Nonlinear Coupled Dynamics Analysis of A Truss Spar Platform

Accurate prediction of the offshore structure motion response and associate mooring line tension is important in both technical applications and scientific research. In our study, a truss spar platform, operated in Gulf of Mexico, is numerically simulated and analyzed by an in-house numerical code ＇COUPLE＇. Both the platform motion responses and associated mooring line tension are calculated and investigated through a time domain nonlinear coupled dynamic analysis. Satisfactory agreement between the simulation and corresponding field measurements is in general reached, indicating that the numerical code can be used to conduct the time-domain analysis of a truss spar interacting with its mooting and riser system. Based on the comparison between linear and nonlinear results, the relative importance of nonlinearity in predicting the platform motion response and mooring line tensions is assessed and presented. Through the coupled and quasi-static analysis, the importance of the dynamic coupling effect between the platform hull and the mooting/riser system in predicting the mooting line tension and platform motions is quantified. These results may provide essential information pertaining to facilitate the numerical simulation and design of the large scale offshore structures.

Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft:A Survey

Inspired by the integrated guidance and control design for endo-atmospheric aircraft,the integrated position and attitude control of spacecraft has attracted increasing attention and gradually induced a wide variety of study results in last over two decades,fully incorporating control requirements and actuator characteristics of space missions.This paper presents a novel and comprehensive survey to the coupled position and attitude motions of spacecraft from the perspective of dynamics and control.To this end,a systematic analysis is firstly conducted in details to show the position and attitude mutual couplings of spacecraft.Particularly,in terms of the time discrepancy between spacecraft position and attitude motions,space missions can be categorized into two types:space proximity operation and space orbital maneuver.Based on this classification,the studies on the coupled dynamic modeling and the integrated control design for position and attitude motions of spacecraft are sequentially summarized and analyzed.On the one hand,various coupled position and dynamic formulations of spacecraft based on various mathematical tools are reviewed and compared from five aspects,including mission applicability,modeling simplicity,physical clearance,information matching and expansibility.On the other hand,the development of the integrated position and attitude control of spacecraft is analyzed for two space missions,and especially,five distinctive development trends are captured for space operation missions.Finally,insightful prospects on future development of the integrated position and attitude control technology of spacecraft are proposed,pointing out current primary technical issues and possible feasible solutions.

Dynamic model of vertical vehicle-subgrade coupled system under secondary suspension

As it is known, track transportation can be divided into track system above and track system below. While the train is moving, the parts above and below are interacted and influenced. Therefore, in fact, the problem of track transportation is the match between the vehicle and the raihvay line system. In this paper, on a basis of dynamic analysis of the vehicle-subgrade model of vertical coupled system under primary suspension, utilizing track maintenance standard and simulating track irregularity excitation, the dynamic interaction of vehicle-track-subgrade system is researched in theory and dynamic model of the vertical vehicle-track-subgrade coupled system under secondary suspension is established by compatibility condition of deformation. Even this model considers the actual structure of a vehicle, also considers vibration characteristic of the substructure of track including subgrade and foundation. All these work want to be benefit for understanding and design about the dynamic characters of subgrade in high speed railway.

Numerical simulation of aircraft arresting process with an efficient full-scale rigid-flexible coupling dynamic model

The arresting process of carrier-based aircraft is widely recognized as a challenging task,characterized by the highest accident rate among all carrier-based aircraft operations.Dynamic simulation plays a crucial role in assessing the intricate responses of the arresting process,favoring the design of carrier-based aircraft.An efficient and accurate rigid-flexible coupling model for analyzing the dynamic response of the arresting process is proposed.By combining the dynamic characteristics of airframe,landing gear,arresting hook and arresting gear system,the rigid-flexible coupling dynamic model is established to reflect the relative motion of the coupling parts and arresting load.The dynamic model is verified through simulations of landing gear landing drops and by comparing the arresting simulation results with corresponding data in the US military standard.Additionally,simulations of the arresting process under different off-center distance and aircraft yaw angle are conducted to obtain the dynamic response of the aircraft during the arresting process.The result indicates that the rigid-flexible coupling dynamic model proposed is effective for analyzing the arresting dynamics response of carrier-based aircraft.The axial force of the arresting cable on both sides of the hook engagement point,pitch and yaw angle of aircraft are inconsistent under yaw and off-center arresting.The analysis method and obtained results provide valuable references for assessing the dynamic responses of carrier-based aircraft during arresting process and offer valuable in-sights in the design of carrier-based aircraft.

