喷气涡流纺工艺参数对气流场影响的数值计算

通过数值计算的方法研究喷嘴结构参数及喷孔出口速度对喷嘴内部流场流动特征的影响。研究结果表明:喷孔倾角增加,喷嘴轴线负压先增大后减小,倾角为30°时负压最大;切向速度随喷孔倾角的增加而减小,轴向速度随喷孔倾角的增加而增大;喷孔出口速度越大,切向、轴向、径向速度越大,在喷嘴轴线上负压也越大;空心锭外径对喷嘴内气流速度值影响较小,但空心锭外径较小时可使喷嘴轴线上负压增大;随空心锭与喷嘴入口间距的增加,速度场呈减小趋势,喷嘴内部静压减小,喷嘴进口负压增大。     

喷气涡流纺喷嘴内气流流动的二维数值模拟

 为探讨喷嘴内部气流流动特征对纤维加捻成纱的作用,建立计算流体动力学(CFD)模型,对喷气涡流纺喷嘴中的气流流动进行二维数值模拟,并根据计算结果分析喷嘴内高速气流的速度场和压力场分布。模拟结果表明:气流的最大速度可达超音速,由于切向速度所产生的离心力和加捻作用,纤维的尾端从纤维束中分离出来,并旋转加捻到纤维束上,形成具有真捻的纱线;喷嘴入口区域的压力小于外界气压,这有利于由前罗拉钳口处输出的纤维束吸入喷嘴。研究还表明CFD技术是研究喷气涡流纺喷嘴内气流流动的重要手段。     

喷气涡流纺喷嘴参数对内流场特性的影响

为探究高速气流在喷气涡流纺内流道的流场特性规律,课题组基于FLUENT建立喷嘴的参数化模型,采用单一变量法分别研究喷孔数量、喷孔倾角和供气压力对喷嘴内流场的影响。结果表明：受引导部件的影响,内流场气流特性分别存在不规则性,且有较多的回流和涡流现象的存在;随着喷孔数量的增加,喷孔出口气流速度略有增大,内流场涡流现象减少,气流旋转性能显著增强;随着喷孔倾角的增大,气流速度峰值先增大后减小,导引部件螺旋面两侧的轴向速度和切向速度分布有明显不同,而当喷孔倾角超过70°后角度对速度的影响逐渐减弱;随供气压力的增加,气流速度增大,气流旋转特性增强,纱线加捻效果有所提高。该研究对于喷气涡流纺喷嘴的结构设计具有参考价值。     

喷嘴参数对喷气涡流纺内流场特性的影响研究

为明确喷气涡流纺纱的纺纱机理,研究喷嘴中喷孔数量、喷孔倾角和供气压力对喷气涡流纺内流场的影响情况,文章采用Fluent软件进行喷气涡流纺的内流场模拟分析.通过结果对比分析发现:喷孔数量和供气压力对喷嘴内流场的气流旋转运动影响较为显著,随着喷孔数量和供气压力的增加,喷嘴内气流的旋转运动显著增强,对纱线自由端纤维的加捻效果...     

喷气涡流纺纱线细节产生机制分析

通过数值计算对喷气涡流纺喷嘴内部流场衰减规律进行探讨。讨论加捻腔中纤维的受力情况及涡流作用下的运动状况;建立倒伏在空心锭上的纤维自由端绕空心锭旋转的临界角速度与进入纱尾的纤维头端长度、纤维半径等参数间的函数关系,以临界角速度作为衡量纤维头端是否被抽拔的依据,解释喷气涡流纺落纤、成纱细节产生的原因。临界角速度随进入纱尾纤维头端长度的增加而增大;纤维半径越大,临界角速度越小,在同一喷嘴气压下,半径大的纤维纺纱时落纤、成纱细节较多;增加喷嘴气压对成纱强力有利,超过某临界值落纤、成纱细节增加,对成纱质量不利;增加喷嘴内部负压,适当减小前罗拉与空心锭的距离可减少落纤、细节的产生。     

