Variable stiffness design of redundantly actuated planar rotational parallel mechanisms

Redundantly actuated planar rotational parallel mechanisms (RAPRPMs) adapt to the requirements of robots under different working conditions by changing the antagonistic internal force to tune their stiffness. The geometrical parameters of the mechanism impact the performances of modulating stiffness. Analytical expressions relating stiffness and geometrical parameters of the mechanism were formulated to obtain the necessary conditions of variable stiffness. A novel method of variable stiffness design was presented to optimize the geometrical parameters of the mechanism. The stiffness variation with the internal force was maximized. The dynamic change of stiffness with the dynamic location of the mechanism was minimized, and the robustness of stiff-ness during the motion of the mechanism was ensured. This new approach to variable stiffness design can enable off-line planning of the internal force to avoid the difficulties of on-line control of the internal force.     

从教练机需不需要“超音速”谈现代训练理念

讨论了教练机需不需要超音速、要不要加力等争论问题,基于国外训练理论和实践,对现代军事飞行训练的一些理念进行了总结,并对教练机和训练理念发展新动向进行了介绍。     

挠性杆的镗加工技术

针对挠性杆的结构特点和加工难点,提出了有效的工艺措施,从装夹定位、刀具材料与几何参数选择、刃磨方法、切削用量的选择,以及挠性杆内应力的分析等方面详细地阐述了加工过程中的关键技术,解决了挠性杆镗削加工的技术难题。     

无人机载SAR一体化显控系统的设计研究

阐述了无人机载SAR一体化显控系统的设计,对系统实现中应用到的一些关键技术进行了详细说明,就多位面技术、多线程技术及内存映射技术进行了探讨。     

电磁超介质研究进展

电磁超介质是当前电磁学和物理研究领域中的前沿与热点，文章将左手材料、复合左／右手传输线、光子晶体统一在电磁超介质的体系下进行介绍，并论述了电磁超介质的发展现状。     

扩大斜切式缓冲结构对时速400km铁路隧道口微气压波缓解研究

针对时速400?km高铁隧道口的微气压波研究,建立了基于三维可压缩非定常N?S方程和RNG?k-ε?双方程湍流模型的数值模拟方法,并通过动模型试验对计算方法进行了验证.文中分析了隧道长度、缓冲结构(带斜切的扩大段)长度和缓冲结构开孔数对微气压波的影响.研究结果表明:在一定隧道长度内,微气压波幅值随着隧道长度的增加逐渐增大;隧道口设置带斜切(30°)的等截面扩大段缓冲结构能有效缓解微气压波幅值,且随着缓冲结构的长度增加,微气压波幅值的缓解率先增大后减小,其中缓冲结构长88.56?m时缓解效果最佳,缓解率可达59.2％;该缓冲结构开孔后能进一步缓解微气压波幅值,缓冲结构开2个孔时的缓解效果最佳,缓解率可达70.9％.本文提出的缓冲结构能使得5?km及以下长度隧道的微气压波幅值达到国家规定标准,研究成果对时速400?km/h高速铁路隧道口缓冲结构的设计具有参考价值.     

钛合金精密零件的活性屏离子渗氮

采用活性屏离子渗氮技术对钛合金进行渗氮处理,并将渗氮层的组织、形貌、维氏硬度和零件的变形情况与普通离子氮化的试件作对比。结果表明,活性屏离子氮化的组织和性能优于普通离子氮化,工件变形小、表面光洁度高、操作简单、过程可控、质量一致性好,可以解决钛合金精密零件普通离子氮化存在的问题。     

A data-driven health indicator extraction method for aircraft air conditioning system health monitoring

Prognostics and Health Management (PHM) has become a very important tool in modern commercial aircraft. Considering limited built-in sensing devices on the legacy aircraft model, one of the challenges for airborne system health monitoring is to find an appropriate health indicator that is highly related to the actual degradation state of the system. This paper proposed a novel health indicator extraction method based on the available sensor parameters for the health monitoring of Air Conditioning System (ACS) of a legacy commercial aircraft model. Firstly, a specific Airplane Condition Monitoring System (ACMS) report for ACS health monitoring is defined. Then a non-parametric modeling technique is adopted to calculate the health indicator based on the raw ACMS report data. The proposed method is validated on a single-aisle commercial aircraft widely used for short and medium-haul routes, using more than 6000 ACMS reports collected from a fleet of aircraft during one year. The case study result shows that the proposed health indicator can effectively characterize the degradation state of the ACS, which can provide valuable information for proactive maintenance plan in advance.     

NONLINEAR PREDICTIVE CONTROL FOR TERRAIN FOLLOWING

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