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振动系统结构参数估计的Taylor变换法 被引量:3
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作者 苏志霄 刘宏昭 +1 位作者 李鹏飞 曹惟庆 《应用力学学报》 EI CAS CSCD 北大核心 2000年第1期47-53,共7页
引入了求解非线性微分方程的 Taylor变换法 ,将振动系统原分析模型变换为离散域内的代数方程组 ,建立了估计系统质量、阻尼和刚度矩阵的方程。该方法可以利用任意外载激励下的瞬态响应估计系统的结构参数 ,而不需要进行系统的模态试验 ... 引入了求解非线性微分方程的 Taylor变换法 ,将振动系统原分析模型变换为离散域内的代数方程组 ,建立了估计系统质量、阻尼和刚度矩阵的方程。该方法可以利用任意外载激励下的瞬态响应估计系统的结构参数 ,而不需要进行系统的模态试验 ,具有一定的工程应用价值。文中还研究了测试信号受噪声干扰时的参数估计方法 ,最后给出了 30 0 T转炉倾动机构的参数估计实例。 展开更多
关键词 Taylor变换法 系统结构参数估计 振动系统
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双线阵CCD交汇测量系统结构优化与精度分析 被引量:6
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作者 汪大宝 刘上乾 王会峰 《光学技术》 CAS CSCD 北大核心 2008年第S1期29-31,共3页
双线阵CCD交汇测量系统在检测目标着靶点坐标方面具有十分广泛的应用。在介绍双线阵CCD交汇测量原理的基础上,综合分析了交汇测量精度与系统结构参数之间的关系,建立了相应的数学模型,给出了最优结构参数设计的方法。利用计算机仿真技... 双线阵CCD交汇测量系统在检测目标着靶点坐标方面具有十分广泛的应用。在介绍双线阵CCD交汇测量原理的基础上,综合分析了交汇测量精度与系统结构参数之间的关系,建立了相应的数学模型,给出了最优结构参数设计的方法。利用计算机仿真技术对其进行了分析,得出在相应技术指标要求情况下的最优化系统结构,并给出了靶面坐标测量误差的三维分布图。 展开更多
关键词 交汇测量 系统结构参数 误差分析 结构优化
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降低结构参数对高速凸轮输出响应影响的设计方法 被引量:1
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作者 张家鑫 李树军 《科学技术与工程》 2007年第12期2796-2798,2802,共4页
对高速凸轮进行简单的动力学建模,建立并求解其动力学方程。用正弦加速度运动规律凸轮作为研究对象,并且考虑输入轴速度波动,分析了系统质量、系统刚度这些结构参数对系统输出运动规律的影响。作出输出相应曲线,以此为依据设计凸轮系统。
关键词 高速凸轮 系统结构参数 输入轴速度波动 输出响应
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车用柴油机复合增压系统的模拟计算及验证 被引量:3
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作者 孙万臣 刘巽俊 +1 位作者 刘忠长 李骏 《农业机械学报》 EI CAS CSCD 北大核心 2000年第3期11-14,共4页
应用一维波动模型对一台车用 6缸直喷式柴油机采用脉冲谐振废气涡轮复合增压系统进行了模拟计算 ,模型预测的进气压力波与实测压力波十分吻合。分析了谐振系统结构参数对进气压力波及充量系数的影响 ,发现对于一定的发动机转速 ,充量系... 应用一维波动模型对一台车用 6缸直喷式柴油机采用脉冲谐振废气涡轮复合增压系统进行了模拟计算 ,模型预测的进气压力波与实测压力波十分吻合。分析了谐振系统结构参数对进气压力波及充量系数的影响 ,发现对于一定的发动机转速 ,充量系数达到最大时所对应的谐振管长度比压力波幅值达到最大时对应的长度小0 .15~ 0 .2 5 m。参数优化的谐振进气系统的最大充量系数比不用谐振时提高 6 展开更多
关键词 车用柴油机 涡轮增压 模拟 谐振系统结构参数
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拖式滚动冲击压路机的水平隔振
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作者 林慕义 张洪 《建筑机械》 2000年第3期38-39,共2页
本文建立了拖式滚动冲击压路机水平隔振系统的力学模型,经分析测试提出系统结构参数的选择改进方法。
关键词 隔振 压路机 滚动冲击 系统结构参数
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Investigation on the Optimizing Range of CombustionChamber Configuration Parameters of DSCS 被引量:1
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作者 李向荣 张国栋 魏熔 《Journal of Beijing Institute of Technology》 EI CAS 1998年第2期147-153,共7页
Aim To obtain an optimizing range of the main configuration parameters of double swirls combustion system (DSCS) Methods To analyze the influence of DS combustion cham-ber configuration parameters on fuel spray and mi... Aim To obtain an optimizing range of the main configuration parameters of double swirls combustion system (DSCS) Methods To analyze the influence of DS combustion cham-ber configuration parameters on fuel spray and mixing by means of the fuel jet developmentperiphery charts obtained by the high speed photography with a modeling test device deve-loped by authors,and to examine it by the tests on a single cylinder diesel engine.Resultsand Conclusion The mixing process can be divided into four phases.The optimizing range of the ration of the inner chamber diameter to the cylinder bore,d2/D,is 0.4-0.7; and the outerchamber diameter,d1 the height of the circular ridge to the piston top face,h1,the radius of outer/inner chamber circle,R1,R2 ,the max depth of outer/inner chamber bowl,H1,H2,etc. are also important 展开更多
关键词 diesel engine double swirls combustion system configuration parameter optimizing range
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Probabilistic model and analysis of coupled train-ballasted track-subgrade system with uncertain structural parameters 被引量:5
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作者 MAO Jian-feng XIAO Yuan-jie +2 位作者 YU Zhi-wu Erol TUTUMLUER ZHU Zhi-hui 《Journal of Central South University》 SCIE EI CAS CSCD 2021年第7期2238-2256,共19页
