Silver Film Growth on Glass Ceramic by Radio Frequency Magnetron Sputtering

Thin silver films are deposited by radio frequency magnetron sputtering on glass ceramic at room temperature.Variations of sputtering power,bios voltage and power density are carried out for each deposition,then parts of as-deposited samples are subjected to annealing at 600 ℃ within a vacuum chamber.Structural properties are studied by X-ray diffraction(XRD),scanning electron microscope(SEM)and laser scanning confocal microscope(LSCM).It is shown that structural properties have a strong dependency on sputtering power and annealing temperature.Electrical contact resistance measured by a four point probe instrument is directly affected by the thickness of films.It is also found that the film conductivity,especially in thinner films,is improved by the increasing grain size.Finally,the film adhesion is observed by scratch tests.And the adhesive ability deposited by radio frequency magnetron sputtering shows a better performance than that produced by traditional methods.     

Dry Grinding of Titanium Alloy Using Brazed Monolayer cBN Wheels Coated with Graphite Lubricant

The purpose of this study is to investigate the effect of graphite lubricant on the dry grinding performance of Ti-6Al-4Valloy,using graphite-coated,brazed monolayer,cubic boron nitride(cBN)wheels.Brazed monolayer cBN wheels both with and without a coating of polymer-based graphite lubricant are fabricated and subsequently compared for grinding performance based on measurements of grinding temperature,surface microstructure and grinding.In terms of grinding temperature,considerable improvement in dry grinding performance of titanium alloy is achieved using coated brazed monolayer cBN wheels,with 42%—47%reduction in grinding temperature as opposed to uncoated wheels.The grinding force ratio with the coated wheels is observed to remain between 1.45to1.85despite material removal rates reaching up to 1 950mm3/mm.No tangible change in ground titanium surface microstructure is noted as a result of grinding with the graphite coated wheels as opposed to the uncoated ones.     

整体构件周向叶片电解加工流场设计及实验

针对整体构件周向叶片的特点与加工难点,设计了带有内置绝缘腔的电解套型加工工具阴极,建立了两种进液方式的流场三维模型,采用有限元法对两种进液方式的流场进行仿真计算。计算结果表明由绝缘腔的叶盆叶背两侧进液并对出液口进行优化的流场方式较好,电解液流速较高且流场较均匀。使用根据有限元仿真结果设计的阴极开展实验,结果表明实验与流场仿真结果相符,采用优化流场模型的加工过程流场稳定,加工效率较高。     

The influence of orbital maneuver on autonomous orbit determination of an extended satellite navigation constellation

The right ascension of the ascending node is unobservable if only the inter-satellite ranging is used for autonomous orbit determination (AOD) of an Earth navigation constellation. However, if an Earth-Moon libration point satellite is added to the Earth navigation constellation to construct an extended navigation constellation, all the orbital elements can be determined with only the inter-satellite ranging. Furthermore, the extended navigation constellation can provide navigation information for interplanetary probes. For such an extended navigation constellation, orbital control needs to be considered due to the instability of the libration-point satellite orbit. This study concerns the influence of satellite orbital maneuver on the AOD of the extended navigation constellation. An AOD method under orbital maneuver is proposed. A low thrust controller is designed to achieve libration point satellite autonomous orbit maintenance by using AOD results. A navigation constellation consisting of three GPS satellites and one libration point satellite are designed for simulation. The simulation results show that libration point satellites can achieve autonomous navigation and autonomous orbit maintenance by only using inter-satellite ranging information. The rotation drift error of the Earth navigation constellation is also suppressed.     

Attitude stability and periodic attitudes of rigid spacecrafts on the stationary orbits around asteroid 216 Kleopatra

In this work, equilibrium attitude configurations, attitude stability and periodic attitude families are investigated for rigid spacecrafts moving on stationary orbits around asteroid 216 Kleopatra. The polyhedral approach is adopted to formulate the equations of rotational motion. In this dynamical model, six equilibrium attitude configurations with non-zero Euler angles are identified for a spacecraft moving on each stationary orbit. Then the linearized equations of attitude motion at equilibrium attitudes are derived. Based on the linear system, the necessary conditions of stability of equilibrium attitudes are provided, and stability domains on the spacecraft’s characteristic plane are obtained. It is found that the stability domains are distributed in the first and third quadrants of the characteristic plane and the stability domain in the third quadrant is separated into two regions by an unstable belt. Subsequently, we present the linear solution around a stable equilibrium attitude point, indicating that there are three types of elemental periodic attitudes. By means of numerical approaches, three fundamental families of periodic solutions are determined in the full attitude model.     

手机阅读平台发展策略探究

手机阅读是一种新的阅读方式,从开始出现就显现出蓬勃的生命力。中国的三大运营商也对这样的发展势头给予极大的重视,纷纷投入手机阅读的建设中来。随着4G技术的出现,对本来刚刚走向稳定的移动阅读市场带来了新的冲击,三大运营商们在这样的环境下也表现出明显的不足和缺憾,通过一些专业网站的分析调查数据可以看到运营商在移动阅读平台运营上具体的匮乏之处,并通过分析问题找到解决问题的方法。     

低本底α、β测量仪效率校准研究

简述了低本底α、β测量仪效率校准的基本原理,研究了自吸收和面积与探测效率的关系,评定了效率校准中的不确定度,并分析了效率在α、β样品测量中的应用。     

模糊数学在机械工程材料选择中的应用

介绍了模糊数学中的基本概念、隶属函数及模糊评判的基本理论，并首次提出将模糊数学的理论知识、分析方法与人工智能基本理论相结合，并借助于计算机完成机械工程材料的选择，从而使机械工程材料选择更为科学、更为简单。本文还对此方法进行了实例验证，其效果良好，设计者只需输入工作要求，便可以确定出欲选材料的优先次序。     

航空工业企业架构构建方法研究

重点介绍了航空工业企业架构研究的方法体系及研究内容,并重点描述了航空工业业务架构的构建方法,用以提炼航空工业先进业务运作流程、手段与方法,确定了研究推进路线,并进行了成果验证,研究成果对推进航空工业通用业务模式的总结、表达及信息化通用参考模型的设计,信息系统的开发、实施具有指导意义。