Improved frequency modeling and solution for parallel liquid-filled pipes considering both fluid-structure interaction and structural coupling

The dynamic characteristics of a single liquid-filled pipe have been broadly studied in the previous literature.The parallel liquid-filled pipe(PLFP)system is also widely used in engineering,and its structure is more complex than that of a single pipe.However,there are few reports about the dynamic characteristics of the PLFPs.Therefore,this paper proposes improved frequency modeling and solution for the PLFPs,involving the logical alignment principle and coupled matrix processing.The established model incorporates both the fluid-structure interaction(FSI)and the structural coupling of the PLFPs.The validity of the established model is verified by modal experiments.The effects of some unique parameters on the dynamic characteristics of the PLFPs are discussed.This work provides a feasible method for solving the FSI of multiple pipes in parallel and potential theoretical guidance for the dynamic analysis of the PLFPs in engineering.

井下钻具耦合振动测量模型及实钻数据分析

为了监测井下钻柱的实际振动情况,调整钻进参数来控制井下钻柱的振动特性,从而优化钻进,提高钻速。针对如何通过测量的加速度信号对不同振动形式进行解译与表征的井下振动测量关键问题,建立钻柱振动的解析动力学模型,研究了某种特定振动模式下传感器输出信号的测量,分析了传感器输出信号与钻柱振动模式的关系。通过对模拟信号中振动模式所对应的加速度输出特征进行研究,分析得出实钻数据中所包含的振动信息。为井下振动测量信号的量化分析与运动模式解译提供依据。

浮动基多机悬吊系统动力耦合响应分析

为了研究浮动基多机悬吊系统在不规则波作用下的动力耦合关系,首先利用动量定理和动量矩定理建立了浮动基机器人动力学模型,其次利用达朗贝尔原理建立了悬吊系统的动力学模型,并提出了系统动力学的耦合关系分析步骤;最后结合实例,仿真分析了浮动基多机器人协调悬吊系统在不同波高、不同波长比和不同起吊速度下动力耦合响应过程。结果表明,该系统的理论研究进行了补充和完善,同时也为浮动基多机悬吊系统在实际的吊运过程中,判断安全的吊运环境提供技术支撑。

超大型地下结构系统地震响应高性能弹塑性流固耦合分析

随着城市地下空间开发进行加快,地下结构的抗震安全问题日益受到重视。为了研究饱和土层,尤其是可液化场地中超大型地下结构的地震响应,必须解决高性能计算、弹塑性本构模型、流固耦合等关键问题。该文基于高性能数值仿真平台GEOSX,开发一套高性能弹塑性流固耦合分析方法。以北京城市副中心站综合交通枢纽为例,采用砂土液化大变形模型进行动力弹塑性流固耦合分析,计算规模超千万自由度。计算结果表明,所开发的分析方法具有较高的并行计算效率,可以实现可液化场地地下结构系统的大规模高效弹塑性流固耦合模拟。对于这一主要处于饱和砂土地层中的超大型地下结构系统,在基本地震作用下,饱和砂土层的最大超静孔压比达到约0.5,产生较为明显的弱化;结构地震层间位移角和内力均满足规范要求,由于存在开洞等断面变化,结构响应三维效应明显;由于与地下结构相连的地上结构相对较小,地上结构对地下结构地震响应影响有限。

