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Environmental Effects on Long Term Displacement Data of Woven Fabric Webbings under Constant Load for Inflatable Structures

机译:充气结构在恒定载荷下对织物网的长期位移数据的环境影响

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An experimental study of the effects of environmental temperature and humidity conditions on long-term creep displacement data of high strength Kevlar and Vectran™ woven fabric webbings under constant load for inflatable structures is presented. The restraint layer of an inflatable structure for long-duration space exploration missions is designed to bear load and consists of an assembly of high strength webbings. Long-term creep displacement data of webbings can be utilized by designers to validate service life parameters of restraint layers of inflatable structures. Five groups of high-strength webbings were researched over a two year period. Each group had a unique webbing length, load rating, applied load, and test period. The five groups consisted of 1.) 6K Vectran webbings loaded to 49% ultimate tensile strength (UTS), 2.) 6K Vectran webbings loaded to 55% UTS, 3.) 12.5K Vectran webbings loaded to 22% UTS, 4.) 6K Kevlar webbings loaded to 40% and 43% UTS, and 5.) 6K Kevlar webbings loaded to 48% UTS. Results show that all webbing groups exhibit the initial two stages of three of a typical creep curve of an elastic material. Results also show that webbings exhibit unique local wave patterns over the duration of the test period. Data indicate that the local pattern is primarily generated by daily variations in relative humidity values within the test facility. Data indicate that after a three to six month period, where webbings reach a steady-state creep condition, an annual sinusoidal displacement pattern is exhibited, primarily due to variations in annual mean temperature values. Data indicates that variations in daily temperature values and annual mean humidity values have limited secondary effects on creep displacement behavior. Results show that webbings in groups 2 and 5 do not exhibit well defined annual displacement patterns because the magnitude of the applied loads cause large deformations, and data indicate that material yielding within a webbing tends to neutralize the annual sinusoidal displacement pattern. Study indicates that applied load, environmental effects, mechanical strength, coefficient of thermal expansion, and hygroscopic properties of webbings are fundamental requirements for quantifying accurate creep displacements and behaviors over multiple year time periods. Results from a study of the environmental effects on long-term creep displacement data of Kevlar and Vectran woven webbings are presented to increase the knowledge base of webbing materials and to enhance designs of inflatable space structures for long-duration space missions.
机译:提出了环境温度和湿度条件对充气结构在恒定载荷下高强度Kevlar和Vectran™机织织物的长期蠕变位移数据的影响的实验研究。用于长期太空探索任务的充气结构的约束层经设计可承受载荷,并由高强度安全带组成。设计人员可以利用织带的长期蠕变位移数据来验证充气结构约束层的使用寿命参数。在两年的时间内研究了五组高强度织带。每组都有唯一的织带长度,额定载荷,施加的载荷和测试时间。这五个组包括1.)加载到49%极限抗拉强度(UTS)的6K Vectran织带,2。)加载到55%的UTS的6K Vectran织带,3。)加载到22%的UTS的12.5K Vectran织带,4。) 6K Kevlar织带负载到40%和43%的UTS,以及5.)6K Kevlar织带负载到48%的UTS。结果表明,所有织带组均表现出弹性材料典型蠕变曲线中的三个的初始两个阶段。结果还表明,织带在测试期间内表现出独特的局部波型。数据表明局部模式主要是由测试设施内相对湿度值的每日变化产生的。数据表明,在三到六个月的安全带达到稳态蠕变状态后,主要由于年平均温度值的变化,出现了年正弦位移模式。数据表明,日温度值和年平均湿度值的变化对蠕变位移行为的次要影响有限。结果表明,第2组和第5组中的安全带没有表现出明确的年度位移模式,因为施加的载荷的大小会引起较大的变形,并且数据表明,安全带内的材料屈服倾向于抵消年度正弦位移模式。研究表明,施加的载荷,环境影响,机械强度,热膨胀系数和织带的吸湿性是量化多年时间内准确的蠕变位移和行为的基本要求。提出了对凯夫拉尔纤维和Vectran编织带的长期蠕变位移数据的环境影响研究的结果,以增加带材料的知识基础并增强用于长期太空任务的充气式空间结构的设计。

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