直升机旋翼多层层压黏弹阻尼器多参数动力学建模与分析

针对基于柔性多体系统动力学的直升机旋翼系统动力学建模方法的要求,结合嵌入式多层层压黏弹阻尼器结构特点,建立了基于内变量理论的嵌入式多层层压黏弹阻尼器时域模型.通过引入多层内变量场,改善模型在较宽应变幅值范围和激振频率范围内计算阻尼器动特性及双频激振下动特性的能力.在阻尼器建模过程中考虑了嵌入式多层层压黏弹阻尼器中金属隔片的影响,引入温度传递函数考虑了阻尼器在工作过程中温度上升对黏弹材料的影响,提高了阻尼器模型的精度.通过计算分析与实验结果相比较,验证了阻尼器模型在不同应变幅值、激振频率以及双频激振下的有效性,为直升机旋翼气弹分析计算提供了一种嵌入式多层层压黏弹阻尼器模型.      

一种用于垂直降落重复使用运载器的缓冲器性能分析

以对称分布四腿支柱式垂直降落重复使用运载器为研究对象,基于一种新型油液-蜂窝式多级缓冲器,建立了计及地面弹塑性变形的运载器软着陆过程动力学模型,并给出了运载器着陆时的五种临界着陆工况。以前四种着陆工况为基础对多级缓冲器进行了缓冲参数协调分析,在此基础上以翻倒极限着陆工况为基础重点研究了多级缓冲器缓冲参数对着陆稳定性能的影响。研究表明多级缓冲器中油孔面积、活塞杆直径和阻尼阀调节弹簧预紧力等油液缓冲参数对蜂窝压溃载荷的选取有着显著影响,同时以上参数的合理选择可以有效增加运载器的着陆稳定性能。     

适于时变幅值分析的直升机黏弹减摆器模型

针对现有适于宽幅值范围的黏弹减摆器模型一般含有动幅值参量,不便用于幅值变化的直升机旋翼/机体耦合动稳定性时域分析的问题,给出了小摆振阻尼比时,黏弹减摆器在单频及双频条件下动幅值参量的计算方法,运用该方法计算系统在收敛、中性稳定及发散3种情况下的幅值曲线,较好地反映了响应幅值在时域上的变化趋势。将改进的黏弹减摆器模型用于直升机地面共振非线性时域分析,为准确获取旋翼摆振后退型响应,给出了所需桨叶激振力矩的计算方法,在不同转速不同复模量状态下,采用该方法确定的激振力矩对桨叶进行激振激出的响应幅值与预期值误差不超过6%。对摆振后退型响应进行分析可知,系统稳定时,与线性化结果相比,计入黏弹减摆器非线性后,旋翼摆振后退型响应衰减更快,其模态阻尼在时域上呈增加趋势。      

Rotordynamic characteristics prediction for scallop damper seals using computational fluid dynamics

Enhancing damping characteristic is one of the effective methods to solve the instability problem of the rotor system. The three-dimensional numerical analysis model of scallop damper seal was established, and the effects of inlet pressures, preswirl ratios, rotational speeds, interlaced angles and seal cavity depths on the rotordynamic characteristics of scallop damper seal were studied based on dynamic mesh method and multi-frequencies elliptic whirling model. Results show that the direct stiffness of the scallop damper seal increases with decreasing inlet pressure and increasing rotational speed and cavity depth. When the seal cavity is interlaced by a certain angle, which shows positive direct stiffness. The effective damping of the scallop damper seal increases with the increasing inlet pressure, the decreasing preswirl ratio and the rotational speed and cavity depth. There exists an optimal interlaced angle to maximize the effective damping and the system stability. The leakage of the scallop damper seal is significantly reduced with decreasing inlet pressure. The preswirl will reduce the leakage flowrate, and the rotational speed has a slight effect on the leakage performance. The leakage of the scallop damper seal decreases with increasing seal cavity depth.     

冲击/周期载荷作用下分布式调谐质量阻尼器对响应控制的影响

本文研究了采用分布式调谐质量阻尼器(TMD)对悬臂梁进行振动抑制的问题.首先建立了安装N个TMD的悬臂梁的动力学方程;然后通过有限单元法离散偏微分方程,使用Newmark-β法进行含TMD的悬臂梁动响应求解;最后基于数值计算模型,分别研究周期荷载与冲击荷载作用下,梁振动控制的效果.研究表明:TMD可以有效抑制悬臂梁振动...     

Pressure performance for a thin-walled ring and turbulent-jet orifice modeled elastic squeeze film damper

This paper explores an analytical model for Elastic Ring Squeeze Film Damper (ERSFD) with thin-walled ring and turbulent-jet orifices, and uncovers its Oil Film Pressure Performance (OFPP). Firstly, the ring deformation is addressed by using the Fourier series expansion approach and the orifice outflow rate is characterized with the Prandtl boundary layer theory. Secondly, applying finite difference scheme, the influence of elastic ring flexibility, orifice diameter, and attitude angle on the OFPP is analyzed. Finally, Outer chamber pressure was measured experimentally at different rotor speeds. The results indicate that the outer chamber pressure coats an individual load-carrying region and spreads symmetrically pertaining to the attitude angle. Its amplitude drops as the elastic ring flexibility decreases but boosts with the reduction of the orifice diameter. For inner chamber pressure, the orifice diameter effects a similar trend to the outer cavity, but exhibits more stable distribution regarding the attitude angle. Minimizing the elastic ring flexibility causes an increase in amplitude. The model is validated by the test results giving that the outer chamber pressure shifts synchronously and periodically with the variation of the attitude angle, while the pressure amplitude increases slightly at higher rotor speeds.