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226 results about "Nonlinear vibration" patented technology

Engineering nonlinear vibration detecting method

The invention provides an engineering nonlinear vibration inspection method. The method adopts a wavelet nonlinear threshold value filtering wave to filter wide-frequency background noise of a three-direction acceleration signal and to remove DC bias so as to get the treated acceleration signals after frequency domain filtering and removal of trend term. Then speed signals and displacement signals are obtained after the acceleration signals is subject to a first time and second time integrals and removal of trend term. The characteristics and types of the nonlinear vibration are determined through a three-dimensional phase space diagram and other calculations of a reconstructed phase space tested by the three-dimensional phase space diagram. The invention adopts three-direction low resistance piezoelectricity acceleration meter to measure the vibration accelerations of three orthogonal directions. The invention has convenient installation, easy usage and reliable analysis, overcomes the problems of drifting, delay and aberration of the actual acceleration signals after passing through analog integration or digital integration. The invention plays an important role in the engineering nonlinear vibration inspection for mechanical mechanisms, bridges, dams and buildings, etc.
Owner:TAIYUAN UNIV OF TECH

Vibration amplifier and testing method for simulating high-order nonlinear vibration fatigue of blade

The invention discloses a vibration amplifier and a testing method for simulating the high-order nonlinear vibration fatigue of a blade. The vibration amplifier comprises a base, a fixed shell, an upper cushion block, a lower cushion block, first fixing screws, a second fixing screw, an amplification arm and a clamping block; the upper cushion block and the lower cushion block are located in the fixed shell; one end of the amplification arm sequentially passes through one side surface of the fixed shell, a space between the upper cushion block and the lower cushion block, and the other side surface of the fixed shell, and then extends out from the fixed shell; the clamping block is located on the upper surface of the other end of the amplification arm; the first fixing screws pass through the clamping block and the amplification arm, so that the clamping block can be connected with the amplification arm; and the second fixing screw passes through the top of the fixed shell, extends into the fixed shell and contacts with the upper surface of the upper cushion block, so that the upper cushion block, the lower cushion block and the amplification arm can be fixedly connected with one another. With the amplifier and the method adopted, detection on the fatigue strength of the blade can be realized based on a fatigue testing process of resonance frequency and amplitude.
Owner:中国人民解放军空军工程大学航空航天工程学院

Vibration response simulation analyzing method for rolling bearing with single-point failures

ActiveCN103927414ASolve the problem of long cycle and high costSpecial data processing applicationsEngineeringMATLAB
The invention relates to a vibration response simulation analyzing method for a rolling bearing with single-point failures. On the basis of a Hertz contact theory, related knowledge about kinematics and kinetics are utilized to establish a five-degree-of-freedom nonlinear vibration mode of a rolling bearing and kinetic differential equations of the rolling bearing while influencing factors like slipping of rolling balls, oil slick rigidity and the like are taken into consideration, according to that the rolling balls change due to contact deformation is caused when the rolling balls roll through partial failures, a partial failure model of the rolling bearing is introduced into the kinetic differential equations of the rolling bearing, and the single-point failures of the rolling bearing are classified according to length-width ratios of the failures and size ratios between the failures and the rolling balls so as to establish different failure shape functions; the differential equations are solved by an ode solver in MATLAB (matrix laboratory) software, and vibration responses of the rolling bearing are simulated when an inner ring, an outer ring and the rolling balls of the rolling bearing are suffered from the single-point failures. By the aid of the vibration response simulation analyzing method, vibration responses of the bearings with failures in different sizes can be simulated. Compared with traditional methods for acquiring vibration responses of failed bearings, the vibration response simulation analyzing method has the advantages that an experimental period is short and experimental cost is saved. The computation for the vibration responses for the failed rolling bearings can lay the foundation of late failure diagnosis for the rolling bearings.
Owner:BEIJING UNIV OF TECH

Positioning and detection method and system for crack position of wind turbine blade

The invention discloses a positioning and detection method and a system for crack positions of a wind turbine blade. The positioning and detection method comprises the following steps: marking the wind turbine blade, and determining a plurality of mark point positions; collecting a non-cracking nonlinear vibration response signal of each mark point position when the wind turbine blade is not cracked and a cracked nonlinear vibration response signal of each mark point position when the wind turbine blade has a crack for a same piece of wind turbine blade under a same working state; calculatinga mutual information entropy of nonlinear vibration response signals before and after crack damage occurs at each mark point position according to the non-cracking nonlinear vibration response signaland the cracked nonlinear vibration response signal; calculating a vibration response nonlinear degree change amount before and after crack damage occurs at each mark point position according to the mutual information entropy; and determining the crack position according to the vibration response nonlinear degree change amount. The positioning accuracy of the crack position of the wind turbine blade can be improved by adopting the positioning and detection method and system provided by the invention.
Owner:HUNAN UNIV OF SCI & TECH