柔性齿轮运动特性及其振动抑制性能的实验研究

在三缸发动机平衡轴齿轮传动系统的传动过程中,存在着较大的振动和噪声问题,为此,提出了一种附加阻尼环的齿轮传动系统刚柔耦合模型,对柔性齿轮结构的运动特性及其振动抑制性能进行了实验研究。首先,采用集中质量法,建立了考虑齿轮间隙和时变啮合刚度的附加阻尼环6自由度齿轮传动系统的弯曲-扭转模型,利用石川公式计算出了柔性齿轮的时变啮合刚度,对比了有无阻尼环的齿轮系统的振动响应;然后,搭建了专门的齿轮传动系统测试设备,测试了不同转速下钢齿轮和柔性齿轮的加速度和噪声峰值;最后,设计了激光位移试验台,对比分析了不同转速下齿轮的微抖动,对柔性齿轮的减振效果进行了测试,并验证了理论模型的正确性。研究结果表明:当转速为1000 r/min时,钢齿轮和柔性齿轮的最大加速度信号分别为35.58 m/s^(2)和20.37 m/s^(2);当齿轮转速为4000 r/min时,柔性齿轮的阻尼效果最佳,加速度峰值降低了45.23%,噪声峰值降低了39.06%;钢齿轮的微抖动幅值明显高于柔性齿轮,两者的变化趋势相似。柔性齿轮能有效抑制轮齿微抖动振幅曲线的不平滑、毛刺现象,从而增强了三缸发动机平衡轴系的稳定性。

基于全耦合模型的海上吊装作业动力响应特征研究

针对现有海上吊装模拟方法不能有效考虑浮吊船舶—系泊系统—吊物系统之间的动态耦合,难以实现基座回转、吊臂变幅连续模拟问题,基于Matlab/Simulink、ADAMS联合仿真平台建立了海上吊装作业全耦合动力分析模型,探究了中长周期波作用下波浪周期、吊缆收放、基座回转、吊臂变幅等参数变化对吊装作业系统动力响应的影响规律。结果表明,波浪周期接近吊物系统固有周期时会引发共振,导致吊物摇摆幅值显著增加。基座回转、吊臂变幅等因改变了吊物的空间位置从而引发了浮吊船舶倾覆力矩的变化,进而对浮吊船舶运动响应产生显著影响。当基座回转90°后,浮吊船舶的横倾角增加约2.74°。

耦合气阀故障的往复压缩机性能分析

可靠性、容积流量、能耗是评价往复压缩机性能的重要指标,压缩机性能与气阀有着密切关系,气阀工作在高频、高冲击等恶劣条件下,极易损坏,不仅影响压缩机运转率,而且导致指示功增多,排气量减少。因此,通过建立正常工况及气阀故障工况下的往复压缩机数学模型,获取不同工况下的动态压力数据,开展基于动态压力数据的往复压缩机性能分析,对比正常工况与气阀故障工况性能参数,从而获取压缩机机组的气阀故障特征,为之后的故障诊断奠定基础。

锂离子电池组液冷式热管理系统的设计及优化

为了设计一款新的锂离子电池组液冷式热管理系统,建立了锂离子电池组热管理系统试验台架以及该系统耦合电动汽车动力学的一维仿真模型。首先,以试验结果验证了仿真模型的准确性。其次,研究了系统配置参数对电池温度的影响机理;最后,以电池温度不超过32℃和最低的系统功耗作为优化目标,建立多目标优化模型对系统的配置参数进行了优化。结果表明:试验与仿真结果的误差在3.0%内。较高的流量、较低的入口温度、较低的冷却液浓度会降低电池温度,而延迟冷却干预可以降低20%左右的系统功耗,采用响应面法结合MOGA-Ⅱ算法进行多目标优化后,在1.0 C放电倍率时,最高电池温度为30.83℃,并且可进一步将系统功耗降低至2750 W。这说明优化得到的系统最优配置参数方案较好地平衡了电池温度与系统功耗,试验与仿真结合的设计方法为电动汽车锂离子电池组的热管理系统设计提供了参考。