Random dynamic responses caused by the uncertainty of structural parameters of the coupled train-ballasted track-subgrade system under train loading can pose safety concerns to the train operation.This paper introduce... Random dynamic responses caused by the uncertainty of structural parameters of the coupled train-ballasted track-subgrade system under train loading can pose safety concerns to the train operation.This paper introduced a computational model for analyzing probabilistic dynamic responses of three-dimensional(3D)coupled train-ballasted track-subgrade system(TBTSS),where the coupling effects of uncertain rail irregularities,stiffness and damping properties of ballast and subgrade layers were simultaneously considered.The number theoretical method(NTM)was employed to design discrete points for the multi-dimensional stochastic parameters.The time-histories of stochastic dynamic vibrations of the TBSS with systematically uncertain structural parameters were calculated accurately and efficiently by employing the probability density evolution method(PDEM).The model-predicted results were consistent with those by the Monte Carlo simulation method.A sensitivity study was performed to assess the relative importance of those uncertain structural parameters,based on which a case study was presented to explore the stochastic probability evolution mechanism of such train-ballasted track-subgrade system. 展开更多
关键词 coupled train-ballast-subgrade system structural parameter uncertainty stochastic dynamic analysis probability density evolution method wheel-rail interaction
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Effects of Geometric Parameters on Performance of Rectangular Submerged Inlet for Aircraft 被引量:1
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作者 LIU Chao PEI Houju +2 位作者 CHEN Changdong XU Wenbing YANG Kaijie 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2021年第6期984-992,共9页
To improve the comfortability and safety of aircraft,the demand of rectangular submerged inlets(RSIs)with low resistance is proposed to increase the inlet flow rate of ram air. A theoretical model is built to numerica... To improve the comfortability and safety of aircraft,the demand of rectangular submerged inlets(RSIs)with low resistance is proposed to increase the inlet flow rate of ram air. A theoretical model is built to numerically analyze the effects of geometric parameters on the inlet mass flow rate of RSIs. The geometric parameters in question here encompass the aspect ratio of 2—4,the ramp angle of 6°—7°,the characteristic parameter of the throat of 0.20 —0.30,the ramp length of 939—1 337 mm,and the cone angle of 0° —3°. Simulation results demonstrate that the mass flow rate(MFR)is positively correlated with the aspect ratio,ramp angle,ramp length,and cone angle,and negatively correlated with characteristic parameter of the throat. Within the range of the geometric parameters considered,the RSI with the aspect ratio of 3,the ramp angle of 6°,the characteristic parameter of the throat of 0.20,the ramp length of 1 337 mm,and the cone angle of 3° obtains the largest MFR value of about 2.251 kg/s. 展开更多
关键词 ram air system rectangular submerged inlet geometric parameter mass flow rate(MFR)
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Numerical simulation of deepwater deployment for offshore structures with deploying cables 被引量:1
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作者 胡小舟 刘少军 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第3期922-930,共9页
