某型飞机液压油箱内部隔板变形故障分析

在进厂大修过程中,发现多架某型飞机液压油箱内部的隔板出现变形和疑似裂纹的质量问题。通过分析该故障的发生机理,复查修理过程,最终确定故障原因是该型飞机液压油箱增压系统存在设计缺陷。     

装备时延校准及监控技术研究CSCD

装备时延校准误差是靶场测控系统中事件记录和交会定位的重要误差因素,其精确校准是实现装备时间同步的关键技术。针对装备时延问题展开研究,提出了一种物理含义清晰、易于测量的装备时延定义,实现了离散站点装备时延校准,验证了基于改进型B码的装备时延校准监控的有效性。试验结果表明,时延校准的精度达到了十微秒量级。     

超薄零件车削加工变形研究

超薄零件车削加工后存在较大的变形,严重制约了该类关键器件的广泛应用。为实现超薄零件加工变形的预测与分析,基于力学分析,建立了加工仿真系统并进行超薄零件精加工过程模拟研究。实际加工验证了所建立模型的准确性,同时基于该系统对超薄零件加工后变形进行分析,其结果对改进加工工艺和减小工件变形具有指导意义。     

First results of MWC SAS3 electromagnetic wave experiment on board of the Chibis-M satellite

The main goals of the Chibis-M mission are the testing of a new micro-satellite technology, the study of new physical processes related to lightning activity and the verification of possible monitoring techniques of Space Weather phenomena. In frames of the Chibis-M mission an electromagnetic wave complex MWC is installed on board of the satellite composed of electromagnetic sensors and SAS3 measuring unit. The obtained data show that the scientific instrumentation operates properly and produces interesting information. Here we present the first results of the first year of operation of the MWC in the ELF–VLF bands in different operation modes. An important conclusion is that basing on the experience of the first year it is possible to realize an effective and reliable Space Weather monitoring system using micro-satellites and simultaneously operating ground support equipments.     

结构变形对斜流压气机性能的影响研究

采用基于有限元的结构静强度分析和CFD全三维流场仿真手段,对某斜流压气机工作状态下结构变形和变形后的气动性能进行研究,结果表明:提出的数值仿真流程能够有效模拟压气机工作状态下结构变形对气动性能的影响,从而为发动机系统参数平衡提供数据支撑;压气机叶片前缘顶部刚度小,变形量大,但对叶轮气动性能影响较小;叶轮尾缘边径向变形对压气机增压能力影响显著;顶部泄漏间隙的变化对压气机效率产生影响.     

航空发动机地面监控站开发标准初探

文章对国外发动机状态监控地面站的相关标准进行了深入分析,在此基础上构建了国内航空发动机地面监控站开发标准的框架,并给出了标准的主体内容以及相关标准体系建设的一些建议。     

核统计分析和监测方法处理多模式批处理过程

提出了一种解决批处理过程多种工作模式故障检测问题的方法。该方法从多种工作模式中提取各个模式相类似的信息,解决了该工作模式下故障检测建模问题;将核函数应用到算法中,利用核技术提高算法处理非线性数据故障检测的能力;将在每种工作模式下的数学模型进行分解,将反映相似信息和各个模式不同的信息进行分离,并分别建立故障检测模型,通过分析可以辨别出当前所处的工作模式,并且有效地检测故障的发生。     

航空发动机健康评估技术综述

健康评估技术是航空发动机健康管理的关键技术之一。详细阐述了航空发动机健康评估的研究内容,重点分析了发动机气路性能、结构以及机械系统健康评估的特点,并指出了开展航空发动机健康评估关键技术研究的重要性。     

Monitoring coastal sea level using reflected GNSS signals

A continuous monitoring of coastal sea level changes is important for human society since it is predicted that up to 332 million people in coastal and low-lying areas will be directly affected by flooding from sea level rise by the end of the 21st century. The traditional way to observe sea level is using tide gauges that give measurements relative to the Earth’s crust. However, in order to improve the understanding of the sea level change processes it is necessary to separate the measurements into land surface height changes and sea surface height changes. These measurements should then be relative to a global reference frame. This can be done with satellite techniques, and thus a GNSS-based tide gauge is proposed. The GNSS-based tide gauge makes use of both GNSS signals that are directly received and GNSS signals that are reflected from the sea surface. An experimental installation at the Onsala Space Observatory (OSO) shows that the reflected GNSS signals have only about 3 dB less signal-to-noise-ratio than the directly received GNSS signals. Furthermore, a comparison of local sea level observations from the GNSS-based tide gauge with two stilling well gauges, located approximately 18 and 33 km away from OSO, gives a pairwise root-mean-square agreement on the order of 4 cm. This indicates that the GNSS-based tide gauge gives valuable results for sea level monitoring.     

双S弯喷管的流固耦合特性研究

为了明晰S弯喷管的流固耦合特性,数值模拟了流固耦合作用下双S弯收敛喷管的结构变形特征及其内/外流特性。结果表明：S弯喷管的圆转方弯曲构型产生了非均匀的流场分布,并增强了结构的弹性特征,它们通过交换气动载荷与变形位移数据形成了S弯喷管流固耦合的作用机理。在气动载荷作用下,S弯喷管沿Y向的最大变形位移为25.3mm,它位于喷管出口上壁面的中心位置。当喷管的结构变形稳定时,第二弯转弯处下壁面的气流加速至局部超音速,壁面静压大幅降低;第一弯下游上壁面附近形成了气流分离区;喷管出口喷流沿轴向向上偏转。流固耦合作用导致S弯喷管的流量系数减小0.6%,推力系数降低1.8%。矩形截面与弯曲构型是影响S弯喷管流固耦合特性的主要几何特征,其中矩形截面能够显著增大喷管的变形位移;S形弯曲构型虽然能够有效抑制变形特征,但它导致喷管多个区域出现变形,喷管的结构变形分布变得更加复杂。