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在飞机生产和飞机大修过程中,经常遇到飞机上连接孔的超差问题需要处理.这些:孔主要指飞机机体结构重要接头机械连接紧固孔,如机翼、机身连接接头孔,垂直安定面与机身连接接头孔,舵面与安定面连接接头孔,起落架转轴接头孔,操纵摇臂连接拉杆孔等. 相似文献
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通过SiC颗粒增强Al基复合材料与Al合金的焊接工艺试验研究,重点分析了材料组合,保湿工艺,连接时间等工艺参数对连接接头性能的影响以及连接接头的微观组织及成分分布,研究表明,TLP扩散连接是一种适用于复合材料连接的重要方法,在相同工艺条件下,LF6/SiCp-6061Al的接头性能明显优于LF6/SiCp-2024Al,连接时间过短或过长,都将影响到接头性能,并且连接时间对不同材料组合的影响也不同,采用二次保温工艺可以较大幅度地提高接头性能。 相似文献
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自冲铆接技术作为新型连接技术,在薄板材料的连接中具有优异的连接性能。其接头质量受连接的可行性和连接参数的影响,而接头质量主要由接头的力学性能来表征,因此接头的质量和力学性能已成为目前自冲铆技术的主要研究方向。随着数值模拟技术的发展,它在自冲铆连接技术上的应用成为一种研究趋势。对近年来自冲铆数值模拟技术的发展进行系统阐述,从自冲铆接头成形质量的数值模拟技术出发,对自冲铆数值模型建立、自冲铆影响因素研究、数值模型优化和数值预测模型4个方面进行说明,综述了材料连接的可行性和连接参数对接头性能的影响,对接头力学性能进行模拟,并对接头力学强度和疲劳寿命进行预测,为自冲铆工艺的研究和发展提供新的方向。 相似文献
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介绍了3种机身侧挂架接头的结构设计方案,即盒梁形式、交点框形式以及盒梁和框综合形式。论述了侧挂架接头的6种连接形式,通过分析对比,认为交点框传力形式和机身内锥体斜挂式挂架接头连接方案为最佳设计方案。 相似文献
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邹贵生%杨俊%吴爱萍%巫世杰%顾兆旃 《宇航材料工艺》2002,32(6):1-5,13
为降低陶瓷与陶瓷或金属的连接温度,目前采用的连接方法有过渡液相扩散连接、兰固态连接、机械连接、粘接、铟封和陶瓷表面低温改性后低温钎焊等。本文从上述连接方法的原理设计、连接材料设计与制备、接头性能及各自的优缺点等方面综述了陶瓷与陶瓷或金属低温连接研究的现状。 相似文献
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吴昌忠%陈静%陈怀宁%林泉洪 《宇航材料工艺》2005,35(3):17-20,30
综述了钛及钛合金高温钎焊结构在现代工业中的应用。在分析了钛基钎料应用和发展的基础上,重点分析了钎焊接头的组织与接头性能的关系以及影响因素。指明接头组织中脆性金属间化合物相的存在形态是决定接头性能的主要因素,接头间隙和钎焊时间决定了接头的组织形态,从而影响接头的性能。钛及钛合金高温钎焊接头的拉伸性能、高温性能和疲劳性能是优越的,而接头氧化后的性能急剧下降。并展望了钛基材料连接的发展方向。 相似文献
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为揭示连接孔垂直度误差对航空复合材料连接性能的影响规律,对准各向同性碳纤维环氧树脂复合材料板进行了单钉单剪试验研究。以极限承载强度、弦刚度、2%偏移承载强度为指标研究连接孔的倾斜角度、倾斜方向以及螺栓扭矩对接头承载性能的影响规律。试验结果表明:当连接孔倾斜角度从0°增加到4°时,接头弦刚度增大10%~40%,极限承载强度下降9%~12%;连接孔倾斜方向对极限承载强度影响甚微,却可使接头弦刚度产生20%~30%的变化;增加螺栓扭矩可以有效提高极限承载强度,但对接头刚度无明显影响;连接孔倾斜角度越大,则螺栓扭矩的增大对2%偏移承载强度的强化效果越不明显。 相似文献
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基于飞机油箱模型形状特征油量测量切片步长选择方法研究 总被引:1,自引:0,他引:1
在分析飞机数字式油量测量过程中目前广泛使用的切片法油量测量原理的基础上,针对现有的定步长切片法无法得到准确、可靠的燃油质量特性数据库的缺陷,结合对飞机油箱模型形状特征的分析,提出了基于飞机油箱模型形状特征的油量测量切片步长选择方法。此方法包括切片步长整体和局部选择两个过程,整体选择以实现相邻两切片平面所夹油箱模型体积近似相等为目的来确定切片步长,以体现油箱模型截面整体变化规律;局部选择以设计切片平面与截面突变平面重合或尽可能接近的方式,突出油箱截面的局部变化特征。实验结果表明:该切片步长选择方法较定步长方法能够建立更为合理、可靠的燃油质量特性数据库,从而提高了油量测量精度。 相似文献
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The effect of inlet conditions on the flow and heat transfer in multiple rotating cavity with axial throughflow 总被引:1,自引:0,他引:1
This paper discusses experimental results from two different build configurations of a heated multiple rotating cavity test rig.Measurements of heat transfer from the discs and tangential velocities are presented.The test rig is a 70% full scale version of a high pressure compressor stack of an axial gas turbine engine.Of particular interest are the internal cylindrical cavities formed by adjacent discs and the interaction of these with a central axial throughflow of cooling air.Tests were carried out for a range of non-dimensional parameters representative of high pressure compressor internal air system flows(Re up to 5×106 and Rez up to 2×105).Two different builds have been tested.The most significant difference between these two build configurations is the size of the annular gap between the(non-rotating) drive shaft and the bores of the discs.The heat transfer data were obtained from thermocouple measurements of surface temperature and a conduction solution method.The velocity measurements were made using a two component,LDA system.The heat transfer results from the discs show differences between the two builds.This is attributed to the wider annular gap allowing more of the throughflow to penetrate into the cavity.There are also significant differences between the radial distributions of tangential velocity in the two builds of the test rig.For the narrow annular gap,there is an increase of non-dimensional tangential velocity V/Ωr with radial location to solid body rotation V/Ωr=1.For the wider annular gap,the non-dimensional velocities show a decrease with radial location to solid body rotation. 相似文献
