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管道模型瞬态动力分析间隙刚度取值研究 被引量:2
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作者 黄文慧 李朋洲 +1 位作者 陈学德 李锡华 《核动力工程》 EI CAS CSCD 北大核心 2016年第S2期103-106,共4页
建立与模型结构的非线性边界条件(间隙)相符合的数学模型,应用试验中测量得到的冲击台面上管道模型支承处的加速度时程作为输入载荷,采用ANSYS大型通用有限元程序,进行一系列的几何非线性瞬态动力时程分析,计算管道模型在冲击载荷作用... 建立与模型结构的非线性边界条件(间隙)相符合的数学模型,应用试验中测量得到的冲击台面上管道模型支承处的加速度时程作为输入载荷,采用ANSYS大型通用有限元程序,进行一系列的几何非线性瞬态动力时程分析,计算管道模型在冲击载荷作用下的非线性动力响应,将计算结果与试验的测量值进行比较。通过对各种计算方案的几何非线性冲击动力瞬态时程计算分析结果与试验的测量值之间的分析比较,探索支承间隙的合理模拟方法。 展开更多
关键词 管道模型 瞬态分析 间隙刚度
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迎角对间隙舵面的非线性颤振特性影响研究 被引量:5
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作者 张伟伟 王忠波 +1 位作者 叶正寅 杨永年 《机械强度》 CAS CSCD 北大核心 2011年第2期296-301,共6页
针对典型超音速舵面,采用基于CFD(computational fluid dynamic)技术的当地流活塞理论计算气动载荷,运用等效线化方法分析带有间隙非线性的舵面颤振特性。研究飞行迎角和舵面间隙大小对系统极限环颤振特性的影响规律。计算结果表明,适... 针对典型超音速舵面,采用基于CFD(computational fluid dynamic)技术的当地流活塞理论计算气动载荷,运用等效线化方法分析带有间隙非线性的舵面颤振特性。研究飞行迎角和舵面间隙大小对系统极限环颤振特性的影响规律。计算结果表明,适当赋予一定的气动预载荷、减小间隙大小等措施,可以提高带有间隙舵面的气动弹性稳定性。对于该舵面模型而言,无间隙颤振速度和舵面间隙大小满足国军标要求时,有间隙舵面在实际飞行中不会发生破坏性颤振,只在0°迎角情况下才会出现微幅极限环运动。 展开更多
关键词 颤振 气动弹性 间隙非线性刚度 当量线化 当地流活塞理论
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外部激励对齿轮系统非线性振动的影响 被引量:1
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作者 张琛 翁建生 《轻型汽车技术》 2013年第4期28-30,共3页
以齿轮非线性动力学理论为基础,建立了包含时变刚度和齿侧间隙的单对齿轮副系统模型。利用数值仿真法得到系统在不同外界激励下的时间历程曲线和幅频响应曲线。分析表明,随着外部激励幅值的增大,系统的振动幅值也逐渐增大。同时,系统出... 以齿轮非线性动力学理论为基础,建立了包含时变刚度和齿侧间隙的单对齿轮副系统模型。利用数值仿真法得到系统在不同外界激励下的时间历程曲线和幅频响应曲线。分析表明,随着外部激励幅值的增大,系统的振动幅值也逐渐增大。同时,系统出现了除主频之外的其他频率分量,系统的振动特性趋于复杂。 展开更多
关键词 时变刚度间隙非线性外部激励
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Simulation and Experimental Research for Piping Damper with Plunger-type Accumulator
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作者 罗小辉 胡军华 +1 位作者 王晓斌 牛子华 《Journal of Marine Science and Application》 2010年第3期274-279,共6页
It can be beneficial to reduce vibrations in shipboard piping, so the authors designed a new kind of piping damper with a plunger-type accumulator.Special requirements for the piping damper included low impact displac... It can be beneficial to reduce vibrations in shipboard piping, so the authors designed a new kind of piping damper with a plunger-type accumulator.Special requirements for the piping damper included low impact displacement, low speed, as well as an appropriate locking speed.Inside the damper, a plunger-type accumulator was installed and on the outside of the piston rod, a tube with exposed corrugations was added.Between the piston and the cylinder, a clearance seal was added.Using mathematical modeling, the effects of the dynamic performance of the damper's impact displacement on vibrations were observed.Changes to the clearance between the piston and the cylinder, the stiffness of the spring in the accumulator, the throttle valve size, and locking speed resistance of the damper were respectively simulated and studied.Based on the results of the simulation, dampers with optimal parameters were developed and tested with different accumulator spring stiffnesses and different throttles.The simulation and experimental results showed that parameters such as seal clearance between piston and cylinder, accumulator spring stiffness and throttle parameters have significant effects on the damper's impact displacement, low speed resistance and locking speed. 展开更多
