Quasi-zero stiffness (QZS) vibration isolation,by introducing stiffness nonlinearity,effectively addresses the inherent contradiction between load-bearing capacity and isolation bandwidth in conventional linear isolators. As a result,it exhibits superior low-frequency isolation performance. The core challenge in realizing QZS isolation lies in designing mechanical structures whose force-displacement curves simultaneously demonstrate high static stiffness and low dynamic stiffness. Focusing on QZS isolation design methodologies,this paper first outlines the fundamental principles of QZS isolation and categorizes the traditional approaches according to the means of stiffness nonlinearization into four groups: geometric motion nonlinearity,geometric deformation nonlinearity,magnetic nonlinearity,and stress-strain nonlinearity. Subsequently,it introduces emerging design strategies based on nonlinear positive-stiffness structures,including hardening and softening types,and compares them with conventional approaches,with particular attention to their differences in static and dynamic behavior. Finally,the paper summarizes and discusses future directions from the perspectives of negative-stiffness structure design,QZS characteristic tuning,and potential applications,aiming to provide a comprehensive overview of the latest research progress and to offer insights into future development trends of QZS isolation systems.
To investigate the fault mechanism of blade cracks and to analyze the effects of blade crack on the three-dimensional (3D) tip clearance of the rotor system,while comprehensively considering blade radial deformation,flap-wise bending,and chordwise bending,this paper develops a novel dynamic model of the rotor system based on continuum theory. With the blade breathing crack model under the three-dimensional stress state,a 3D tip clearance dynamic response model of rotor system with blade cracks is further established. The accuracy of the dynamic model is validated by comparing it with the finite element model and experiments. On this basis,the effect of blade crack depth and location on the 3D tip clearance in rotor system is further analyzed. The results show that the amplitudes of the high frequency doubling component of the 3D tip clearance increase with crack depth,while both the fundamental frequency and the high frequency doubling component of the 3D tip clearance show a non-monootonic trend as the relative crack location increases. The research results provide theoretical guidance for research on monitoring and diagnosis method of aero-engine blade crack based on 3D tip clearance.
The theoretical framework of Hertzian contact model for soft sphere collisions is well-established; however limited research has been done on the collision between rigid particles and elastoplastic materials. In this study,a novel damping form is introduced by incorporating the elastoplastic half-space contact constitutive relationship,and a viscoelastoplastic collision model between hard spherical particles and polyurethane surfaces is established. The nonlinear dynamic equations for particle and elastoplastic surface collision are derived. Furthermore,by conducting experiments to measure the coefficient of restitution for coal pellets colliding with polyurethane,the Meyer's index of the polyurethane material and the damping coefficient in the dynamic equations are determined. Additionally,the correctness of the damping model proposed in this study is validated by considering different damping forms in the equations. The changes in contact force at different stages are analyzed under various damping coefficients. The variations of displacement,velocity,and contact force during the collision process between particles and elastoplastic polyurethane are investigated. The results reveal that with an increase in the initial collision velocity,the irreversible plastic deformation of polyurethane increases from 1.636×10-4 m to 5.657×10-4 m,the coefficient of restitution decreases from 0.583 2 to 0.501 2,the collision time decreases from 6.963×10-4 s to 4.737×10-4 s,and the proportion of plastic compression stage decreases from 59.81% to 59.04%.The model established in this paper can be used in scenarios where particles collide with softer planes,such as the separation of metal ores and particle dampers. This paper provides theoretical support for the transportation,collision,impact,and separation of particle systems.
Aiming at the chatter problem in the process of milling screw rotors,a chatter monitoring method based on RelifF algorithm to the least square support vector machine (RF-LSSVM) is proposed. Firstly,the vibration signals in the milling process of the screw rotor are decomposed,and feature extraction and selection are performed using the variational modal (VMD) and the RelifF algorithm. Secondly,the penalty factor,kernel parameter,the number of near neighbor samples of RelifF algorithm and the length of dimension reduction feature of LSSVM are iteratively optimized using the enhanced whale optimization algorithm (E-WOA). Finally,a flutter identification model is established by inputting the reduced-dimensional flutter eigenvector matrix and outputting the flutter occurrence state. The experimental results show that the proposed VMD-RF-LSSVM model has a higher recognition accuracy than the unoptimized variational modal decomposition-support vector machine (VMD-SVM) model,reaching 99.5% accuracy. The proposed method can effectively monitor the chatter problem in the screw milling process,provides a thought for the optimization of the screw milling processing.
In view of the current situation that the detection indices of maglev train boot rail system both domestically and internationally are relatively limited,and there is a lack of detection data within the 100—140 km/h speed range,a comprehensive detection framework for high-speed maglev train boot rail system is proposed. Firstly,in accordance with relevant standards and specifications of pantograph and conductor rail system testing,a detection method is developed,which includes conductor rail contact force,vibration acceleration,electric shoe current,arc combustion and transverse geometric parameters of the conductor rail. Secondly,a real-time side conductor rail monitoring system that combines video surveillance and data statistical analysis is proposed,and a supporting program for extraction,processing and analysis of original detection data is developed. Finally,a medium- and low-speed maglev line is taken as the test object,and the data measured at different speed levels of the maglev train are analyzed. The results show that the dynamic performance of the pantograph differs during the upward and downward runs of the maglev train; The contact force and vibration degree at the expansion joint are larger than those in the middle section,indicating poorer dynamic performance of the conductor rail. Toe vibration mainly comes from vertical vibration. Relevant studies reveal the characteristics and issues of the maglev train boot rail system under different working conditions,providing theoretical support and practical basis for the further optimization of the maglev train boot rail system.