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Abnormal Shape Mould Winding 总被引:1,自引:0,他引:1
Fu Hongya Wang Xianfeng Han Zhenyu Fu Yunzhong 《中国航空学报》2007,20(6):552-558
为解决网格化芯模的缠绕问题,本文提出了复合材料面片缠绕机理;接着详细分析了面片缠绕过程中的芯模凹曲面上纤维滑线和架空现象,应用微分几何曲面理论和空间几何理论,提出判据及其解决方案;最后,针对飞机发动机进气道的缠绕成型,编制缠绕控制程序并进行相应的实验,验证了面片缠绕方法的可行性。 相似文献
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航天器返回地球的气动特性综述 总被引:4,自引:0,他引:4
航天器返回地球的飞行过程中,气动特性是实现将宇宙飞行速度减到落地前速度、保证再入飞行得到有效控制以及再入防热安全可靠的关键因素。针对简单旋成体气动外形、半弹道式再入控制、烧蚀防热类返回航天器,综述了返回地球过程中变化的空气流域特性、航天器周围的气体绕流环境、空气与航天器作用产生的动力学与热效应等。系统地给出了该类航天器的再入气动特性参数与飞行性能的共性规律,包括:气动阻力与再入减速、气动升力与再入轨迹控制、配平攻角与飞行稳定性、气动加热与防热,以及再入过程中不同气动特性航天器、气象条件变化等对再入飞行性能的影响规律。为航天器开展返回飞行过程的跨流域气动性能工程研制提供设计参考。 相似文献
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Research on Auto-detection for Remainder Particles of Aerospace Relay Based on Wavelet Analysis 总被引:2,自引:0,他引:2
GAO Hong-liang ZHANG Hui WANG Shu-juan 《中国航空学报》2007,20(1):75-80
Aerospace relay is one kind of electronic components which is used widely in national defense system and aerospace system. The existence of remainder particles induces the reliability declining, which has become a severe problem in the development of aerospace relay. Traditional particle impact noise detection (PIND) method for remainder detection is ineffective for small particles, due to its low precision and involvement of subjective factors. An auto-detection method for PIND output signals is proposed in this paper, which is based on direct wavelet de-noising (DWD), cross-correlation analysis (CCA) and homo-filtering (HF), the method enhances the affectiv-ity of PIND test about the small particles. In the end, some practical PIND output signals are analysed, and the validity of this new method is proved. 相似文献
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Effects of Mo on the Microstructure and Hydrogen Sorption Properties of Ti-Mo Getters 总被引:1,自引:0,他引:1
ZHOU Hong-guo WEI Xiu-ying MAO Chang-hui XIONG Yu-hua QIN Guang-rong 《中国航空学报》2007,20(2):172-176
The effects of Mo on the microstructure evolution, porosity and hydrogen sorption properties of Ti-Mo getters are investigated in this work. The results show that the addition of Mo prolongs the densification process of Ti-Mo getters and results in a significant amount of sintered pores. With the Mo content increasing, the porosity of getters firstly increases reaching the maximum value as it at- tains about 7.5wt.%, and then drops. At the room temperature, the hydrogen sorption property of getters increases progressively with the Mo content increasing, but the tendency is not very clear before its content lies below 2.5wt.%. When the Mo content achieves about 7.5wt.%, the hydrogen sorption property proves to be the best. The discussion is made about the above mentioned phenomena inclusive of hydrogen sorption properties of getters under different activation conditions (from 500-750 ℃). 相似文献
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YANG Fen ZHANG Xue-jun TIAN Fang WU Xu GAN Fu-xing 《中国航空学报》2007,20(2):181-186
Antimony-doped tin hydroxide colloid precipitates have been synthesized by hydrolysis of SnCl4 and SbCl3 using: (1) an ion-exchange hydrolysis to remove chlorine ions, and (2) isoamyl acetate as an azeotropic solvent to obviate water. The obtained dried powder is of high dispersivity without any need for further grinding. The size and dispersivity of the final particles are investigated with the aid of TG-DTA, BET, XRD and TEM. After having calcined, the antimony-doped tin oxide nanopowder possesses a tetragonal rutile structure with high dispersivity, uniform particles and low hard agglomeration. 相似文献