Wind array type magnetic nonlinear piezoelectric power generation device

The invention discloses a wind array type magnetic nonlinear piezoelectric power generation device, and relates to the field of electromagnetic driving and new energy utilization. The wind array typemagnetic nonlinear piezoelectric power generation device has the advantages of being simple in structure, low in cost, wide in resonance frequency band and the like. The device is composed of a generator casing, L-shaped supporting beams, linear supporting beams, ceramic piezoelectric plates, magnets, a driving shaft, bearings, fan blades and a base. The ceramic piezoelectric plates, the L-shapedsupporting beams and the magnets form L-shaped piezoelectric vibrators; the L-shaped piezoelectric vibrators and the base form a stator part of a generator; the linear supporting beams, the ceramic piezoelectric plates and the magnets form linear piezoelectric vibrators; the linear piezoelectric vibrators, the driving shaft and the blades form a rotor part of the generator; and power is input to the rotor through the blades, the rotor is driven to rotate in the stator by the power of the blades, and meanwhile, the L-shaped piezoelectric vibrators and the linear piezoelectric vibrators generatenonlinear vibration. The device is used for meeting the energy requirements of low-energy-consumption electronic products.
Owner:SHANDONG UNIV OF TECH

Testing method and testing system for nonlinear internal resonance representation of fiber composite boards

InactiveCN107870074ASatisfy the necessary conditions for the formation of internal resonanceAccurate natural frequencyVibration testingFiberCoordination theory
The invention discloses a testing method and a testing system for nonlinear internal resonance representation of fiber composite boards. The method includes selecting internal resonance inherent frequencies of two steps of a composite board, and pre-determining dimension parameters and material parameters, for forming internal resonance of the composite board, according to an integral-multiple coordination method; processing the composite board; testing the internal resonance inherent frequencies of the two steps of the composite board; judging whether the internal resonance inherent frequencies of the two steps are in integral-multiple relation or not, and if not, adjusting the clamping position of the composite plate slightly and retesting the internal resonance inherent frequencies of the two steps of the composite board to enable the internal resonance inherent frequencies of the two steps to have integral-multiple relation; performing internal resonance representation testing on the composite board under different stimulation conditions, analyzing vibration characteristics of nonlinear internal resonance, and concluding change rules of nonlinear vibration response. By the testing method, an integral-multiple coordination theory is provided to calculate the inherent frequency of the composite board, specific parameters of the composite board are determined, and accordingly,testing accuracy and efficiency are high.
Owner:NORTHEASTERN UNIV

Piecewise nonlinear vibration isolator and design method therefor

InactiveCN105046008ASuppression of frequency island phenomenonSimple designSpecial data processing applicationsIsolatorStructural engineering
The invention discloses a piecewise nonlinear vibration isolator and a design method therefor. The method comprises: firstly, adopting an analytic method, i.e., an average method to obtain an amplitude frequency expression of vibration response of the piecewise nonlinear vibration isolator; secondly, according to the amplitude frequency expression, obtaining a relationship expression of an extreme response value and each parameter of a vibration system, adopting a numerical solution to obtain correct solutions and the number of solutions of the extreme response value, and obtaining a changing rule that the number of extreme response values changes with the parameters of the vibration system; thirdly, analyzing main structural parameters of the piecewise nonlinear vibration isolator, such as an influence of different measurement values of damping ratio and the value of base excitation on a frequency island and a changing rule of the number of the extreme response values, and if the number of the extreme response values is larger than 1, determining that the vibration response possibly causes a frequency island phenomenon, or otherwise, determining that the frequency island phenomenon does not occur; and finally, according to the values of the base excitation and the damping ratio, determining the structural parameters of the segmental nonlinear vibration isolator, so that the segmental nonlinear vibration isolator that avoids the frequency island phenomenon is designed. According to the method, the condition for removing frequency islands can be conveniently obtained; and the method is high in operability.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Guideway joint feature-considered vibration response analysis method for upright post-spindle system

InactiveCN105571847ATrue expressivenessSolving for Response CurvesMachine part testingSystem dynamics modelHarmonic balance
The invention provides a guideway joint feature-considered vibration response analysis method for an upright post-spindle system. Firstly, the relationship between a single roller and the bearing capacity is represented based on the Hertz contact theory, and a relational expression between the load and the deformation is established. After that, in the multiple-support excitation and multiple-support response manner, the inherent frequency and the inherent damping of a guideway joint at each order are identified. Then, a kinetic model for the upright post-spindle system is established. Finally, according to the improved harmonic balance method, the vibration response of the upright post-spindle system under the effect of sinusoidal excitation is calculated. According to the technical scheme of the invention, on one hand, the equivalent stiffness of a roller linear guide rail under an arbitrary load is calculated, and the guideway joint is simplified as a system capable of providing the non-linear restoring force. On the other hand, the nonlinear vibration theory-based calculation method is adopted to provide a vibration model for the upright post-spindle system, and the harmonic balance method is improved. Moreover, a response curve is obtained more quickly based on the principle of least square method. The above method provides a solving means for conducting the accuracy research and the optimized design of linear guide rails.
Owner:BEIJING UNIV OF TECH

