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朱超 《航空精密制造技术》2007,43(6)
"最大限度满足顾客的需求",这一不变的信念伴随着北京凝华实业有限公司走过了13年的风风雨雨,如今,这个观念已经深入到企业经营理念和企业文化的方方面面,并不断通过业务流程的重组和人员区域化的设置,成为公司上下遵从的理念。此外,凝华的"诚信、卓越、责任、中兴"价值观将全体员工的心凝聚在一起,尽展个人才华。而对于公司的常务副总裁李欲超先生来说,思考更多的,则是公司的发展方向。 相似文献
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航油价格忧思录 总被引:4,自引:0,他引:4
命运多舛的世界航空公司业刚从"9.11"事件和"非典"两大灾难的冲击后稍稍缓过一口气来,又面临着前所未有的油价高水平。每桶原油的标价由2004年初的三十多美元迅速攀升到年中的四十多美元,10月份则飙过了55美元的高峰。 一时间航空公司的股价又泛起绿潮。刚开始为民营低成本航空公司在中国露头而欣喜的中国消费者和媒体纷纷猜测:"油价升了,机票价格上涨还会远吗"?许多业内同仁或业外的经济学家则聚焦在民航的管制政策上:民航局明令取消的燃油附加费应否恢复?目前的机票公布价要不要更上一层楼?成本上涨了,价格似乎是当然的排泄口。也有不少人寄希望于期货市场,呼吁民航局为航空公司打开通往期贷市场的大门,用期货保值交易来对冲高油价的冲击。 本文试图从更广阔的视野来探讨这些问题和对策,有些想法同业内流行的观点不尽相同,提出来与同行们商榷,以期兼听则明。 相似文献
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空空导弹综合保障现状与对策 总被引:1,自引:0,他引:1
针对空空导弹的特点,总结了某型号开展的综合保障工作和收效,结合存在的问题,分析了综合保障现状,指出了空空导弹综合保障目前急需开展的工作和需要突破的技术. 相似文献
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航空维修思想的框架研究 总被引:1,自引:0,他引:1
提出并详细论述了由维修目标和所需资源的确定、重要维修项目的确定、故障模式及其影响分析、维修策略的选择、维修策略参数的优化、应用和评估、反馈修改组成的完整的航空维修思想框架结构。 相似文献
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在虹膜识别系统中,质量较差的虹膜图像可能被系统拒识,导致身份识别或身份认证的失败.因此有必要在虹膜图像的采集端引入质量评价环节,从虹膜图像采集仪输出的视频序列中挑选出符合识别系统要求的虹膜图像.为了减少序列图像质量评价的时间,根据图像的性质,对输入的序列图像进行步进式质量评价,不同的阶段设置不同的门限,只有满足要求的图像才能进入下一阶段的评价,这样将大大减少进行全部步骤评价的图像数量,能有效缩短序列图像评价的时间,保证了选取图像的质量和速度.试验结果表明,该算法能够有效地选择符合质量要求的虹膜图像. 相似文献
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2010年,将开启21世纪第二个十年。回首过去的十年,中国民航经历了一系列未曾预计到的挑战。首先是恐怖主义威胁。2001年的9.11事件,空前地将全世界的目光聚焦在恐怖主义对航空业的威胁上,世界民航业为此付出了惨重代价。对中国民航的影响要小一些, 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