Deepwater deployment of offshore structures in different sea states was investigated. The whole deployment system was modeled as a lumped mass model, and discretization scheme for cable geometry and methodology for ca... Deepwater deployment of offshore structures in different sea states was investigated. The whole deployment system was modeled as a lumped mass model, and discretization scheme for cable geometry and methodology for calculating the internal and external force acting on deploying cable were presented. The deployment model suitable for the time-varying length of deploying cable was specified. The free-surface flow fields together with the ship motions were used to calculate dynamic tension in the deploying cable during deployment of the structure. The deployment of deep sea mining system which was a typical subsea working system was employed. Based on lumped mass analysis model and parameters of deep sea mining system, numerical simulations were performed, and dynamic load and dynamic amplification factor(DAF) with different cable parameters, deploying velocities and sea states were obtained. It is shown that cable parameters and amplitudes of ocean waves can significantly influence the dynamic load and DAF, and the time-varying natural period of deploying system is a dominant factor, while the effect of deploying velocity is not obvious. 展开更多
关键词 deployment cable dynamic load dynamic amplification factor
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Method to avoid the structural interference of the thrust system of a shield tunneling machine
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作者 WANG LinTao SUN Wei +1 位作者 GONG GuoFang YANG HuaYong 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2017年第5期701-712,共12页
Several malfunctions of the shield tunneling machine (STM) caused by structural interference have been encountered in actual tunnel excavation. This paper is focusing on providing an effective method to avoid the st... Several malfunctions of the shield tunneling machine (STM) caused by structural interference have been encountered in actual tunnel excavation. This paper is focusing on providing an effective method to avoid the structural interference based on making the reachable and the required workspaces of the thrust system match each other. The main structure of the thrust mechanism is analyzed, and coordinate systems are built up to describe the pose and workspace of the thrust mechanism. Constraint conditions are derived and the formulation of each constraint condition is carried out to facilitate the analysis of the reachable workspace of the thrust mechanism. Meanwhile, a reachable workspace determination algorithm is introduced based on interval analysis method. The mathematical model for determining the required workspace of the thrust mechanism is presented based on the analysis of the process when the STM excavates along a specific tunnel axis. Two applications are included to show how to avoid these problems by choosing reasonable parameters of the designed tunnel axis and the key structural parameters of the thrust mechanism based on workspace matching. 展开更多
关键词 shield tunneling machine thrust system specific tunnel axis reachable workspace
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CONSTRUCTIONS OF UNITARY SPACE-TIME CODES WITH FULL DIVERSITY
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作者 TONG Hongxi 《Journal of Systems Science & Complexity》 SCIE EI CSCD 2013年第4期650-664,共15页
The problem of constructing unitary space-time codes with high diversity product has been studied in many prior works.Recently,constructions of parametric fully diverse unitary space-time codes for prime number antenn... The problem of constructing unitary space-time codes with high diversity product has been studied in many prior works.Recently,constructions of parametric fully diverse unitary space-time codes for prime number antennas system have been introduced.In this paper,the authors propose new construction methods based on these constructions.And fully diverse codes of any number antennas are obtained from these constructions.Unitary space-time codes from present constructions are found to have better error performance than many best known ones. 展开更多
关键词 Differential space-time modulation diversity products full diversity parametric space-time codes unitary space-time codes.