Fiber composite thin plate nonlinear vibration characterization test method based on vibration measurement with laser

The invention relates to a fiber composite thin plate nonlinear vibration characterization test method based on vibration measurement with laser, First, the inherent frequency and modal shape of a fiber composite thin plate needs to be obtained accurately. Then, a nonlinear vibration characterization test is carried out according to a test idea of from a time domain to a frequency domain and thento a time-frequency domain. The specific steps are as follows: testing inherent frequency of each order of the fiber composite thin plate; testing the modal shape of each order of the fiber compositethin plate according to the inherent frequency; carrying out a harmonic distortion nonlinear characterization test; carrying out a nonlinear time-varying damping characterization test; carrying out ahard/soft rigidity nonlinear characterization test; carrying out a characterization test of amplitude dependent on nonlinear damping; carrying out a nonlinear jump characterization test; carrying outan ultraharmonic/subharmonic resonance nonlinear characterization test; and carrying out an internal resonance nonlinear characterization test. The method provided by the invention can obtain variousnonlinear vibration characterization of the fiber composite thin plate through one-time testing, a test result is relatively accurate, the test efficiency is improved, and an important reference is provided for establishing a method system for a nonlinear vibration test of a composite structure of this type.
Owner:NORTHEASTERN UNIV

Vibration isolation device for vehicle with Mecanum wheels

The invention discloses a vibration isolation device for a vehicle with Mecanum wheels. The vibration isolation device comprises a supporting part, two vibration isolation units, a moving part and a spring; a first boss is arranged on the top of the supporting part, and a second boss is arranged at the bottom of the moving part and is positioned above the first boss; the two vibration isolation units are fixedly connected to the top of the supporting part and are symmetrically arranged along the center line of the supporting part; the moving part is positioned between the two vibration isolation units and is respectively movably connected with the two vibration isolation units; and the spring is sleeved on the second boss and the first boss, the top of the spring is fixedly connected with the bottom of the moving part, and the bottom of the spring is fixedly connected with the top of the supporting part. The vibration isolation device has the advantages that the requirement on a nonlinear vibration isolation function can be met in a complicated engineering work environment; the vibration isolation device in a static state is high in rigidity, namely the bearing capacity; and when moving, the vibration isolation device is low in rigidity, in other words, a low-frequency vibration isolation effect is realized, and the vibration isolation device is good in vibration isolation effect.
Owner:苏州欧米麦克机器人科技有限公司 +1

BP-neural-network-technology-based improved method of spherical harmonic function of ionized layer

InactiveCN107622304ADescribe nonlinear vibration characteristicsHigh precisionSatellite radio beaconingNeural architecturesNonlinear vibrationPuncturing
The invention discloses a BP-neural-network-technology-based improved method of a spherical harmonic function of an ionized layer. The method comprises the following steps: S1, obtaining a puncturingpoint geographic longitude, a puncturing point geographic latitude and an electronic content in the vertical direction of the puncturing point of an observation point of a region; S2, on the basis ofa spherical harmonic function model format of an ionized layer, establishing an ionized layer error compensation model and calculating an electronic content of the puncturing point in the vertical direction and a residual value of the ionized layer error compensation model; S3, carrying out model compensation on a spherical harmonic function by using a BP neural network technology and establishinga fusion model; and S4, with the newly established fusion model, predicting a vertical total ionized layer electronic content residual by spherical harmonic function model fitting, thereby improvingthe model compensation precision. According to the invention, the nonlinear vibration characteristics of the delay information of the ionized layer with time is described accurately; the space-time changing characteristics of the regional ionized layer are simulated well; and compared with the pure spherical harmonic function model, the provided spherical harmonic function model enables the precision to be improved.
Owner:SOUTHEAST UNIV

Nonlinear vibration damping device for suppressing in-orbit micro-vibration of spacecraft

The invention discloses a nonlinear vibration damping device for suppressing in-orbit micro-vibration of a spacecraft. The nonlinear vibration damping device comprises a chamber, a spring, a circular permanent magnet, a damper, and a permanent magnet. The circular permanent magnet is fixedly connected to the inner wall of the chamber. One end of the spring is connected to the top of the chamber, and the other end of the spring penetrates the inner circle of the circular permanent magnet to be connected with the permanent magnet. One end of the damper is connected to the top of the chamber, and the other end of the damper penetrates the inner circle of the circular permanent magnet to be connected with the permanent magnet. After the nonlinear vibration damping device with the unique structural design is mounted at the inner part, having high damping requirement, of the spacecraft, the nonlinear vibration damping device is suitable for suppressing vibrations of structures operating in the microgravity environment; accordingly, the effect of suppressing vibrations of the spacecraft inner structures operating in outer space is good. The nonlinear vibration damping device is simple in structure, convenient to manufacture and low in cost.
Owner:SHANGHAI UNIV
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