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高同轴度精密零件在精密加工中,用普通方法很难保证其同轴度精度要求。本文采用增加径向辅助定位面的方法,从而使被加工零件的轴向和径向定位误差得到误差补偿,较好地满足了同轴度要求。 相似文献
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高同轴度精密零件在精密加工中,用普通方法很难保证其同轴度精度要求。本文采用增加径向辅助定位面的方法,从而使被加工零件的轴向和径向定位误差得到误差补偿,较好地满足了同轴度要求。 相似文献
3.
王瑞珍 《航空精密制造技术》1992,(2)
303研究所近期研制出了一台加工高同轴度的专用车床,主轴采用液体静压轴承,主轴座下设有高精度端齿盘,利用单面车削的方式,加工两端孔或轴要求高同轴度的零件。它比其它机床加工出的同心度要高出一个数量级。通过对铝、铜零件的试切,同轴度可稳定地达到1μm之内;圆度小于0.5μm;表面粗糙度高于Ra0.16((?)10)μm。这台设备不仅加工精度达到了国内外先进水平,而且外观新颖、结构紧凑、操作方便。这台机床的研制成功同时为航空航天部仪表、电机壳体、框架等类高同轴度零件的加工,开发出新的途径。 相似文献
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张灿海 《航空精密制造技术》1994,(5)
简要介绍了精密端齿分度盘的特点,并利用其特点开辟出端合转位同轴双面车削法,解决了同轴背孔零件高同轴度的加工难点,并研制了相应的加工设备,加工出较理想的试件和产品零件。 相似文献
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现有各类车床加工外圆或镗孔,均采用径向切入法,即把刀具安装于机床的中心高处,以横刀架进给对零件作径向进刀切削。由于一般车床横刀架刻度盘每格的刻度值为0.05毫米,因此,其进给精确度受到了一定限制。对于精度要求较高的零件,属于黑色金属材料的,往往在机械加工后进行磨削,而一些镁、铝及铜合金零件,则需在精密机床上加工。在精密设备较少的情况下,能否采用普通车床,加工出精度较高的镁、铝、铜合金零件呢?我们采取切向进刀法,较好地解决了这一问题。现介绍如下: 相似文献
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以具有较高同轴度和相交垂直度孔系的框架类零件为研究对象 ,抽象出有代表性的特征零件。分析了该类零件的精密加工工艺及其测量工作 相似文献
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三○三所在分析传统加工方法加工误差的基础上,研究了同轴双面车削法这一提高背孔零件同轴度的工艺措施。并研制了相应的加工设备:SMC-Ⅰ型和SMC-Ⅲ型双面车床。使原来传统加工方法所能达到的同轴度(5~10微米)提高到一个新的水平——可达到1微米。本文简要地介绍了有关情况。 相似文献
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《航空精密制造技术》1999,(6)
超精密加工的动向和思考NO.1超精密车床位置精度的计算机辅助测试系统 NO.1精密石墨零件的研磨 NO.1三轴中框轴系静态设计与装调(下)NO.1金钢石和超硬材料的应用与展望NO.2振动主动控制及其在超精密加工车床中的应用NO.2电镀CBN砂轮在转子槽磨削的应用NO.2超精密车床加工精度在线测量技术研究NO.3超精密空气主轴回转精度的测量与数据处理NO.3变螺距丝杠精密加工研究NO.4数控全自动磨床砂轮平衡装置的研究NO.4液压主轴的温度变化与超精密加工NO.4表面粗糙度的现状及发展NO.5… 相似文献
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为解决框架类零件的高位置度孔的精密镗削加工问题,研发了ZYTC600专用镗削机床.其精度指标优于现有的通用镗床(包括进口镗床),尺寸在500mm范围内,同轴度优于2μm,垂直度优于5μm,其中的关键部件双回转轴系分度精密转台采用了一套精密调整机构,可以实现0.2s”的精密调整,通过有限元分析得到其驱动刚度可达到800N/μm,可以满足加工需求. 相似文献
11.
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
20.
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