Impact of lubricant traction coefficient on cage's dynamic characteristics in high-speed angular contact ball bearing

In this paper, the formulas of elasto-hydrodynamic traction coefficients of three Chinese aviation lubricating oils, 4109, 4106 and 4050, were obtained by a great number of elasto-hydrodynamic traction tests. The nonlinear dynamics differential equations of high-speed angular contact ball bearing were built on the basis of dynamic theory of rolling bearings and solved by Gear Stiff (GSTIFF) integer algorithm with variable step. The impact of lubricant traction coeffi-cient on cage's dynamic characteristics in high-speed angular contact ball bearing was investigated, and Poincare map was used to analyze the impact of three types of aviation lubricating oils on the dynamic response of cage's mass center. And then, the period of dynamic response of cage's mass center and the slip ratio of cage were used to assess the stability of cage under various working con-ditions. The results of this paper provide the theoretical basis for the selection and application of aviation lubricating oil.     

上舱门框体高速数控加工技术

就某轻型公务机上舱门框体零件所采用的高速数控加工工艺、工装的订制、加工刀具、编程、变形控制技术等方面进行研究分析,同时论述了如何解决这类零件加工难点及提高生产效率问题。     

太阳风中的Alfven波耗散与电子和质子温度分布问题

根据动力论Alfven波耗散机制,详细计算了动力论Alfven波衰减的能量分配给质子和电子的比率.初步解释了高速太阳风中质子温度比电子温度高的事实,定性说明了r＜10R_s时电子快速冷却的原因.      

高速1553B智能通用总线测试平台设计

传统的1 Mbps 1553B由于总线带宽受限,在航天测量控制领域正逐步被4 Mbps高速1553B总线替代.一般的高速1553B总线测试仪不具备精准时序控制、动态消息插入和系统故障恢复的功能,难以模拟系统实际工况.因此,通过各模式下总线的初始化配置和数据收发控制,采用SDRAM动态读取和硬件定时触发技术,结合基于心跳...     

高速燃油离心泵空化特性分析

为揭示高速燃油离心泵内部空化形态及隔舌区域空化的发生工况,对其进行了非定常数值计算,分析了不同流量下高速燃油泵内空化流场特性及压力瞬态特性。结果表明：在不同流量下,空泡首先在叶片前缘生成;随着空化数降低,空泡在叶片根部及延伸叶片背面产生;在1.2倍设计流量下隔舌区域的空化在低空化数下发生;空化对叶片表面根部的压力载荷影响较大;叶轮流道监测点压力脉动主频为叶轮轴频;隔舌监测点脉动主频为叶频,在1.2倍设计流量下的低空化数下隔舌区域监测点压力脉动频谱上轴频倍频特征增强。     

无人机大气数据高速检测系统的设计

无人机大气数据(高度、空速)的检测速度关系到飞行控制系统的性能。选定传感器模块后,要从采集前端提高检测系统的速度较困难。基于GM8123芯片建立的数据检测系统,提出了运用串口扩展技术提高数据传输速率,进而实现系统对数据的高速采集和处理。实验证明:本系统对于提高无人机大气数据检测的动态性能,提高测量精度有较高实用价值。     

典型难加工材料叶片切削加工研究

本文通过建立刀具磨损预测模型,并将该模型理论和现场生产实际相结合,在保证加工质量要求的前提下,给出了难加工材料(GH2132)经济效益最大化的切削加工参数,并在航空发动机叶片型面加工中获得验证,取得了加工质量、加工效率和加工成本的最优结合,为解决航空典型难加工材料的切削参数优化问题提供了重要依据和解决途径,这对于提高航空发动机难加工材料的加工效率和降低加工成本具有重要意义。     

Modeling high-speed cutting of SiCp/Al composites using a semi-phenomenologically based damage model

In this paper, we attempts to investigate cutting mechanisms in high-speed cutting of Al6061/SiC_p/15p composites using a semi-phenomenologically based damage model in the equivalent homogeneous material (EHM) framework. By combining macroscale EHM modeling and underlying microscale physical mechanisms, a feasible semi-phenomenological plastic model is proposed for prediction of cutting forces and chip morphology during high-speed turning Al6061/SiC_p/15p composites. This model incorporates the modified Weibull weakest-link effect to represent the strain-based damage evolution in large deformations. This proposed semi-phenomenological constitutive model is implemented by compiling material subroutines into cutting finite element (FE) codes. The effects of the critical shear stresses on chip formation that depend on the tool-chip frictional coefficient are accounted for in the cutting FE model. The chip formation mechanism affecting material removal behaviors during high-speed turning is further investigated. The capabilities of the proposed constitutive model are evaluated by comparing cutting forces and chip morphologies between experiments and simulations at different cutting speeds associated with strain rates. The EHM-based and microstructure-based models are further compared in both computational efficiency and accuracy. The simulation results show that the developed semi-phenomenological constitutive formalism and cutting model are promising and efficient tools for further investigation of dynamic mechanical and cutting behaviors of particle-reinforced composites with different volume fraction and particle size.     

基于V9机的高速采集存储系统在光电经纬仪中的应用

以数字视频替代摄影系统已成为近二十年来光测设备研制与使用人员的追寻目标,随着高分辨率高速CCD图像技术日臻完善,用高帧频的数字相机取代摄影机已成为可能。本文基于美国Vision Research,Inc生产的高速数字相机——Phantom V9.0(黑白)的特性提出了高速采集存储系统的设计方案。并已在某光电经纬仪中得到了应用。     

Variable load failure mechanism for high-speed load sensing electro-hydrostatic actuator pump of aircraft

This paper presents a novel transient lubrication model for the analysis of the variable load failure mechanism of high-speed pump used in Load Sensing Electro-Hydrostatic Actuator (LS-EHA). Focusing on the slipper/swashplate pair partial abrasion, which is considered as the dominant failure mode in the high-speed condition, slipper dynamic models are established. A forth sliding motion of the slipper on the swashplate surface is presented under the fact that the slipper center of mass will rotate around the center of piston ball when the swashplate angle is dynamically adjusted. Besides, extra inertial tilting moments will be produced for the slipper based on the theorem on translation of force, which will increase rapidly when LS-EHA pump operates under high-speed condition. Then, a dynamic lubricating model coupling with fluid film thickness field, temperature field and pressure field is proposed. The deformation effects caused by thermal deflection and hydrostatic pressure are considered. A numerical simulation model is established to validate the effectiveness and accuracy of the proposed model. Finally, based on the load spectrum of aircraft flight profile, the variable load conditions and the oil film characteristics are analyzed, and series of variable load rules of oil film thickness with variable speed/variable pressure/variable displacement are concluded.