基于水力-热力耦合模型的供热管网优化调度研究

在城市集中供热管网运行过程中,供热系统的输配能耗由水泵能耗和供、回水管网的热损组成,降低供热系统的输配能耗对实现低碳供热目标具有重要意义.本文基于网络图论、流体输配原理和管道的一维传热,建立了集中供热管网的动态水力-热力耦合模型,并针对天津市实际供热管网的运行过程进行了仿真模拟,利用实际运行数据验证了动态水力-热力耦合模型的精确性.建立了集中供热管网输配能耗的计算模型,并对供热系统的运行能耗进行经济性分析.基于所建立的能耗分析模型,结合粒子群优化算法,建立了多热源环状管网的优化调度方法,该方法以供热管网的总输配损耗的成本最低为目标函数,以热源的供水温度、热源泵的转速比、热力站入口处的阀门开度为决策变量,以满足能量守恒和质量守恒为约束条件,通过进行算法参数匹配,给出基于PSO算法的多热源环状供热管网优化调度的计算步骤,并结合天津市实际管网对优化调度方法的调控过程进行了分析.仿真计算结果表明,由于管网存在输配延迟属性,热力站的总负荷变化与室外温度变化不存在静态的正相关性,此外,也发现水泵运行费用为整个管网运行费用的主要组成部分,占总运行费用的58%以上.本研究为城市集中供热管网运行调节的优化提供了一套有效的计算工具.

复杂载荷下大柔性多臂节机械臂架系统刚柔耦合动力学分析

为更加准确地研究复杂载荷下大柔性、多臂节机械臂架系统的动力学特性,提出基于刚柔耦合特性对臂架系统进行动力学仿真分析的方法。首先,根据臂架系统及部件的实际尺寸建立三维模型,并将臂架系统中弹性变形较大的转台,三、四、五节臂架考虑成柔性体;然后,在ANSYS WorkBench中建立臂架系统的刚柔耦合模型并进行仿真分析;最后,通过分析得到关键柔性体部件铰点的载荷受力曲线与臂架系统中柔性体部件的应力云图。分析结果表明:大柔性、多臂节机械臂架系统在设计中考虑柔性体因素进行刚柔耦合分析与工程实际更加相符,也可以更好地为臂架系统的改进与结构优化奠定基础。

OCT内窥镜驱动控制用微型压电马达的机电耦合动力学特性研究

针对光学相干成像技术(optical coherence tomography,OCT)内窥镜驱动控制应用要求,开发设计了直径1 mm、长度5 mm的微型压电马达。利用铁木辛柯梁模型和模态求和法推导马达定子在外部激励电压下的动态响应,结合Hamilton能量变分原理计算得到定子表面质点的模态振动位移和椭圆运动轨迹;进一步利用定转子接触模型和转子力矩平衡原理建立了微型马达的整体机电耦合动力学模型,仿真分析了不同参数对马达力矩-转速,力矩-效率以及负载特性等的影响。试验结果表明,当施加幅值30 V,频率21 kHz的激励电压时,马达转速随负载增加而减小,空载最大转速和力矩分别为400 r/min和2.4 mN·m,满足OCT内窥镜驱动控制应用要求。

高温动压涨圈密封结构参数多目标优化分析

针对航空发动机涨圈密封在高温工况下磨损严重的特性,提出一种动环端面开设螺旋槽的动压涨圈密封。综合考虑切口对主密封端面流动的相互影响,建立流固热耦合数值分析模型,分析动压涨圈密封的密封性能,采用响应面法对静环结构参数进行多目标优化分析,试验验证模型的准确性。研究结果表明:动压涨圈的密封性能主要受切口间隙影响,而减磨性能主要受轴向厚度和径向宽度影响;切口间隙的增大将导致密封性能和减磨性能的下降,但轴向厚度和径向宽度的增加可有效减弱切口间隙的不利影响。优化参数组合为切口间隙0.2 mm、轴向厚度13 mm、径向宽度6.5 mm,优化后泄漏率降低26.73%,密封性能、减磨性能得到明显提升。

