一种新型热线热膜流速计

在剖析传统热线热膜风速计存在问题的基础上,提出了解决这些问题的思路、方案和具体的线路模型,形成了预移相型热线热膜流速计的构思.首先对传统热线风速计的物理模型进行改进,用数学方程加以描述并求出其解析解提出一系列设计公式,进而选择适当的线路环节,编制相应的软件,实现上述物理模型、数学方程和设计公式的要求,形成了具有6大特色的"IFV900A型智能热线热膜流速计".     

一种新型热线热膜流速计

在剖析传统热线热膜风速计存在问题的基础上,提出了解决这些问题的思路、方案和具体的线路模型,形成了预移相型热线热膜流速计的构思。首先对传统热线风速计的物理模型进行改进,用数学方程加以描述并求出其解析解提出一系列设计公式,进而选择适当的线路环节,编制相应的软件,实现上述物理模型、数学方程和设计公式的要求,形成了具有6大特色的“IFV900A型智能热线热膜流速计”。     

电传飞机人机闭环系统的诱发振荡

 具有潜在危险、突发性的,可能导致飞行失控的严重人机闭环诱发振荡(PIO——Pilot Induced Oscillation)是电传飞机发展阶段频频发生飞行事故的首要原因.迫使人们去研究它产生的飞行动力学机理;查明引发它的飞行控制系统设计缺陷,寻找防范严重PIO的设计方法、工具和工作流程…….电传飞机的PIO事故,实际上在世界范围内推动了对人机耦合问题的新一轮的再认识,其中包括提出更确切的定义;提出更全面的多种分类方法;开发更有效的,考虑非线性因素、能辨识严重PIO振荡趋势的评估准则.     

基于CT 技术的金属键合引线三维测量专用夹具

准确测量金属键合引线三维形貌,进而通过仿真方式获得键合引线S参数,是评估键合引线对器件级联工艺影响的重要手段。X射线电子计算机断层扫描技术是进行级联电路芯片中金属键合引线测量的有效工具,但是由于级联电路芯片中的键合引线材料、形状、尺寸的特殊性,需要研究专用的夹具提升测量准确度,本文通过结构优化、材料筛选,设计出一种更加稳定、准确度更高的新型测量夹具。     

程序调参飞行控制律的神经网络实现

为保证飞行品质,现代飞机中多采用程度调参飞行控制律,由于调参规律的高度非线性,使得控制律的工程实现相当困难。为此,对程序调参飞行控制律的神经网络实现方法进行了研究。通过应用ＢＰ神经网络逼近非线性调参规律。探讨了用ＢＰ网络实现程序调参飞行控制律的一般方法,给出了网络的结构及其优化算法,并以某型飞机电传操纵系统倾斜阻尼通道的程序调参控制律为例,对该实现方法进行降验证。结果表明,实现精度符合工程要求。     

Integrating aeromagnetic data and Landsat-8 imagery for detection of post-accretionary shear zones controlling hydrothermal alterations: The Allaqi-Heiani Suture zone,South Eastern Desert,Egypt

The Arabian-Nubian Shield (ANS) underwent a regional carbonation event with CO₂ fluxes derived from the mantle and circulated along post-accretionary shear zones, thus affecting the redistribution of gold mineralization. Formerly, the analyses of remotely-sensed data have suggested regions of gold mineralization linked to the post-accretionary structured framework, but the results were insufficient for detailed prospecting in the ANS. In this research, aeromagnetic data and Landsat-8 imagery were integrated for delineating new high potential zones of gold mineralization in the Allaqi-Heiani Suture (AHS) zone, the ANS, South Eastern Desert (SED) of Egypt. Aeromagnetic data were enhanced using the Center for exploration targeting (CET) grid enhancement technique to detect the main structures that control hydrothermal alterations in the study area. Principal Component Analysis (PCA) technique and ratios of spectral bands were applied to Landsat-8 data for mapping zones of hydrothermal alteration associated with gold mineralization. The traced structural elements from RTP, CET and Landsat-8 maps were statistically plotted and interpreted using rose diagrams. These diagrams indicated that the NW and NE trends are the most dominant in the RTP map and that the intersection zones obtained from the CET analysis are aligned along the NW-oriented trend. While the NNW, WNW and NE trends were the most dominant ones in Landsat maps. The integration of the results indicates several new high potential zones of gold and Cu/Ni mineralization types, which are mostly concentrated at the western part of the AHS zone. The hydrothermal alteration zones and associated gold mineralization are strongly linked to NW, NE, E-W and WNW trending lineaments. The approach used in this study can be applied to other parts of the ANS and other regions with similar geological conditions around the world.     

计入导线故障的民机安全性定量分析方法研究

将导线故障引入安全性定量分析方法中，介绍了安全性分析的现状、存在的问题以及计入导线故障的必要性。通过将导线故障和安全性分析相结合，提出一种计人导线故障的安全性定量分析方法。对影响导线故障的机理进行探究与分析，提出“导线故障率影响因子”概念，阐述了影响导线故障率的主要因素及其类型，建立了一种民用飞机实际导线故障率计算方法与模型，以及在单一状态和多种状态下导线故障率计算方法，并对方法进行案例分析，使安全性定量分析更准确、有效和完善，大大减少了导线故障所引起的不安全事件，为民用飞机安全性和合格审定工作提供了有力的支持。     

高阶椭圆齿轮的三维实体设计与线切割加工

非圆齿轮可以实现周期性的非匀速比运动,在各种精密机械中都得到了日益广泛的应用。综合应用CREO的参数化设计功能、ADAMS的运动仿真功能、CAXA线切割的代码生成功能实现了三阶椭圆齿轮的设计与制造,为单件及小批量生产场合创建了典型范式,适用于各种类型非圆齿轮的设计与制造。     

Experimental study of flow field distribution over a generic cranked double delta wing

The flow fields over a generic cranked double delta wing were investigated. Pressure and velocity distributions were obtained using a Pitot tube and a hot wire anemometer. Two different leading edge shapes, namely ‘‘sharp" and ‘‘round", were applied to the wing. The wing had two sweep angles of 55° and 30°. The experiments were conducted in a closed circuit wind tunnel at velocity 20 m/s and angles of attack of 5°–20° with the step of 5°. The Reynolds number of the model was about 2 ×10~5 according to the root chord. A dual vortex structure was formed above the wing surface. A pressure drop occurred at the vortex core and the root mean square of the measured velocity increased at the core of the vortices, reflecting the instability of the flow in that region. The magnitude of power spectral density increased strongly in spanwise direction and had the maximum value at the vortex core. By increasing the angle of attack, the pressure drop increased and the vortices became wider; the vortices moved inboard along the wing, and away from the surface; the flow separation was initiated from the outer portion of the wing and developed to its inner part. The vortices of the wing of the sharp leading edge were stronger than those of the round one.     

CMT增材制造工艺对5356铝合金熔敷层组织及力学性能的影响

采用冷金属过渡(CMT)电弧增材方法,以5356铝合金焊丝为试验对象,研究了送丝速度与焊接速度对5356铝合金电弧增材制造成形的影响,并分析了熔覆层微观组织特性和增材试样的力学性能。结果表明:送丝速度和焊接速度是电弧增材制造尺寸精度的重要影响因素;熔覆层微观组织可分为3个区域。不同焊接速度下,增材试样的力学性能均超过焊丝拉伸强度标准值,抗拉强度平均值达到274.7 MPa。