摘要：Kirigami arts have provided a more promising method for building multiscale structures,which can shape two-dimensional(2D)sheets into three-dimensional(3D)configurations by cutting and ***,we first carried out a theoretical analysis of the mechanical properties of 2D honeycomb lattice structures and experimental verification combined with finite element(FE)***,a series of thick-walled 3D kirigami-inspired honeycomb(TW3KH)structures with different mechanical properties were designed and fabricated on the exploration and optimization of geometric parameters of 2D honeycomb *** investigations of folding feasibility,self-expansion,and self-folding performance experimentally showed that our designed four-dimensional(4D)printing structure had good programmability and shape memory capability and a large volume change ratio during shape ***,research on its compression deformation behavior found that the TW3KH structures can recover load-bearing capacity very well when the angle is ***,these TW3KH structures have great advantages in space-saving smart load-bearing equipment.

摘要：The deployable structures based on shape memory polymer com-posites(SMPCs)have been developed for its unique properties,such as high reliability,low-cost,lightweight,and self-deployment without complex mechanical devices compared with traditional deployable *** order to increase the inflatable structure system’s robustness and light the weight of it,a cubic deployable support structure based on SMPC is designed and analyzed *** cubic deployable support structure based on SMPC consists of four dependent spatial cages,each spatial cage is composed of 12 three-longeron SMPC truss booms and end *** shape recovery of arc-shaped deployable laminates drive the three-longeron SMPC truss booms to unfold,thus realize the expansion of the deployable support *** concept and operation of the cubic deployable support structure are described in detail.A series of experiments are performed on the three-longeron deployable laminates unit and the simplified cubic deployable support structure to investigate the shape recovery behavior in the deployment *** indicate that the cubic deployable support structure has a high deployment-tgo-stowage volume ratio and can achieve self-deployment,package,and deploy without complex mechanical devices.

摘要：应用多材料常数的Ogden弹性应变能函数分析了介电弹性体的力学行为,研究了介电弹性体的机电稳定性.数值结果表明,通过对材料系数(如材料常数比和电致伸缩系数等)的恰当调节可以使得介电弹性体材料或介电弹性体结构更趋稳定.这些有益于深入理解介电弹性体的机电稳定性行为,进而设计恰当的介电弹性体器件.

摘要：机翼翼尖对飞行器的气动性能和操控性能有重要影响,在起飞、爬升、巡航、下降等不同飞行阶段,飞行器对机翼翼尖几何参数有不同需求。变翼尖机翼技术是一种多功能、局部变体技术,可用于提升机翼气动性能、提高燃油效率、减轻阵风载荷、强化操控性能等用途。从气动特性、结构响应和操控特性3方面,对变翼尖机翼技术效益进行梳理,从翼尖变形形式、材料与结构组成2个角度,展开对变翼尖机翼技术研究现状的讨论,指出变翼尖机翼技术正在向多功能集成、组合变形和智能化方向发展。提出变翼尖机翼技术亟需解决的4项关键技术,即全局气动优化、变形/承载一体化蒙皮技术、高效驱动系统设计、智能控制技术,分析了各项关键技术的技术特点和研究难点。变翼尖机翼关键技术若得到突破,相关技术将可以移植应用到全局变体飞行器技术中。

摘要：Synchrotron radiation X-ray micro-computed tomography(SR-μCT)is a 3D imaging technique that is widely employed for the characterization of defects in advanced materials and *** this study,we characterize several typical defects in octettruss and re-entrant 3D lattice structures by using SR-μ*** 3D micro-lattice structures are manufactured using projection micro litho stereo exposure(PμLSE)additive manufacturing *** as-fabricated 3D lattice samples are characterized using optical microscopy,and subsequently,by SR-μ*** more,a statistical analysis is performed to characterize the surface roughness and internal defects qualitatively,whereby the statistical geometrical parameters of struts along different directions and strut joints are analyzed and ***,several typical defects are identified:(1)holes at the joints of the strut and irregular diameter deviations of the strut in the octet-truss lattice structure;(2)irregular diameter variations,bulges,dislocations,grooves,accumulations,and torsion in the re-entrant lattice *** of these defects are related to the building direction,the weight of the structure,bubbles,dust,and impurities during the PμLSE additive manufacturing process.

