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Preliminary Study on Broadband Resonance of Shaking Table Based on the Compressibility of Gas 被引量:1
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作者 Xinghua Zhou Xiao Sun +2 位作者 Kehong Tang Lili Cheng dingxuan zhao 《Journal of Beijing Institute of Technology》 EI CAS 2019年第2期257-264,共8页
In order to improve the performance of the shaking table,a vibration-enhanced shaking table which exploited broadband resonance was constructed.The broadband resonance was realized by an adjustable stiffness mechanism... In order to improve the performance of the shaking table,a vibration-enhanced shaking table which exploited broadband resonance was constructed.The broadband resonance was realized by an adjustable stiffness mechanism which exploited gas compressibility.Different from the traditional device,a gas filled cylinder(GFC)was mounted between the shake table and the exciter,and a pressure regulator was designed to regulate the gas pressure of the GFC.The natural frequency of the designed shaking table can be adjusted based on the compressibility of gas during the test.The principle of stiffness adjustment was theoretically analyzed and a series of experiments were carried out to investigate the effects of regulating the natural frequency.The experimental results indicate that the amplitude can be twice amplified and the natural frequency can be regulated between 2 0 Hz and 6 0 Hz. 展开更多
关键词 SHAKING TABLE GAS COMPRESSIBILITY hydraulic variable stiffness BROADBAND RESONANCE
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Modeling and analysis of landing collision dynamics for a shipborne helicopter
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作者 dingxuan zhao Haojie YANG +3 位作者 Carbone GIUSEPPE Wenhang LI Tao NI Shuangji YAO 《Frontiers of Mechanical Engineering》 SCIE CSCD 2021年第1期151-162,共12页
A Lagrange dynamic model is established based on small-angle approximation to improve the simulation model for shipborne helicopter landing collision.To describe fuselage motion effectively,the proposed model consider... A Lagrange dynamic model is established based on small-angle approximation to improve the simulation model for shipborne helicopter landing collision.To describe fuselage motion effectively,the proposed model considers ship motion,the interaction of the tires with the deck,and tire slippage.A mechanism of sliding motion is built,and a real-time reliability analysis of the algorithm is implemented to validate the proposed model.Numerical simulations are also conducted under different operation conditions.Results show that the proposed dynamic model can simulate the collision motion of helicopter landing in real time.Several suggestions for helicopter pilot landing are likewise provided. 展开更多
关键词 shipborne helicopter landing model Lagrange equations DYNAMICS VALIDATION
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