化纤丝束吹风冷却装置研究进展

综述了化纤熔融纺丝冷却吹风装置及丝束冷却过程中冷却风流场仿真的研究进展.讨论了针对吹风装置冷却风不均匀、不稳定、提高丝束质量、降低装置能耗等问题所采取的相关对策与措施.对吹风冷却装置的研究和应用前景进行了展望.     

环锭纺纱线气圈的研究

用圆柱坐标系建立纱线微段的微分方程,用数值方法求解可获得气圈形态及其纱线受力的精确解。用解析方法建立气圈形态及其纱线受力的近似解析表达式,可反映气圈各参数对形态或受力的影响,其分析过程清晰、简捷的特点显著。两种计算结果的相对误差甚微。     

转杯纺杯内纱段捻度分布研究

通过对纱条在假捻盘上的运动和受力分析,对转杯纺杯内的捻度分布进行研究,并得到了杯内捻度分布的一般规律.     

高浓度PAN/DMSO原液粘度特性及纺丝工艺性的研究

在研究了聚丙烯腈／二甲基亚砜纺丝溶液粘度特性的基础上,初步探讨了纺丝液中ＰＡＮ的质量分数与纤维的可牵伸性及致密性的关系。     

三边形圆弧截面空心零件旋压成形数值模拟及试验研究

采用有限元分析软件MSC.MARC对三边形圆弧截面空心零件旋压成形进行数值模拟,对其应力应变分布规律进行了研究,重点研究了旋轮轴向进给比和毛坯厚径比对旋压成形质量的影响,分析了起皱、减薄、回弹现象产生的原因以及容易出现这些缺陷的部位。模拟及试验结果表明,口部（即成形过程中的坯料凸缘）、侧壁靠近圆角处大圆弧区和圆角区域小圆弧部位是三边形圆弧截面空心零件拉深旋压过程中易分别产生起皱、减薄和破裂的部位。     

Study on Airflow Field of Condensing Zone in Compact Spinning System with Perforated Drum

Negative pressure plays a very important role in compact spinning system. To know airflow field and its distribution is helpful to look into the condensing principle of fiber bundle. Therefore, computational fluid dynamics (CFD) software was used to simulate airflow field in this paper. Airflow velocity distributions both in different fiber layers and under different negative pressures were discussed. The results indicate that airflow velocity in upper layer of the fiber bundle is greater than that in lower layer.Airflow velocities in both X and Y axis directions have a positive correlation with negative pressure. It can provide a theoretical base to make high quality compact yarns in productive practice.     

薄壁轴向微沟槽铜管高速旋压成形数值模拟

本文利用有限元分析软件MARC对薄壁轴向微沟槽铜管钢球高速旋压成形过程进行模拟,建立了简化的1/4旋转对称模型,并采用了更新拉格朗日算法和全局网格重划分技术,成功解决了模拟过程中的网格穿透和收敛问题.对薄壁微沟槽铜管的成形特征和残余应力、等效应力应变的分布规律进行了分析.结果表明,成形过程中,金属会出现回弹效应并由此产生凹口等缺陷;等效应力应变及三向应力应变沿轴向呈层状分布,表层应力超过材料应力极限导致铜屑产生,且易出现断管现象;沟槽底部的等效应力应变和残余应力大于齿顶与外表面.过大的残余应力容易造成材料脆化,进而产生粗糙形貌.该研究对优化成形工艺参数,抑制缺陷产生有着重要意义.     

摩擦条件对超薄壁大径厚比屏蔽套旋压过程的影响

建立了Hastelloy-C276材料超薄壁大径厚比屏蔽套的二维正旋仿真模型,应用大型有限元软件MSC.MARC进行了仿真分析,探讨了旋轮与工件以及工件与芯模之间摩擦因数的变化对应力,应变和材料流动的影响规律,并分析了在旋压过程中由于摩擦因数过大而引起的断裂现象,从而为大径厚比,超薄壁屏蔽套的制造方法提供理论指导。     

管式发射巡飞弹的气动特点及设计

讨论了管式发射巡飞弹的气动特点和设计,分析了折叠翼的低雷诺数高升力翼型的气动特性、设计方法以及弹翼的折叠设计,并分析了柔性充气翼的发展、优缺点、气动特性以及目前存在的技术难题.研究结果表明,封装后的充气翼不会破坏机翼结构的整体性,体积降为展开体积的1/10,避开了传统飞行器复杂的折叠结构,质量也大为减轻.分析结果表明充气翼的发展优势以及巡飞弹气动一体化总体设计技术的重要性.     

Stability margin of the quadruped bionic robot with spinning gait

Spinning gait is valuable for quadruped robot, which can be used to avoid obstacles quickly for robot walking in unstructured environment.A kind of bionic flexible body is presented for quadruped robot to perform the spinning gait.The spinning gait can be achieved by coordinated movement of body laterally bending and legs swing, which can improve the mobility of robot walking in the un-structured environments.The coordinated movement relationship between the body and the leg mechanism is presented.The stability of quadruped robot with spinning gait is analyzed based on the center of gravity ( COG) projection method.The effect of different body bending angle on the stabili-ty of quadruped robot with spinning gait is mainly studied.For the quadruped robot walking with spinning gait, during one spinning gait cycle, the supporting polygon and the trajectory of COG pro-jection point under different body bending angle are calculated.Finally, the stability margin of quadruped robot with spinning gait under different body bending angle is determined, which can be used to evaluate reasonableness of spinning gait parameters.