喷气涡流纺喷嘴喷孔参数的分析

喷气涡流纺是利用喷嘴内高速气流的旋转对纤维加捻成纱的设备,为了分析喷嘴的结构参数对成纱质量的影响,选择喷嘴的喷孔直径d为0.5 mm,分别在不同喷孔数量n(5,6)及不同喷孔角度θ(60°,65°,70°,75°,80°)下,在新型涡流纺纱机上对粘胶原料进行纺纱实验。实验结果得到了喷孔最优结构参数:喷孔孔径×数量φ0.5×5;喷孔角度70°。     

喷气涡流纺喷嘴内部三维流场的数值研究

采用3D CFD建立喷气涡流纺喷嘴结构模型,应用Fluent 6.2流体计算软件对模型内气流场进行数值模拟,表征了喷嘴内部三维流场的流动状态,解析了喷嘴内气流流场的压力场和速度场分布,分析了流场与成纱机制的相关关系。研究表明:压缩气流经喷孔后在喷嘴内形成三维旋转气流,切向、轴向气流速度分布符合旋转气流理论;切向气流对边缘自由端纤维加捻,轴向气流对纤维束的牵伸作用可忽略,径向气流对纤维束起膨胀作用,在切向气流作用下获得更多的包缠纤维;喷嘴内部静压呈U形分布;边缘自由端纤维在不同位置加捻程度的差异导致纱线捻度不匀。     

喷气纺纱喷嘴对纱线强力影响的研究和探讨

喷气纺纱是继转杯纺纱(气流纺纱)、自捻纺纱、涡流纺纱之后发展起来的一种新型纺纱方法。它利用高速旋转气流来推动须条形成高速旋转的气圈运动，经固定喷嘴加捻成纱的。但是，喷气纱强力较低一直是喷气纺纱进一步发展的瓶颈。本文探讨了喷气纺纱喷嘴的主要结构参数对喷气纱强力的影响,并通过大量试验和科学计算优化出较理想的喷嘴结构参数，使纺出的涤棉混纺纱达到同类环锭纱强力的90％以上。     

空心锭结构参数对喷气涡流纺内流场的影响

为研究空心锭外圆锥面上斜孔结构对喷气涡流纺成纱性能的影响,采用Solidworks建立了加捻腔的三维CAD模型,利用Fluent 15建立了加捻腔的流体计算力学模型,并进行了流场仿真,研究了流场的气流流动特性以及压力场、速度场的分布规律。结果表明:气流经喷孔喷出后以螺旋状推进,加捻腔内部静压场呈现U型分布;在靠近空心锭入口处存在负压,有利于纤维加捻后吸入空心锭内;空心锭外圆锥面上开通的斜孔有利于增加纤维输出时的轴向速度并且能够有效减缓轴向速度减小的趋势;斜孔角度对纤维进入加捻腔时的轴向速度起到一定的影响,轴向速度随斜孔角度的增加存在先增大后减小的趋势;斜孔能够提高纤维的加捻效果,改善成纱性能。     

传统型与自捻型喷气涡流纺的对比

针对喷气涡流纺纱技术气流加捻过程中落纤率较高导致纱线细节较多以及纱线结构中芯纤维平行伸直导致纱线强力较低的问题,提出自捻型喷气涡流纺纱技术,依据动摩擦原理,采用镭射激光加工处理,增大自由端纤维与空心锭接触面之间的动摩擦力,实现纤维在空心锭表面旋转运动过程中自身发生扭转后包缠到纱线中,增大纤维间的抱合力。同时基于流体力学模拟和样纱试纺实验,对比分析了传统型喷气涡流纺和自捻型喷气涡流纺空心锭结构参数、喷嘴内部近壁面处的流场特征和纱线结构性能,验证了自捻型喷气涡流纺纱技术的可行性。     

Numerical and experimental research on the influence of parameters on the tensile properties of Murata vortex yarn

In this paper, a three‐dimensional numerical simulation is presented on the flow field inside the nozzle of Murata vortex spinning. Four parameters; nozzle pressure; jet orifice angle, twisting surface angle, and distance between the nozzle inlet and the spindle, are selected to investigate their influences on the airflow characteristics in the nozzle and, consequently, on yarn tensile properties. Experimental research is also conducted to investigate the influence of these parameters on the yarn tensile property. The computational results are compared with the experimental results and they are in good agreement. The research shows that with the increase of the nozzle pressure and the twisting surface angle, the yarn tenacity first increases and then decreases. Yarn tenacity increases with increasing jet orifice angle. Yarn tenacity decreases with the increasing distance between the nozzle inlet and the spindle.     

