铝合金构件的原位快速表面处理方法研究

着重探讨了在外场操作条件下，对航空铝材进行原位、快速表面处理的几种方法以及不同表面处理对粘接效果的影响。结果表明：对受损的通用航空铝合金(LY12-CZ)表面，采用自行研制的酸膏进行氧化处理，能造就具有一定特征形貌的铝合金表面氧化层，从而使粘接强度提高76．0％，并可实现对构件表面的快速、原位处理，能满足装备构件外场修复的基本要求。     

硝胺推进剂界面键合的表征研究

从红外光谱分析，表面（界面）自由能测定、光电子能谱分析等方面，研究了键合剂，包覆固体填料颗粒对界面增强的效果，并与静态力学性能的数据进行了对比，结果表明；取代酰胺类键合剂对ＨＭＸ间的作用力为氢键。效果倨于醇胺，多元胺类化合物，其中一种键合剂对ＨＭＸ的浸润可以在热力学和动力学两方面达到较好的统一，键合效果并不仅仅取决于包覆度的大小，还与键合剂附着在ＨＭＸ表面上形成的界面层或预包覆层的性质有关。     

Remote estimation of the structure of the surface layer of Mercury

Results of the optical observations of Mercury and the Moon confirm the close similarity of photometric properties of the bodies. Undoubtedly, the surface of Mercury, which is subjected to the same processes, is covered by a mantle of shattered rocks – the regolith. The structure of the reflecting layer determines the photometric and polarization characteristics of the surface of a planetary body. Despite the general similarity of the integral optical properties of the surfaces of Mercury and the Moon, specific characteristics of the media of these celestial bodies manifest themselves as identifiable differences in the details of the measured parameters: Mercury’s regolith is smoother than of the Moon, probably contains a greater fines fraction, and has greater maturity.     

测量超光滑表面粗糙度参数的反散射计算研究

介绍一种高分辨力、无接触式测量超光滑表面粗糙度参数的反散射计算测量技术。实现该技术的测量装置的角分辨力为0.1°。它可以测量导体或非导体表面纳米级精确度的粗糙度。     

镜反射凹面及相互可视表面的轨道外热流计算

通过对空间表面所受外热流以及镜反射表面所具有的特性的分析，提出了采用蒙特卡罗法计算镜反射凹面及镜反射相互可视表面的轨道热流的方法，并对半球凹面和两相互垂直可视平板的轨道热流进行了计算。     

表面组装技术和片状元件在空间应用的可能性

文章简单介绍了表面组装技术和片状元件的概况;结合卫星的特点,阐明了表面组装技术和片状元件在空间电子设备中应用的必要性和可能性。     

基于特征的参数化设计方法

从集成角度,分析了特征定义及信息构成,并采用层次结构表达特征信息。在此基础上提出特征最小构成单元特征面,通过附着面特征之间发生联系。在参数化造型时,以尺寸驱动方式修改特征形状与定位,提出用局部坐标架网表示特征之间位置依赖关系,最后,提出运用面向对象方法组织特征信息。     

Thermoelastohydrodynamic analysis of misaligned bearings with texture on journal surface under high-speed and heavy-load conditions

Hydrodynamic journal bearings are used to support the planetary gears in the transmission system of a Geared Turbo Fan engine, and they operate under severe working conditions, such as misalignment, high speed, and heavy load. Surface texture is regarded as an effective approach to improve mechanical properties under severe working conditions. However, the effects of surface texture on misaligned journal bearings under severe conditions have not been well studied. Therefore, a thermoelastohydrodynamic(TEHD) lubricating model with a textured and misaligned journal is presented in this study. Solid deformation, heat transfer between oil and the bearing, and heat convection between air and the bearing are considered in the model. The effects of cavitation and viscosity-temperature are also taken into account. The impacts of surface texture parameters and the misalignment angle on lubricating properties are investigated in the model. Results indicate that the bearing lubricating performance is greatly improved by optimal surface texture considering journal misalignment. The maximum oil film pressure and load-carrying capacity of a journal bearing increase with journal misalignment. Meanwhile, the oil film temperature increases sharply while considering misalignment.     

Experimental study of effect of post processing on fracture toughness and fatigue crack growth performance of selective laser melting Ti-6Al-4V

For Ti-6Al-4V, a titanium alloy increasingly used in aerospace structure, selective laser melting (SLM) is an attractive additive manufacturing technology, which is attributed to its complex construction capability with high accuracy and good surface quality. In order to obtain qualified mechanical properties, SLM parameters and post processing should be tailored for diverse service conditions. Fracture toughness and fatigue crack growth (FCG) behavior are critical characteristics for damage tolerance evaluation of such metallic structures, and they are affected by post processing technologies significantly. The objective of this study is to obtain the fracture toughness and fatigue crack growth behavior of Ti-6Al-4V manufactured by SLM, and to evaluate the influence of post-SLM thermomechanical treatment and surface machining. Fracture toughness and FCG tests were performed for SLM Ti-6Al-4V in three types of post processing status: as-built, heat treated and hot isostatically pressed (HIPed), respectively. Specimens with as-built and machined surface were tested. The microstructure and fractography were analyzed as well in order to investigate the relevance among manufacture process, microstructure and mechanical properties. The results demonstrate that as-built SLM Ti-6Al-4V presents poor ductility and FCG behavior due to martensitic microstructure and residual stresses. Both heat treatment and hot isostatic pressing improve the plane-stress fracture toughness and FCG performance considerably, while surface machining shows slight effect.     

星用介质材料表面充放电效应试验研究

航天器表面介质材料易遭受表面充放电危害。利用30keV单能电子对几种不同的航天介质材料进行了表面充放电模拟试验,测量了不同电子通量辐照下的表面充电电位以及放电脉冲。试验结果表明,聚酰亚胺薄膜在接地处理不当时表面可充至千伏以上,易发生表面放电,且辐照强度越大,放电频率越高。表面镀铝的聚酰亚胺薄膜在不接地时,铝膜成为悬浮导体更加剧了放电的危害。而通过渗碳处理的聚酰亚胺薄膜,其良好的导电性能可有效抵御nA/cm~2量级电子的表面充电。聚四氟乙烯天线罩表面未进行防静电处理时,表面充电电位可达万伏量级,极易发生放电。