摘要：为了降低压电旋转驱动器的成本,提高承载能力,实现分辨率可调,设计研制一种新型压电旋转驱动器。驱动器采用单个压电堆栈作为原动件,经二级位移放大机构将压电堆栈的变形进行放大,再通过运动转换将放大后的直线运动转化为棘轮转子的旋转转动。制作了压电旋转驱动器样机,对其进行试验测试。试验结果表明:驱动器的输出转角具有很好的可控性,当驱动电压分别为200 V、350 V和650 V时,可获得三种稳定的单步输出转角,旋转分辨率为0.034 9 rad,最大承载扭矩为0.392 N·m。频率为20 Hz时,最大运转速度为2.094 4 rad/s。该驱动器在降低成本的同时,还具有分辨率可调、运转速度较高和承载能力强的优点,在精密驱动和大转角驱动领域有较大的应用潜力。

摘要：软体机器人由于其内在的高度的灵活性、良好的顺应性、出色的适应性和自然安全的可交互性,在医疗、教育、服务、救援、探索、探测、可穿戴设备等领域越来越受到重视,并显示出巨大的发展潜力.气动软体机器人由于重量轻、效率高、无污染、环境适应性强等特点在软体机器人领域占据了重要地位.同时,气动软体机器人技术的发展与新材料、新设计和新工艺的应用密不可分.本文首先从驱动器结构设计、制作工艺综述了气动软体机器人的研究现状与主要进展,而后对软体机器人的多功能化、模块化以及仿生学设计趋势进行了分析和讨论.并对气动软体机器人在系统可靠性、气源供给和运动控制方面研究面临的问题和挑战进行了相关分析和讨论,最后对气动软体机器人的未来发展方向和意义进行了展望和总结.

摘要：变体飞行器可以根据不同的飞行条件改变自身形状以获得最优的气动性能,大大提高飞行器的综合性能,是未来飞行器发展的重要方向之一。新型智能材料和结构具有驱动、变形、承载、传感等特点,为变体飞行器的设计提供了新的技术途径。本文根据不同可变形机翼结构分类,详细阐述了智能材料和结构在自适应结构、智能驱动器和变形蒙皮等方面的研究现状。变体飞行器的实现亟需解决变形/承载一体化蒙皮技术、轻质大输出力驱动器技术和自适应结构技术等关键技术,本文还对智能材料和结构未来在变体飞行器上的应用前景进行了展望。

摘要：建立了压电纤维复合材料桨叶的非线性动力学模型。在此基础上,研究了压电纤维铺层对复合材料桨叶固有频率和桨叶扭转运动阻尼特性的影响。计算结果表明:桨叶扭转角变化量随着压电纤维施加电压的增加而增大;当电压为1000 V时,桨尖扭转角变化量大约为2°。压电纤维铺层对桨叶固有频率几乎没有影响,其存在不会改变原设计复合材料桨叶的频率分布。当压电纤维铺设方向与桨叶展向成45°时,其对桨叶扭转方向的阻尼特性有着很大的影响;采用适当的电压控制,可以明显增加扭转方向的阻尼。

摘要：为了探索可变形飞行器气动、结构和控制关键技术,在可变后掠角及展长的翼身组合体风洞试验模型系统设计与特性分析方面开展了研究。系统设计包括总体方案设计、近似理论分析与计算流体力学(CFD)数值模拟、结构与控制技术集成;特性分析包括结构特性、控制特性、定常与非定常气动特性的测试及其分析。结果表明:大尺度变形能显著改变飞行器的升力、阻力和升阻比等气动特性,进而使可变形飞行器能适应多种环境和任务,因而在全飞行周期中比传统固定外形飞行器具有更优的性能。