Experimental study of hydrogen-rich/oxygen-rich gas-gas injectors

Five types of coaxial injectors were investigated experimentally using hot hydrogen-rich gas and oxygen-rich gas, which were respectively provided by a GH2/GO2 hydrogen-rich perburner and a GH2/GO2 oxygen-rich preburner. The injectors were the shear coaxial injector, the oxidizer post expansion coaxial injector, the fuel impinging coaxial injector, the central body coaxial injector, and the shear tri-coaxial injector. The characteristic velocity efficiency and the combustor＇s wall temperatures were obtained for different design parameters through the experiments. It can be con- cluded that angles of the oxidizer post expansion and the fuel impinging have little influence on the combustion performance and the wall temperatures. The contact area between fuel and oxidizer and the mass flow rate have significant impacts on the combustion performance. The shear tri-coaxial injector has the best combustion performance but also the highest wall temperatures among the five types of injectors.     

飞轮振源特征参数提取方法及其分布特性

为了从飞轮微振动输出中提取飞轮转子的振源信息，提出利用鲁棒回归辨识飞轮在升速过程中各主要阶次的振幅对转速的二次幂系数，并将其作为飞轮的振源幅值特征参数；为探究参数的分布特性，利用Weibull分布拟合多个飞轮在同一阶次的特征参数，并计算出特定概率点的分位数。振源特征参数的分位数既系统地展示了飞轮振源分布情况，亦可作为振源分级判据。将该方法成功应用于50 Nms飞轮的振源特征参数分布研究中，为该型飞轮的超静性能筛选和设计改进提供了判定准则和参考依据。     

基于模糊层次分析法的机场管制模拟机评价

采用模糊综合评判法与层次分析法相结合的评估方法,对机场管制模拟机仿真度进行评价.根据机场管制模拟机需求功能选取恰当的评估指标,用层次分析法建立机场管制模拟机仿真度评价指标体系.然后分层次进行模糊综合评判,得出综合评价结果.最后以某机场管制模拟机为例,对其仿真度进行评估.结果表明这种方法科学合理且容易实现,为实验室设备选型提供了合理的依据,具有实际的应用价值.     

去中心化时差频差直接定位方法

针对原始利用时差频差的直接定位(DPD)方法存在数据传输量和计算量大的瓶颈,提出了两种去中心化直接定位方法。第1种方法采用去中心化配对方案,只将各观测站截获信号在站间进行一次传输,将数据传输和计算分散到各观测站间并行计算互模糊函数(CAF),构造仅满足满秩条件的互模糊矩阵(CAM)。第2种方法根据推导的任意互模糊函数间关系公式,采用归约方式去中心化的在各观测站并行计算余下互模糊函数,补全互模糊矩阵。两种方法都降低了直接定位数据传输量,提高了计算效率。性能分析和仿真实验表明本文两种方法精度性能优于两步定位方法,在低信噪比时两种方法都可达到比较理想的精度性能,在高信噪比时第2种方法与原始直接定位方法的精度性能相当。     

基于三维模型定义技术应用的思考

MBD技术是一个新生事物,涉及到系统性问题,它的应用实施是一项长期、复杂而又艰巨的工作。需要考虑的问题不仅涉及技术方面,还有文化、管理、组织和生产方式等方面,只有解决好这些问题,才能充分发挥MBD技术的巨大效力,更好地为我国大飞机研制服务。     

Coastal sea level changes in Europe from GPS,tide gauge,satellite altimetry and GRACE, 1993–2011

Sea level changes are threatening the human living environments, particularly along the European Coasts with highly dense population. In this paper, coastal sea level changes in western and southern Europe are investigated for the period 1993–2011 using Global Positioning System (GPS), Tide Gauge (TG), Satellite Altimetry (SA), Gravity Recovery and Climate Experiment (GRACE) and geophysical models. The mean secular trend is 2.26 ± 0.52 mm/y from satellite altimetry, 2.43 ± 0.61 mm/y from TG+GPS and 1.99 ± 0.67 mm/y from GRACE mass plus steric components, which have a remarkably good agreement. For the seasonal variations, annual amplitudes of satellite altimetry and TG+GPS results are almost similar, while GRACE Mass+Steric results are a little smaller. The annual phases agree remarkably well for three independent techniques. The annual cycle is mainly driven by the steric contributions, while the annual phases of non-steric (mass component) sea level changes are almost a half year later than the steric sea level changes.     

Relationship Between Corrosion Level of Steel Bar and Diameter of Corroded Sensing Steel Wire in Wireless Sensor

A kind of wireless sensor was previously developed,which is powered and transmit signals wirelessly instead of using an electrical connection to the embedded reinforcement.Based on this technique,the relationship between diameters of corroded sensing steel wires and corrosion levels of steel bars is established by experiments.Quadratic function is utilized to fit the experiment results,and the correlation coefficients are all larger than 0.95.Estimated corrosion levels of commonly used steel bars are given for different diameters of corroded sensing steel wires fractured due to corrosion.     

数控仿形铣槽机床仿形系统的设计与改造

FCX-2000型数控铣床是我厂用于大型零件铣槽的设备,针对其控制系统以及仿形系统存在的技术问题,提出了一种控制系统标准化的改造以及利用激光采样进行仿形系统改造的方案,主要从仿形系统的原理分析、硬件与软件方面进行论述.     

天线测试平台系统设计与安装

简要介绍了天线测试平台系统的基本工作原理、系统（机械系统、测量系统、控制系统）设计、材料选择、误差分析和系统的现场安装。     

航天火工品爆炸冲击多参量的测试

航天器上使用了大量的火工装置来完成特定的功能,它们在动作时会引起强烈的高频冲击环境,对航天器上的仪器设备产生不利的影响.本文借鉴活塞压力计的原理设计了一种专用爆发器,它同时具有传统的密闭爆发器和推力测试架的功能,能够同时测试航天火工品爆炸后产生的压力、加速度和位移等冲击参量,可增加一次试验能够获得的测试信息量.