关键词 plunger-type accumulator piping damper impact displacement low speed resistance locking sneed
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Nonlinear Dynamic Analysis of Planetary Gear Train System with Meshing Beyond Pitch Point
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作者 TANG Xin BAO Heyun +1 位作者 LU Fengxia JIN Guanghu 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2020年第6期884-897,共14页
Nonlinear dynamic analysis was performed on a planetary gear transmission system with meshing beyond the pitch point.The parameters of the planetary gear system were optimized,and a two-dimensional nonlinear dynamic m... Nonlinear dynamic analysis was performed on a planetary gear transmission system with meshing beyond the pitch point.The parameters of the planetary gear system were optimized,and a two-dimensional nonlinear dynamic model was established using the lumped-mass method.Time-varying meshing stiffness was calculated by the energy method.The model consumes the backlash,bearing clearance,time-varying meshing stiffness,time-varying bearing stiffness,and time-varying friction coefficient.The time-varying bearing stiffness was calculated according to the Hertz contact theory.The load distribution among the gears was computed,and the time-varying friction coefficient was calculated according to elastohydrodynamic lubrication(EHL)theory.The dynamical equations were solved via numerical integration.The global bifurcation characteristics caused by the input speed,backlash,bearing clearance,and damping were analyzed.The system was in a chaotic state at natural frequencies or frequency multiplication.The system transitioned from a single-period state to a chaotic state with the increase of the backlash.The bearing clearance of the sun gear had little influence on the bifurcation characteristics.The amplitude was restrained in the chaotic state as the damping ratio increased. 展开更多
关键词 meshing beyond pitch point planetary gear system nonlinear time-varying bearing stiffness timevarying meshing stiffness multiple clearances BIFURCATION time-varying friction coefficient
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折叠翼的结构非线性颤振分析 被引量:16
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作者 杨宁 吴志刚 +1 位作者 杨超 曹奇凯 《工程力学》 EI CSCD 北大核心 2012年第2期197-204,共8页
由于折叠机构间隙的存在,折叠翼的刚度特性呈非线性关系特性,工程实践中需要有效的方法,建立并求解折叠翼的非线性气动弹性方程。该文提出了弦向多个自由度具有结构非线性刚度的折叠翼颤振分析方法,并对典型折叠翼面进行了非线性颤振分... 由于折叠机构间隙的存在,折叠翼的刚度特性呈非线性关系特性,工程实践中需要有效的方法,建立并求解折叠翼的非线性气动弹性方程。该文提出了弦向多个自由度具有结构非线性刚度的折叠翼颤振分析方法,并对典型折叠翼面进行了非线性颤振分析。利用动态子结构方法建立了非线性气动弹性方程,分别在频域和时域给出了颤振求解方法。对比工程软件的计算结果,验证了该方法是否满足工程计算精度的要求。通过对典型折叠翼的计算得到以下结论。在弦向多个位置具有初载间隙型非线性的典型折叠翼结构在一定速度范围内会产生稳定的极限环振荡,在一定速度范围内结构响应与初始扰动相关,后缘铰链振动相比于前缘更加剧烈,初载角较大时振荡更加剧烈。 展开更多
关键词 折叠翼 气动弹性 颤振 动态子结构 描述函数 结构非线性 间隙刚度
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