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高性能热塑性复合材料具有高韧性、优异的抗冲击损伤性能及较佳的抗疲劳性能,特别适用于以起落架、尾段、桨毂中央件及传动轴等为代表的直升机高损伤阻抗、高抗疲劳及弹击损伤容限设计需求特定结构部位。高性能热塑性复合材料在国外直升机上的应用正从实现关键层板结构部位全面应用拓展至复合材料夹层结构部位,并大量采用原位自动纤维铺放(automated fiber placement,AFP)等自动化、低成本制造技术和虚拟实验等低成本验证技术,受限于国产热塑性复合材料技术成熟度较低和新研复合材料体系传统积木式方法应用验证的高昂成本及漫长周期,国内直升机热塑性复合材料应用尚处于起步阶段,未来需要重点解决国产热塑性复合材料的性能稳定性及一致性以及在此基础之上的低成本自动化制造工艺、配套低密度耐高温芯材及高效率高置信度虚拟认证技术。 相似文献
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张富官%安鲁陵%李汝鹏 《宇航材料工艺》2008,38(6)
文摘实现复合材料构件成型工装的快速设计对缩短生产准备时间、提高构件质量具有重要意义。本文分析了复合材料构件成型模具的结构和建模特点及要求,提取了结构各部分的设计参数;基于CATIA和CAA平台开发了复合材料构件成型模具设计系统,并应用于飞机复合材料构件的成型模具设计中,验证了本文方法的可行性。 相似文献
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陈挺张迎春谭永刚庄洪兴 《民用飞机设计与研究》2014,(3):39-43
高性能复合材料已经大量应用于民用运输飞机结构,并以飞机主制造商协同供应商的方式进行复合材料飞机结构的制造。介绍了航空器适航审定对复合材料结构制造的适航要求,引出了复合材料结构制造工艺变化的等效性验证方法。目前,复合材料结构制造工艺变化的等效性验证是通过所制造复合材料物理的、化学和基本力学的性能试验,并对试验结果进行统计分析来实现的。最后提供了等效性验证的接受准则。所述内容,对国内民用飞机复合材料结构在不同供应商处制造以及制造过程中工艺变化如何满足航空器适航审定要求提供借鉴;对其它行业复合材料结构制造的质量控制也有借鉴意义。 相似文献
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考虑复合材料蒙皮稳定性的飞机翼面结构布局优化设计 总被引:3,自引:1,他引:2
复合材料蒙皮稳定性是飞机翼面结构设计需要考虑的重要方面。由于翼面结构稳定性理论分析的复杂性,工程中,通常采用与理论分析相比拟的简化方法、使用简便可靠的经验公式在设计过程中进行稳定性校核。多墙式结构是当前翼面结构中普遍采用的结构形式,墙的布局和蒙皮的厚度对复合材料蒙皮的临界屈曲载荷有着重要影响。因此,针对多墙式翼面结构,以工程经验公式为基础,以蒙皮单位长度上的的重量为优化目标,以墙的布局参数和蒙皮厚度为设计变量,以临界失稳载荷为约束,建立了一种考虑复合材料蒙皮稳定性的翼面结构布局优化问题的数学模型,导出了目标函数敏度计算的解析式,并提出了优化问题的求解方法。以翼盒结构为例,验证了该方法的有效性。 相似文献
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针对复合材料泡沫夹芯结构在维修结构性能研究方面的缺失,在完成了复合材料泡沫夹芯板的维修与压缩性能测试之后,建立了结构有限元分析模型,结合夹芯结构的稳定性理论解析模型,并对复合材料泡沫夹芯结构的胶接修理压缩性能进行验证。结果表明:通过试验结果简化了有限元分析模型中的胶层设置;应用复合材料夹芯结构的稳定性理论解析模型,能够快速获得复合材料夹芯维修结构的侧压极限载荷上限值;复合材料泡沫夹芯修理结构的主要侧压破坏模式为面板一阶与二阶屈曲失效,该结果说明复合材料泡沫夹芯修补结构的有限元模型与解析稳定性理论模型的计算精度较高,具有较强的工程实用性。 相似文献
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研究了ICP-AES法测定纯铜中的Bi,Sb,As,Fe,Ni,Pb,Sn,Zn和Ag等9个元素的分析方法.进行了基体元素铜对9个分析元素的光谱干扰研究,选择了合适的分析谱线,同时测定了分析方法的检出限. 相似文献
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Dale P. Cruikshank 《Space Science Reviews》2005,116(1-2):421-439
The diverse populations of icy bodies of the outer Solar System (OSS) give critical information on the composition and structure
of the solar nebula and the early phases of planet formation. The two principal repositories of icy bodies are the Kuiper
belt or disk, and the Oort Cloud, both of which are the source regions of the comets. Nearly 1000 individual Kuiper belt objects
have been discovered; their dynamical distribution is a clue to the early outward migration and gravitational scattering power
of Neptune. Pluto is perhaps the largest Kuiper belt object. Pluto is distinguished by its large satellite, a variable atmosphere,
and a surface composed of several ices and probable organic solid materials that give it color. Triton is probably a former
member of the Kuiper belt population, suggested by its retrograde orbit as a satellite of Neptune. Like Pluto, Triton has
a variable atmosphere, compositionally diverse icy surface, and an organic atmospheric haze. Centaur objects appear to come
from the Kuiper belt and occupy temporary orbits in the planetary zone; the compositional similarity of one well studied Centaur
