高档机床主轴自动换挡PLC控制及实现

通过修改数控系统机床参数与PLC编程,实现了配套国产高档数控系统的大型五坐标双龙门铣床的自动换挡.执行换挡过程中控制主轴电机来回摆动,换挡冲击小,易于液压拔叉推动齿轮实现稳定配合,可靠性高,提高了国产数控系统在航空领域的应用水平.     

基于粗糙集理论的翼型参数优选方法研究

在设计机翼时,通常需要进行多目标决策,而教练机机翼翼型选取的先验经验不足,需要进一步研究,从而得出翼型的选择规则.分析国内外已有教练机机翼翼型使用情况,运用粗糙集理论中基于重要度和条件信息熵结合的权重确定方法,提出在机翼方案设计阶段翼型的选择方法;对比分析三种分段方法在翼型性能指标离散化时的优缺点及其原因,并结合算例进行适用性验证.结果表明:在有限数据条件下,两断点方法是比较合适的属性离散化方法.所提出的方法具有使用价值,对飞机设计方案阶段翼型的选择以及机翼的气动设计具有参考意义.     

起落架有限元梁模型建立及其静力学分析

为了获得起落架载荷传递以及评估几何非线性和静不定对起落架载荷传递的影响,同时探索起落架结构有限元梁模型的建模方法,应用HyperMesh和Ansys联合仿真的方法搭建某型具有局部静不定特征的前起落架、主起落架有限元梁模型;使用此模型进行三种载荷工况的静力学计算,获得考虑静不定和几何非线性的起落架接头和截面载荷,以及在单位载荷作用下起落架的航向、侧向和扭转刚度,并与传统方法计算结果进行对比.结果表明:有限元方法和传统方法获得的接头载荷有差异,部分差异超过了±10％,最大差异达到30％;计算前起落架外筒横梁、斜梁截面内力的传统方法及其简化具有合理性,对起落架支柱设计具有指导意义.     

盾牌击打试验机的研究

在成功研制盾牌击打试验机的基础上，对盾牌击打试验机能量计算所涉及的理论进行了分析，用击打中心理论解释了击打棍的击打位置和击打能量之间的关系，并给出了试验的具体数据。     

波音747飞机起落架拆装车设计及其强度校核

在重点研究起落架拆装过程中所使用的工装设备的基础上，应用CATIA V5三维软件设计了一款波音747飞机起落架拆装车，并用ABAQUS For CATIA V5软件对所建拆装车模型的关键部件进行有限元分析。     

The first new application of the Mathematical Theory of Stochastic Processes to lunar and planetary science: Topography-Profile Diagrams of Mars

The Mathematical Statistics Theory (MST) and the Mathematical Theory of Stochastic Processes (MTSP) are different branches of the more general Mathematical Probability Theory (MPT) that can be used to investigate physical processes through mathematics. Each model of a stochastic process, according to MTSP, can provide one or more interpretations in the MST domain. A large body of work on impact crater statistics according to MST exists, showing cumulative crater frequency (N km⁻²) as a function of age (years) for some particular crater diameter. However, this is only one possible representation in the MST domain of the bombardment of the planetary surface modeled as a stochastic process according to MTSP. The idea that other representations are possible in the MST domain of the same stochastic process from MTSP has been recently presented. The importance of the approach is that each such mathematical-based interpretation can provide a large amount of new information. Coupled with MOLA data, Topography-Profile Diagrams (TPD) are one of the many examples that can provide a large amount of new information regarding the history of Mars. TPD consists of: (1) Topography-Profile Curve (TPC), which is a representation of the planet’s topography, (2) Density-of-Craters Curve (DCC), which represents density of craters, (3) Filtered-DCC (FDCC), which represents DCC filtered by a low-pass filter, included with the purpose of reducing the noise, and (4) Level-of-Substance-Over-Time Curve (LSOTC), which represents interpretation of the influence on the distribution of craters shown by FDCC. TPC uniquely corresponds to the computation of TPD, whereas DCC depends on algorithms for computing the elevation of each crater according to the topography, center coordinates, and radius of impact crater, and FDCC relies on the architecture of the custom designed low-pass filter for filtering DCC. However, all variations of DCC and FDCC, which includes the various impact crater data sets, showed a correlation among the density of craters and elevation over 70–80% of the planet surface. Additionally, if we assume that the ocean primarily caused the noted correlation, LSOTC offers a mathematical approach for estimating topographic change of the ocean’s extent over time. Accordingly, TPD is the first new practical application of MTSP to lunar and planetary sciences, showing correlation of topography to a physical process.     

A generalized rough set-based information filling technique for failure analysis of thruster experimental data

Interval-valued data and incomplete data are two key problems for failure analysis of thruster experimental data and have been basically solved by the proposed methods in this paper. Firstly, information data acquired from the simulation and evaluation system formed as intervalvalued information system （IIS） is classified by the interval similarity relation. Then, as an improvement of the classical rough set, a new kind of generalized information entropy called ＂H＇-information entropy＂ is suggested for the measurement of uncertainty and the classification ability of IIS. There is an innovative information filling technique using the properties of H＇-information entropy to replace missing data by some smaller estimation intervals. Finally, an improved method of failure analysis synthesized by the above achievements is presented to classify the thruster experimental data, complete the information, and extract the failure rules. The feasibility and advantage of this method is testified by an actual application of failure analysis, whose performance is evaluated by the quantification of E-condition entropy.     

Photochemistry in Outer Solar System Atmospheres

The photochemistries of the H₂-He atmospheres of the gas giants Jupiter, Saturn and ice giants Uranus and Neptune and Titan’s mildly reducing N₂ atmosphere are reviewed in terms of general chemical and physical principles. The thermochemical furnace regions in the deep atmospheres and the photochemical regions of the giant planets are coupled by vertical mixing to ensure efficient recyling of photochemical products. On Titan,mass loss of hydrogen ensures photochemical evolution of methane into less saturated hydrocarbons. A summary discussion of major dissociation paths and essential chemical reactions is given. The chapter ends with a overview of vertical transport processes in planetary atmospheres.     

IDENTIFICATION OF NONLINEAR PROPERTIES OF AN AIRCRAFT LANDING GEAR SHOCK STRUT

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基于水平集方法的连续体结构拓扑优化方法研究

考虑到现有各种连续体结构拓扑优化方法的优缺点,提出了一种新的连续体结构拓扑优化新策略。该方法将无网格法和水平集方法结合起来,充分发挥各自的优点,使得该拓扑优化新策略具有良好的收敛性和计算精度。