In response to the challenge of quantitatively diagnosing corrosion damage thickness within pipelines,a quantitative imaging method for pipeline corrosion damage using ultrasonic guided waves is proposed. Firstly,based on the frequency domain finite difference method,a numerical model for multi-path helical propagation of guided waves in pipes is established,enabling rapid calculation of guided wave reception signals when thickness map is known. Secondly,by calculating the received signals in the presence of randomly distributed damage,a database comprising 3 500 samples of damage signals is generated through iteratively running the numerical model. Subsequently,a one-dimensional convolutional neural network imaging model is constructed. The model is trained using the generated database to establish a mapping relationship between thickness maps and reception signals,and inputting the reception signals into the imaging model yields corresponding thickness maps. Finally,the feasibility of the proposed method is experimentally validated. The mean square error between experimental imaging results and actual values is 8.6048×10-4,the correlation coefficient is 0.711 6,and the imaging model runtime is 0.538 5 seconds. The results indicate that the proposed method can achieve quantitative imaging of corrosion damage thickness within pipelines with high imaging efficiency.
In order to analyze the reliablility of hypersonic flight vehicles,the longitudinal model of the vehicle is simplified as a cantilever beam structure,and a limit state function is formulated. To address the uncertainty of variable parameters within the limit state function,a hybrid reliability analysis method based on a two-stage Kriging model is proposed. For the first stage,initial sample points are selected to construct an initial Kriging model centered on potential failure points meeting specified accuracy requirements,ensuring the model satisfies this accuracy criterion. For the second stage,a hybrid reliability analysis of the flight vehicle is performed using the initial Kriging model and the first-order reliability method. The Kriging model is adaptively updated by incorporating learning functions,thereby enhancing the efficiency and accuracy of reliability calculations. Comparing the results with existing methods under different parameters of ultimate strength,cantilever beam height,and width,it is demonstrated that the proposed method can meet the requirements for real-time and accurate reliability analysis of the hypersonic vehicle.
Nonlinear structures exhibit multiple responses under steady-state excitation,making it challenging to directly obtain their dynamic characteristics using traditional vibration test methods. To address this issue,a constant-force dynamic characteristics testing method based on acceleration-response-controlled step-sine frequency sweep test technology is proposed. First,the acceleration response at the excitation point is selected as the control signal,and a step-sine frequency sweep experiment is performed by maintaining a constant response amplitude. Secondly,the resulting simple harmonic excitation spectrum and acceleration response spectrum are obtained through experiments under various acceleration amplitude conditions,and a smooth simple harmonic force surface is constructed using linear interpolation. Then,by extracting the contour lines corresponding to constant force amplitude from this surface,the frequency response curve of the nonlinear structure under constant-force conditions is derived. Finally,the dynamic characteristics of a typical bolted nonlinear structure are investigated. The results show that the proposed approach can accurately capture the frequency response characteristics of bolted nonlinear structures,revealing the pronounced nonlinear dependence on force amplitude. Furthermore,bolt preload and structural reassembly are found to significantly influence the dynamic characteristics of the connection structure.
In order to monitor the operation state of each wheel motor in distributed drive electric vehicle and ensure the safety of the vehicle,a fault diagnosis method of in-wheel motor based on improved multi-class support vector data description (MCSVDD) is proposed. The method incorporates two major improvements. First,a classification judgment rule based on the minimum distance to the cluster center within the class is proposed using the affinity propagation (AP) clustering algorithm to enhance MCSVDD. Second,a Weibull kernel function is constructed from the Weibull distribution to optimize data description model. Meanwhile,a dimensionality reduction method based on minimum-distance propagation discriminant projection (MPDP) is proposed for the multi-dimensional feature set of in-wheel motor operating state,which improves the separability of in-wheel motor fault states under different working conditions. Finally,in-wheel motors with typical bearing faults are customized respectively to collect vibration signals under 7 rotating speeds for verifying the effectiveness of the proposed method. The results show that the reduced dimension data's separability of observed samples of in-wheel motor operating state based on MPDP is better than that of linear discriminant analysis (LDA),minimum-distance discriminant projection (MDP) and locality preserving projection (LPP),and the recognition accuracy of MCSVDD's state recognition system based on Weibull kernel function is higher than that of polynomial and Gaussian kernel function.
Aiming to address the operation stability affected by the parameter time-variation of the ultrasonic motor and the harmonic effect of the drive voltage,this paper focuses on the design and optimization of LLCC resonant network topology as well as total harmonic distortion (THD) of the output voltage for driving linear ultrasonic motors (LUMs). Such method can effectively overcome the issue on the variations of the driving voltages caused by the parameter time-variation to improve their operation stability. Firstly,the calculation method for the LLCC matching parameters is derived by using a contact-based equivalent circuit of LUMs considering the stator/mover contact boundary conditions,and a compensation capacitor is added to improve the elasticity margin and the stability of impedance matching. Furthermore,the filtering characteristics of the LLCC resonant network near the resonant frequency is discussed in depth,and the mathematical relationships are derived between the THD of the output voltage and the parameters of the LLCC resonant network are derived. Furthermore,the influence of the parasitic parameters of the transformer on the LLCC resonant network is also analyzed. On this basis,the design optimization methodology for the LLCC resonant network is proposed while acting the THD of the sinusoidal output voltage as the main target. Finally,a LLCC resonant driver is designed for a V-shape LUM,and the corresponding experiments are conducted. The results indicated that the gain and the THD of the output voltage as well as the peak amplitude of the series capacitor voltage itself are determined by the ratio of the series capacitor and the parallel capacitor in the resonant network. The series inductor is the dominating factor for the soft switching characteristics. The THD of the output voltage is controlled below 3%,which is improved more than 70% compared to the unoptimized LLCC resonant driver.