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461.
采用真空非自耗电弧炉制备了Nb-22Ti-12Si三元以及三种不同V,Al含量的Nb.Ti-Si-V-Al五元Nb-Si合金,研究了四种合金铸态显微组织和1250℃的抗氧化性能.结果表明:V,Al的加入促进了反应Nb3Si→Nb Nb Nb5Si3,使合金相组成由Nb Nb3Si转变成为Nb Nb5Si3,从而增加了合金中Nb相体积分数;合金的抗氧化性能随V,Al含量的增加而提高;V,Al的加入使合金氧化皮结构发生了转变,生成了较为致密的氧化皮,降低了合金的氧化速率,减少了合金氧化皮的剥落和金属氧化损失量.Nb-21.9 Ti-11.9Si-4.4V-4.1Al经过1250℃/50h氧化后金属损失厚度仅为0.1mm. 相似文献
462.
Zoe A. Landsman Cody D. Schultz Daniel T. Britt Makayla Peppin Ryan L. Kobrick Philip T. Metzger Nina Orlovskaya 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(10):3308-3327
The Martian moon Phobos is the target of the upcoming JAXA Martian Moons eXploration (MMX) mission. There are currently no known samples of Phobos, so spacecraft hardware testing and scientific studies require Phobos regolith simulants. Here, we present two new Phobos regolith simulants: Phobos Captured Asteroid-1 (PCA-1) and Phobos Giant Impact (PGI-1). These two simulants reflect the two hypotheses for Phobos’s formation, and thus the two broad possibilities for composition. This work follows previous efforts to document the development of mineralogically accurate simulants, in an effort to overcome past pitfalls with inappropriate uses of simulants. We report physical and geotechnical properties of PCA-1 and PGI-1, including their reflectance spectra, grain size distributions, abrasivity, cohesion, strength, and hardness. Our intent is for PCA-1 and PGI-1 to be open standards for Phobos simulants, and we present the simulant recipes and production methodology for use and modification by the community. 相似文献
463.
《中国航空学报》2020,33(10):2649-2659
The composite leaf spring landing gear of an electric aircraft is optimized. With the strength and workability as constraints and the minimum structural weight as an objective, the two-stage optimization of the leaf spring landing gear with glass fiber unidirectional prepreg is carried out using a genetic algorithm, namely, the optimization of continuous thickness of layup, and the optimization of the layup sequence and discrete thickness. In the optimization process, the ground loads are calculated according to the structural stiffness of each chromosome, thus the stiffness constraints are relaxed, and the optimization results are compared with those using stiffness constraints. The static experiment verification reveals that the numerical simulation and experimental results are consistent, that is, the optimized leaf spring meets the strength requirements. The results show that the leaf spring landing gear based on two-stage optimization method achieves the objective of weight reduction. 相似文献
464.
465.
柔性自适应桁架及其振动最优控制实验 总被引:16,自引:2,他引:14
基于dSPACE系统和所研制的锆钛酸铅(PZT)压电作动器,建立了第一阶频率低达5Hz的三棱柱自适应桁架实验平台,通过有限元建模和实验参数修正,利用异位加速度反馈信号进行了线性二次型Gauss(LQG)最优反馈控制实验和仿真.结果表明:对比无控状态,采用最优控制只需很小控制电压,可使桁架在低阶典型频率激励下的振幅降低90%以上;而当桁架受扰动后,振动衰减时间减少超过80%;验证了实验平台配置的合理性和所研制的PZT压电作动器、控制模型的有效性;控制数值仿真与实验在加控前后振幅抑制程度相同,控制仿真与实验中振幅衰减过程的差别通过激振过程仿真与实验的对比得到了阐明. 相似文献
466.
阮世勤 《西安航空技术高等专科学校学报》2012,(2):58-60
研究飞机机电维修专业公共英语口语教材的建设。通过对我院飞机机电维修专业的学生进行问卷调查,分析目前公共英语口语教学中口语教材的接受现状以及所存在的问题,指出适用于飞机机电维修专业的英语口语教材应由基础部分和拓展部分组成。对口语教材进行定位,并且提出相应的编撰原则,具有一定借鉴价值。 相似文献
467.
采用精馏橄榄油为模拟物,对PVC食品接触材料中四种己二酸酯类增塑剂向脂类食品模拟物的迁移量进行了检测,并对萃取条件和萃取试剂进行了优化,采用GC—MS技术,通过外标法进行迁移量的检测。研究表明,此方法具有方法简便,重现性好,灵敏度高,定性、定量准确可靠的特点,最低检测限可达5mg/kg,回收率为83.20%~106.13%,标准偏差为1.60%~3.34%,可实际应用于PVC食品接触材料己二酸酯类增塑剂迁移量的检测。 相似文献
468.
469.
Hadj Henni ABDELAZIZ Hassen Ait ATMANE Ismail MECHAB Lakhdar BOUMIA Abdelouahed TOUNSI Adda Bedia El ABBAS 《中国航空学报》2011,24(4):434-448
In this paper, a new displacement based high-order shear deformation theory is introduced for the static response of function-ally graded sandwich plate. Unlike any other theory, the number of unknown functions involved is only four, as against five in case of other shear deformation theories. The theory presented is variationally consistent, has strong similarity with classical plate theory in many aspects, does not require shear correction factor, and gives rise to transverse shear stress variation such that the transverse shear stresses vary parabolically across the thickness satisfying shear stress free surface conditions. Two common types of functionally graded sandwich plates, namely, the sandwich with functionally graded facesheet and homogeneous core and the sandwich with homogeneous facesheet and functionally graded core, are considered. Governing equations are derived from the principle of virtual displacements. The closed-form solution of a simply supported rectangular plate subjected to sinu-soidal loading has been obtained by using the Navier method. The validity of the present theory is investigated by comparing some of the present results with those of the classical, the first-order and the other higher-order theories. It can be concluded that the proposed theory is accurate and simple in solving the static bending behavior of functionally graded sandwich plates. 相似文献
470.
Franz-Josef Ebert 《中国航空学报》2010,23(1):123-136
This article presents an overview of fundamentals of rolling element bearing designs and technologies. The aim is to outline the complex interrelation of all fundamentals with the rolling contact fatigue and the attainable bearing life. Such fundamentals include, amongst others, bearing stressing and life capability. The article shows the different types of rolling bearing stressing and the analysis of the stress distribution (principal stresses and equivalent stresses) in the material under the rolling contact area. It becomes obvious that the contamination of the bearing with foreign particles leads to a drastic reduction in bearing life. Furthermore, it demonstrates the impact of the bearing lubrication and coating as well as the effect of additives on the attainable life and wear. Further fundamentals of rolling element bearing design are the materials, the material cleanliness and the heat treatment. The article reveals the importance of the cleanliness of bearing steels as well as different types of inclusions and their effect on rolling contact fatigue. Additionally the article describes how to optimize the material properties (strength, toughness and residual stress) by the heat treatment processes. The outcome of these investigations is that endurance life of a rolling element bearing can be achieved if specific operating conditions, an adequate lubrication, good system cleanliness and specific bearing stressing are met. The article provides a guideline for bearing engineers on how designs and technologies can be applied to optimizing a bearing for a particular industry or aerospace application. 相似文献