与Peclet数之间的比例系数近似为1.732,并且是否遮挡侧开缝底部区域对于两者之间比例关系的影响不大。     

污染源位置对气体污染物影响的数值模拟

在自然通风、置换通风和单侧送侧回式通风3种方式下,通过改变污染源位置,运用CFD软件模拟研究了办公室内苯污染物的浓度分布规律,比较得出最佳通风方式下的最合理污染源位置。结果表明,3种通风方式下污染源放置的最合理位置是点3;苯污染源处于位置3时,3种通风方式中自然通风各平面苯污染物平均浓度普遍相对最高,而单侧送侧回方式的相对最低,置换通风居于二者之间。最终确定单侧送侧回通风方式下污染源处于位置3时为最佳物理模型,在该模型下办公室内通风效果最好,能够有效地排出室内气体污染物。因此,不同污染源位置对办公室内空气品质的影响不同。     

缓释肥侧条施肥技术对水稻产量和氮素利用效率的影响

利用田间小区试验,系统研究了基于缓释肥料的侧条施肥技术对水稻产量和氮素利用效率的影响。试验结果表明：与农民常规施肥处理（FP）比较,侧条施肥技术高缓释肥处理（HF）水稻氮素投入比农民常规施肥处理（FP）降低约40%,水稻产量没有显著降低,穗粒数比农民常规施肥处理增加了8.36%。侧条施肥技术显著提高了水稻地上部吸氮量和氮肥偏生产力,降低了氮素的表观损失量。侧条施肥各处理氮肥偏生产力在39.1～67.8之间,显著高于FP处理的23.7。FP处理氮素表观损失量高达174.2 kg＆#183;hm-2,侧条施肥各处理表观损失量在23.2～61.9 kg＆#183;hm-2之间。综合考虑水稻产量和环境因素,基于缓释肥料的侧条施肥技术是一种资源节约和环境友好的施肥技术。     

厚板件拉深垂直切边模具的设计

采用垂直切边模具，能够保证零件的高度尺寸，不易使零件变形，且适用于不同厚度的零件，故垂直切边模具有较大的通用性。