精确绘制半径样板检测放大图的方法

通过直角坐标系的平移、旋转确定圆弧上点的方法,提出了在万能工具显微镜上利用其有限工作行程,精确绘制半径样板圆弧检测放大图的方法。     

加速度计序贯式测试方法研究

介绍了加速度计在离心机上的序贯式测试方法。通过加速度计在离心机上一次安装即可实现加速度计 1g重力场标定、离心机静态半径测试和加速度计全量程试验。这是一种非常有应用前景的试验方法     

一种简易的双星定位系统定位解算方法

双星导航定位系统采用双星定位体制,其定位基本原理为三球交会测量原理,其中2颗量测量与用户到2颗卫星的距离有关,与用户高程有关的第3个量测量是决定系统定位精度的关键因素.为此,为了简化定位算法,文章根据地球椭球几何及大地纬度的相关知识,推导了与用户高程有关的第3个量测量的精确模型,进而建立了用户的定位算法.该算法具有简单...     

挤压油膜阻尼器失效问题分析

说明了研究挤压油膜阻尼器(简称SFD)减振失效的意义.首先,介绍了国际上研究SFD的J.W.Lund、E.J.Hahn、R.Holmes、R.A.Cookson和E.J.Gunter等五个学术集团,归纳出他们谈论到的有关挤压油膜阻尼器失效的观点,特别着重指出了挤压油膜阻尼器失效的不正确设计.失效的现象是过不了临界和导致转子支承系统产生双稳态特性.避免失效的方法是:调整油膜间隙与不平衡量间的关系,应用全油膜,限制不平衡量和采用弹性支座.本文的结论是:假如设计参数选择不当,挤压油膜阻尼器不仅不能减振,反而会导致转子支承系统工作不稳定或过不了临界.     

Active generalized predictive control of turbine tip clearance for aero-engines

Active control of turbine blade tip clearance continues to be a concern in design and control of gas turbines. Ever increasing demands for improved efficiency and higher operating temperatures require more stringent tolerances on turbine tip clearance. In this paper, a turbine tip clearance control apparatus and a model of turbine tip clearance are proposed; an implicit active generalized predictive control （GPC）, with auto-regressive （AR） error modification and fuzzy adjustment on control horizon, is presented, as well as a quantitative analysis method of robust per- turbation radius of the system. The active clearance control （ACC） of aero-engine turbine tip clear- ance is evaluated in a lapse-rate take-off transient, along with the comparative and quantitative analysis of the stability and robustness of the active tip clearance control system. The results show that the resultant active tip clearance control system with the improved GPC has favorable steadystate and dynamic performance and benefits of increased efficiency, reduced specific fuel consump- tion, and additional service life.     

New design of a compact aero-robotic drilling end effector: An experimental analysis

This paper presents the development of a normal adjustment cell (NAC) in aero-robotic drilling to improve the quality of vertical drilling, by using an intelligent double-eccentric disk nor-mal adjustment mechanism (2-EDNA), a spherical plain bearing and a floating compress module with sensors. After the surface normal vector is calculated based on the laser sensors’ feedback, the 2-EDNA concept is conceived specifically to address the deviation of the spindle from the sur-face normal at the drilling point. Following the angle calculation, depending on the actual initial position, two precise eccentric disks (PEDs) with an identical eccentric radius are used to rotate with the appropriate angles using two high-resolution DC servomotors. The two PEDs will carry the spindle to coincide with the surface normal, keeping the vertex of the drill bit still to avoid repeated adjustment and position compensation. A series of experiments was conducted on an aeronautical drilling robot platform with a precise NAC. The effect of normal adjustment on bore diameter, dril-ling force, burr size, drilling heat, and tool wear was analyzed. The results validate that using the NAC in robotic drilling results in greatly improved vertical drilling quality and is attainable in terms of intelligence and accuracy.     

电极摇动对微细电火花加工微孔深径比的影响

微细电火花具备加工任何导电材料和大深径比微孔的能力。但是随着孔深度的增加,气泡和加工屑很难排出孔外,导致频繁的非正常放电,从而使得电火花常规放电状态下微孔的深径比有限,然而电极摇动可以为电火花狭小放电间隙提供一个非均匀的流场,提高了排屑能力,这有助于提高微孔的深径比。着重研究微孔加工在去离子水和油两种介质下,电极摇动参数和电参数对微孔深径比的影响。试验结果表明:电火花常规放电状态下微孔的深径比随着摇动半径和电容的增加而增加,摇动速度对微孔深径比则没有明显的影响,这为实际生产中加工大深径比微孔提供了参考依据。     

一级旋流入射半径对小尺寸旋流杯下游流动特征的影响

为探索一级旋流入射半径对小尺寸旋流杯下游流动特性的影响,采用PIV测速技术对小尺寸旋流杯下游速度分布特征进行了试验测量。结果表明:不同入射半径的一级旋流会形成扩张流场或扩张-收缩-扩张流场;入射半径方向相反、数值不同将对旋流杯下游流动产生不同影响;旋流杯下游流场涡量分布与同一方案的速度分布相似,旋流杯出口平均涡量较强的旋流沿流向涡量逐渐衰减,且速率变缓;不同一级旋流入射半径的旋流杯方案的平均涡量变化趋势基本一致。在所研究的试验状态下,一级旋流入射半径对小尺寸旋流杯下游速度和涡量分布特征产生了较大的影响。     

干涉配合紧固件孔的弹塑性工程分析

本文根据厚壁筒概念,以平面应变、有限边界情况和理想塑性材料的假定,对铆接或螺接干涉配合紧固件孔边的应力场进行了弹塑性工程分析,给出了便于分析使用的计算弹性配合的极限干涉量,塑性配合的塑性区半径,弹、塑性区内的径向和周向应力分布等参数方程式,这些参数和参数方程式对紧固件孔的疲劳设计和生产工艺都具有十分重要的意义。 应用分析说明了铆距和耳片外边界半径对所得结果的影响,以及平面应变和理想塑性材料与平面应力和幕强化塑性材料假定对于孔边应力分布的影响。     

液固横向耦合系统的动响应及圆柱贮箱中液体节径运动规律研究

导出了圆柱贮箱中液体与弹簧质量系统耦合的动力学方程,并在其动响应的基础上考察了圆柱贮箱中液体节径的运动规律．