(5145 Pholus) to comets is notable. New discoveries continue apace, as observational surveys reveal new objects and refined
observing techniques yield more physical information about specific bodies. 相似文献
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Ion optics are crucial components of ion thrusters and the study of the different ion extraction solutions used since the beginning of the electric propulsion era is essential to understand the evolution of ion engines. This work describes ion engine grids' main functions, parameters and issues related to thermal expansion and sputter erosion, and then introduces a review of ion optics used for significant launched and tested ion thrusters since 1970. Configurations, geometries, materials and fabrication methods are analyzed to understand when typical ion thrusters use two or three grids, what are the thicknesses and aperture sizes of the screen, accelerator and decelerator grids, why molybdenum and carbon-based materials such as pyrolytic graphite and carbon–carbon are the best available options for ion optics and what is the manufacturing method for each material. 相似文献
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A survey of current knowledge about Jupiter, Saturn, Uranus, Neptune, Pluto, and their satellites is presented. The best available
numerical values are given for physical parameters, including orbital and body properties, atmospheric composition and structure,
and photometric parameters. The more acceptable current theories of these bodies are outlined with thorough referencing offering
access to the details. The survey attempts to cover the literature through May 1, 1972.
Prepared Under Contract No. NAS7-100 National Aeronautics and Space Administration. 相似文献
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杰罗姆·格瑞·钱德勒 《航空维修与工程》2004,(6):11-14
大到整个飞机机身,小到某个飞机附件,周转时间都是十分重要的。在成本、质量和速度的三角关系中,后者正在占据越来越重要的地位。现在航空业出现一种新趋势,即航空公司在寻找维修公司时更注重维修周转时间的长短,以前,却是更为注重维修价格的高低。随着飞机营运费用的升高,周转 相似文献
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一直以来,航空公司大多采用ACARS通信系统(飞机通信寻址和报告系统)进行空中通信服务.但与陆地通信系统相比,该系统的传输速度慢而且成本高,成为目前影响飞行数据传输速度的重要因素之一.一些MRO软件供应商已开始开发机载无线通信系统,试图改善以往缓慢、昂贵和复杂的空中无线服务,使飞行中生成的重要维修数据以更低的成本、更快的速度和更高效率实现传输. 相似文献
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N.U. Crooker J.T. Gosling V. Bothmer R.J. Forsyth P.R. Gazis A. Hewish T.S. Horbury D.S. Intriligator J.R. Jokipii J. Kóta A.J. Lazarus M.A. Lee E. Lucek E. Marsch A. Posner I.G. Richardson E.C. Roelof J.M. Schmidt G.L. Siscoe B.T. Tsurutani R.F. Wimmer-Schweingruber 《Space Science Reviews》1999,89(1-2):179-220
Corotating interaction regions (CIRs) in the middle heliosphere have distinct morphological features and associated patterns
of turbulence and energetic particles. This report summarizes current understanding of those features and patterns, discusses
how they can vary from case to case and with distance from the Sun and possible causes of those variations, presents an analytical
model of the morphological features found in earlier qualitative models and numerical simulations, and identifies aspects
of the features and patterns that have yet to be resolved.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献