涡流纺纱中纺纱腔内气流结构数值模拟

 利用Fluent软件对涡流纺纱中流场进行了三维动力学模型仿真,研究了进气喷嘴、纺纱腔与空心锭子之间间隙、出口负压强度等参数对纺纱腔内气流结构的影响,并讨论其对纱线特性的影响。研究结果显示：在流量相同情况下,纺纱腔内涡流强度和均匀性与进气喷嘴方向及数量、纺纱腔与空心锭子间隙等相关。进气喷嘴轴线方向越接近纺纱腔横截面方向、纺纱腔与空心锭子间隙越小,涡流强度越大,而进气喷嘴数量越多,涡流形态越均匀稳定;间隙出口负压强度决定纺纱腔内轴向气流速度,该参数由纱线种类及其特性决定。     

基于螺旋导引槽空心锭子的喷气涡流纺加捻腔流场模拟

针对喷气涡流纺纺纱过程中存在的成纱强力偏低的问题,提出一种基于螺旋导引槽空心锭子以提高成纱强力的方法。通过数值模拟的方法,研究基于螺旋导引槽空心锭子的加捻腔气流场流动特征,验证螺旋导引槽空心锭子结构对成纱性能的改善作用。结果表明：空心锭子外表面的螺旋导引槽可以引导气流流动,使自由尾端纤维的加捻作用增强;此外,螺旋导引槽结构的存在,导致槽内外气流的静压和速度存在差异,引起自由尾端纤维的内外转移,并产生自捻效应,可进一步实现喷气涡流纺纱线强力的提高。     

A numerical and experimental study on the effect of the orifice angle of vortex tube in vortex spinning machine

In order to study the effect of orifice angle of vortex tube on yarn forming in jet vortex spinning, eight levels of nozzle angle are designed, from 40° to 65°, and the corresponding three-dimensional computational fluid dynamics (CFD) models are established to conduct the numerical simulation of the airflow in the nozzle. Through the analysis of numerical simulation, the pressure and velocity distribution are made clear which provides reference for the future design of the vortex tube. Simulation results show that when the orifice angle is around 50°, the airflow state within the nozzle has a large negative pressure with appropriate axial and tangential velocity, which is conducive to the formation of the open ends of fibers and twisting, and the yarn quality is better. Spinning experiment results prove that single yarn strength is the maximum, the irregularity of single yarn strength is the minimum, and other yarn properties are superior with the orifice angle at 50°, which shows a good agreement with the simulation results.     

Effect of the distance between jet orifice and nozzle Alex on properties of vortex spun yarn

This study focuses on the effect of various distances between the jet orifice and the nozzle Alex on the properties of the vortex spun yarn. Four levels of the distance are designed within certain range. Building three-dimensional computational fluid dynamics models, we use the method of numerical simulation to calculate the inner fluid field of nozzle. The results showed that the distance typically affected the airflow movements, particularly in tangential velocity, and the smaller d is beneficial to diffuse the airflow uniformly and to improve the quality of vortex spun yarn. The corresponding experiments have been carried out. In this paper, 100% viscose drawing slivers are spun into vortex spun yarn, and their physical properties are tested. Spinning experiment results prove that when the distance is minimum under the condition of avoiding the high-speed airflow shooting out from the jet orifices colliding with the cone body, the yarn strength reaches the maximum value, while the unevenness of breaking strength meets the minimum, and the other yarn properties are superior, which shows a good agreement with the simulation results.