海上浮式风机的动力学建模与响应分析

在恶劣的海洋环境下,浮式风机展现出复杂的动力特性。因此,对海上浮式风机的动力响应进行研究非常重要。本文基于有限元法与若丹速度变分原理,建立了浮式风机的刚-柔耦合动力学模型,依此编写了相应的数值计算程序并验证了程序的正确性。以安装在OC4半潜型浮式基础上的NREL-5MW水平轴风机为例,通过对比分析,研究了浮式基础的运动对风机动力特性的影响。结果表明,基础运动通过改变风机在风场中的位置与姿态对气动载荷与叶片变形产生影响。本文研究成果可以为海上浮式风机叶片设计提供一些合理建议。

带非对称阻尼器的柔性支撑框架主余震作用分析

研究主余震耦合作用下具有非对称弹塑性特征的非对称摩擦阻尼器(asymmetrical friction damper, AFD)对柔性支撑框架结构的减震作用。传统扁钢柔性支撑(tension-only brace, TOB)存在松弛问题导致柔性支撑结构在主余震耦合作用下性能严重退化。研究表明:AFD适用于柔性支撑结构,具有非对称弹塑性特征,静摩擦阶段发挥非线性“自拉紧”效应,提供较大的恢复力;在滑动摩擦阶段提供稳定的附加阻尼。该研究对静摩擦阶段和滑动摩擦阶段分别给出了简化模型,对滑动摩擦阶段给出附加阻尼比计算方法,提出了基于AFD的拉紧保护模式和阻尼耗能模式。对比分析柔性支撑框架结构TOB方案和2种AFD方案的主震和主余震耦合弹塑性时程反应,TOB方案在中震主余震及大震主震下屈服,而在大震主余震分析下松弛导致结构破坏,证实柔性支撑结构在主余震耦合作用下存在较大风险;而2种AFD方案可有效保护结构,拉紧保护模式为结构提供更高的减震上限,阻尼耗能模式同样有效防止TOB过度松弛,在主余震作用下提升结构减震性能。

考虑桩基础柔性的固定式海上风力机调谐质量阻尼器参数优化研究

将被动调谐质量阻尼器(TMD)应用于单桩基础海上风力机,以降低风、浪联合作用下风力机塔筒结构动力响应。利用等效桩长法模拟桩基础柔性,将该方法引入气动-水动-伺服-弹性-振动控制风力机仿真程序FAST-SC,建立能考虑桩基础柔性影响的固定式风力机-TMD耦合数值仿真模型。同时,选取固定式海上风力机支撑结构一阶弯曲模态为主模态,并将TMD简化为单自由度体系,基于拉格朗日方程建立简化的单桩海上风力机-TMD耦合模型。基于该简化模型,采用响应面法分别对刚性桩基础和柔性桩基础条件下的海上风力机的TMD参数进行优化。将优化的TMD参数代入所建立的能考虑桩基础柔性影响的海上风力机-TMD耦合数值模型中,对比不同风、浪作用下TMD对采用不同桩基础边界条件的海上风力机减振效果的差异。通过对比得出:不同桩基础边界使得单桩基础海上风力机结构频率不同,所得的最优TMD设计参数也不相同,优化设计后的TMD对风、浪联合作用下柔性桩基础海上风力机的减振效果明显优于刚性桩基础。

采煤机截割部刚柔耦合动力学分析与摇臂优化研究

以MG1000/2500-WD型采煤机为研究对象,根据采煤机截割部基本结构特征,构建采煤机截割部刚柔耦合动力学模型,从转速、加速度、啮合力、应力4个角度开展采煤机截割部仿真分析。根据仿真分析结果,获取采煤机截割部摇臂截割过程中应力云图以及关键点应力曲线,确认采煤机截割部摇臂的受力特点,再以此为基础实施摇臂优化设计,具体设计过程包括摇臂瞬态分析以及摇臂优化设计2部分。为验证所提出采煤机截割部摇臂优化设计的有效性,将优化设计应用于工程实践,最终确认优化设计具有一定的应用价值。