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Synergistic Performance Management System and Its Associated Structural Model 被引量:3
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作者 Xiaoyong Luo Gang Du Rui Yan Fei Chen 《Journal of Systems Science and Information》 2009年第3期261-267,共7页
Aiming at the widespread issues of synergistic performance management, a conceptual model of synergistic performance management system is built. The order parameter of system synergy and the main factors, as well as t... Aiming at the widespread issues of synergistic performance management, a conceptual model of synergistic performance management system is built. The order parameter of system synergy and the main factors, as well as the degree of synergy and the concept of synergistic effect are proposed. An associated structural model of synergistic performance management system is established based on the method of structural equation modeling. 展开更多
关键词 SYNERGY performance management order parameter degree of synergy synergistic effect
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STATE DERIVATIVE-FREE VARIABLE STRUCTURE MODEL REFERENCE ADAPTIVE CONTROL OF LINEAR PARABOLIC SYSTEMS
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作者 JIA Chaohua SHAO Zhi-Chao 《Journal of Systems Science & Complexity》 SCIE EI CSCD 2013年第6期957-967,共11页
The problem of constructing a model dimensional parabolic system is considered in this reference adaptive control law for an uncertain 1- article. The controller designed here involves only the plant state but no its ... The problem of constructing a model dimensional parabolic system is considered in this reference adaptive control law for an uncertain 1- article. The controller designed here involves only the plant state but no its derivatives. A priori bounds on the plant's uncertain parameters are used to propose switching laws which serve as an adaptive mechanism. The exponential decay to zero of the state error with any prescribed rate is guaranteed by choosing a controller parameter correspondingly. Numerical studies are also presented to illustrate the applicability of the control law. 展开更多
关键词 Distributed parameter systems model reference adaptive control parabolicsystems.
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四氟乙烷弹射无人机试验及仿真
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作者 王志富 姚术健 +2 位作者 鲁寨军 钟睦 王瑞峰 《航空学报》 EI CAS 2024年第21期175-187,共13页
针对传统无人机气动弹射介质压缩空气动力不足的问题,提出使用四氟乙烷代替空气作为气动介质弹射无人机的方法。四氟乙烷安全性高、容易受热发生相变进行膨胀做功,且相比空气具有更高的比热力学能,因此具有更高的膨胀做功能力。通过弹... 针对传统无人机气动弹射介质压缩空气动力不足的问题,提出使用四氟乙烷代替空气作为气动介质弹射无人机的方法。四氟乙烷安全性高、容易受热发生相变进行膨胀做功,且相比空气具有更高的比热力学能,因此具有更高的膨胀做功能力。通过弹射试验验证了四氟乙烷用于弹射无人机的可行性,建立了以四氟乙烷为弹射介质的气动热力学数值模型,模型验证后进行了压缩空气与四氟乙烷弹射能力对比,进一步探讨了高压储气罐容积、阀门直径和低压室容积对四氟乙烷弹射无人机内弹道参数的影响,结论表明:四氟乙烷能够在毫秒级别的时间内将无人机弹射出筒,弹射能力优于压缩空气,能够完成500磅(1磅=0.453 6 kg)质量以上无人机弹射任务;注液密度一定时,随着高压储气罐容积增大,低压室压力、无人机加速度和无人机弹射出筒的速度逐渐增大,但速度增幅逐渐减小,所提算例的高压储气罐容积增大至500 L时,速度增幅接近为0,在满足指标的前提下,减小高压储气罐容积能降低低压室内压力峰值和温度峰值,可保证弹射安全;对于特定的弹射系统,阀门存在一个极限释放直径,超过该直径,无人机弹射速度将不再增加,只会增加加速度峰值;其他参数不变的情况下,适当增大低压室的容积可以有效降低无人机的加速度峰值,且无人机出筒时速度降低较少。 展开更多
关键词 四氟乙烷 无人机 气动弹射 高比热力学能 弹射系统结构参数
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