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硬质合金上金刚石膜的沉积 总被引:10,自引:0,他引:10
综述了为提高金刚石薄膜与硬质合金基体间结合强度所进行的研究,如制备细晶基体、对基体进行前处理、优化金刚石成膜的工艺条件以及在基体和金刚石膜间施加过渡层等.分析归纳了各种因素的影响规律,并对该研究前景进行了展望. 相似文献
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极厚型金刚石涂覆刀片由美国ASTEX公司新研制出极厚型金刚石涂层硬质合金刀片。其制作过程如下:在硬质合金刀片上涂复一层厚度达1mm的金刚石薄膜(相当于PCD刀片的厚度),然后用EDM或激光机切割成厚度为2~5mm的三角形刀片,再在真空炉中将刀片焊接到... 相似文献
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Al/SiC复合材料的准分子激光表面改性 总被引:1,自引:0,他引:1
利用KrF准分子激光对SiC晶须增强铝基复合材料进行表面改性。借助于显微镜及X射线衍射技术,对激光处理前后试件表层的显微组织及化学结构进行了分析。结果表明,准分子激光处理后,试件表面形成了一个几微米厚的铝层。该薄层中基本上不含金属间化合物,SiC增强相的数量也显着减少。腐蚀测试结果表明,准分子激光表面处理后,材料的抗腐蚀性能得到了显着提高。 相似文献
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为了研究砂轮表面结构化对砂轮磨削性能的影响,利用脉冲激光对树脂结合剂金刚石砂轮进行了表面宏观结构化。采用6种不同类型的金刚石砂轮表面宏观结构进行了氧化铝的磨削实验,建立了激光宏观结构化金刚石砂轮的磨削力模型,比较了6种不同激光宏观结构化金刚石砂轮与非结构化砂轮在不同磨削参数下磨削力的差异,分析了砂轮制造后的表面形貌与结构化砂轮的磨损特性。实验结果表明,砂轮宏观结构化对磨削性能有很大影响,激光宏观结构化砂轮的磨削力可以减小2. 5%~24. 5%,砂轮结构化后的表面形貌出现石墨化现象;宏观结构化砂轮沟槽边缘磨损加剧,但沟槽磨损并没有明显加快宏观结构化砂轮的磨损。 相似文献
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金刚石砂轮是磨削硬质合金材料最有效的工具之一。目前一般都采用树脂结合剂的金刚石砂轮,用于磨方法磨削硬质合金,磨削时磨料尖刃所产生的局部磨削热在400℃以上,致使结合剂软化,影响了磨料与结合剂的结合强度,使得一半左右的磨料还没有充分发挥磨削作用时,就从砂轮上脱落下来了,因而影响了这种工具的广泛使用。针对这个问题,我们在生产实践中摸索出一种比较先进的磨削方法即湿磨法。所谓湿磨法,就是使用铜基结合剂的金刚石砂轮并加冷却液进行磨削。用湿磨法磨削硬质合金,磨削深度由0.02毫米增加到3毫米,砂轮使用寿命由原来的三至六个月延长到二至三年,充分发挥了金刚石砂轮磨削硬质合金的优越性。 相似文献
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对CVD金刚石膜的离子束铣削、电子束加工、激光加工、化学辅助机械抛光、热化学抛光等抛光技术的加工方法与原理进行了介绍,分析了这些方法的优点和不足之处。并展望了CVD金刚石薄膜抛光技术的发展方向。 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