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    18 August 2016, Volume 36 Issue 4 Previous Issue    Next Issue

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    Near Field Pressure Error Sensing Strategy under Less Measurement Point Condition for ASAC Systems
    2016, 36(4): 1-6.  DOI: 10.3969/j.issn.1006-1335.2016.04.001
    Abstract ( )   PDF (1986KB) ( )  

    It is very critical to design a simple and effective error sensing strategy on the basis of active control strategy. In this paper, aiming at the active control strategy based on pressure acoustic radiation modes, an equivalent near-field pressure error sensing strategy under less measuring points is designed in detail. First, by analyzing the truncation manner of pressure acoustic radiation modes, the feasibility of the active control strategy based on pressure acoustic radiation modes is proved. Then, by measuring the pressure distributions at a few measuring points in the near-field measuring surface and solving the underdetermined equations of modal superposition, the approximate adjoint coefficients of the first order radiation modes can be solved, thus we can develop a near-field pressure error sensing method which corresponds to the active control strategy based on pressure acoustic radiation modes. Finally, using the model of a simply supported steel plate in an infinite baffle, a numerical example is presented. The results show that the error sensing strategy proposed in this paper is feasible and the approximate adjoint coefficients of the first order radiation modes are more precise.

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    Analysis of Strain Modals and the Relationship between the Strain Modals and Displacement Modals
    2016, 36(4): 7-13.  DOI: 10.3969/j.issn.1006-1335.2016.04.002
    Abstract ( )   PDF (1298KB) ( )  
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    Vibration Analysis of Orthotropic Functionally Graded Plates
    2016, 36(4): 14-20.  DOI: 10.3969/j.issn.1006-1335.2016.04.003
    Abstract ( )   PDF (1724KB) ( )  
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    Nonlinear Dynamic Response of Laminated Plates with Axial Motion Subjected to Impact Load
    2016, 36(4): 21-23.  DOI: 10.3969/j.issn.1006-1335.2016.04.004
    Abstract ( )   PDF (1260KB) ( )  

    The nonlinear dynamic response of laminated plate with axial motion subjected to blast load is studied. Firstly, based on constitutive relation of single layer material and large deformation theory, the nonlinear dynamical equation is obtained. Then the modal equations are gained through Galerkin method and solved by Runge-Kutta method. Finally, the effects of axial moving velocity, the peak reflected pressure, the positive pressure phase duration of the impulse on the nonlinear dynamic response are investigated.

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    Dynamic Characteristics of Finite-length Periodic Parameter Beams
    2016, 36(4): 24-26.  DOI: 10.3969/j.issn.1006-1335.2016.04.005
    Abstract ( )   PDF (1206KB) ( )  
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    Analysis of the Absorption Characteristics of a Multi-layered Ellipsoid Cavity Anechoic Coating
    2016, 36(4): 27-31.  DOI: 10.3969/j.issn.1006-1335.2016.04.006
    Abstract ( )   PDF (1319KB) ( )  
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    Influence of Damping Layer on Dynamic Performance of     Water-lubricated Rubber Bearings
    2016, 36(4): 32-37.  DOI: 10.3969/j.issn.1006-1335.2016.04.007
    Abstract ( )   PDF (1540KB) ( )  
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    Finite Element Modeling and Analysis of Viscoelastic Damping Plates under Aerodynamic Excitation
    2016, 36(4): 38-43.  DOI: 10.3969/j.issn.1006-1335.2016.04.008
    Abstract ( )   PDF (1377KB) ( )  
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    Study on Shock Resistance Performance of a New Chiral Periodic Structure
    2016, 36(4): 44-47.  DOI: 10.3969/j.issn.1006-1335.2016.04.009
    Abstract ( )   PDF (1446KB) ( )  
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    Analysis of the Influencing Factors of Surface Acoustic Radiation of Plates under the Flow Action
    2016, 36(4): 48-52.  DOI: 10.3969/j.issn.1006-1335.2016.04.010
    Abstract ( )   PDF (1338KB) ( )  

    The DM of ANSYS Workbench 15.0 was applied to build the plate model under the flow, the MESH was used to divide the grid, and the System coupling was utilized to run fluid and Structure Interaction. The reliability of numerical simulation was verified, and then the influencing factor of plate surface’s acoustic radiation under the flow is analyzed. Results from the numerical simulation and analysis show that in the plate model under the flow, plate surface’s acoustic radiation is mainly caused by the pressure in the parallel flow direction rather than the pressure in the vertical flow direction, the large eddy behind the plate and the natural frequencies of the plate. The fundamental frequency of the plate surface’s acoustic radiation is the same as the plate’s vibration which is caused by the flow and the cavity behind the plate, and it is twice the fundamental frequency of the eddy behind the plate. There is no fundamental frequency of pressure in the field where is out of the eddy and not in the cavity. When the large eddy simulation is statistically steady, there is the same results between the synchronous simulation and non-synchronous simulation of the FW-H and LES.

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    Application of FRF Residual-error Method in Finite Element Model Updating
    2016, 36(4): 53-57.  DOI: 10.3969/j.issn.1006-1335.2016.04.011
    Abstract ( )   PDF (1306KB) ( )  

    The dynamic information of the actual structure can be reflected by accurate finite element model effectively. It’s necessary to update the finite element model to reduce the error in structural modeling. Currently, the updating methods based on modal frequencies, mode shapes and FRF have been used widely. The method based on FRF has more advantages because it can avoid error from modal parameters identification as well as it’s unlimited by test DOF. According to objective function, the method based on FRF can be divided to FRF correlation method and FRF residual-error method. FRF correlation method is based on the correlation of shape and amplitude with parameters sensitivity. Misconvergence happened to part of model updating in result of the irrelevance between FRF and parameters. Therefore, with actual structure, the two methods in the finite element model updating were compared; and the effect of the frequency points and frequency range of FRF in FRF residual-error method were analyzed. The results show that the residual-error method can achieve steady convergence and it has high efficiency; meanwhile, reasonable frequency points and wider frequency range are beneficial to improving the updating efficiency.

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    Influence of the Insulation Material Arrangement on Sound Insulation Properties of Composite Sheets
    xu lei zhang xue feiwang rui qian
    2016, 36(4): 58-62.  DOI: 10.3969/j.issn.1006-1335.2016.04.012
    Abstract ( )   PDF (1481KB) ( )  

    The insulation test to a combination of high-speed train flattened structure, when the swap in which two acoustic longitudinal position pad, flat top acoustic properties of composite structure changed significantly. To solve this problem, this paper based on statistical energy analysis explores the double insulation composite sheet material arranged in the order of the overall structure of sound insulation characteristics of law, analyzes the causes of the phenomenon;Subsequently, further use of statistical models to predict the impact energy method three acoustic insulation composite sheet material arranged in order of overall sound insulation properties of inquiry was extended. The results show that: for double-layer composite structure, when the two types of insulation materials is constant, the large amount of insulation material is placed near the sound source, the small amount of noise into the far end of the sound source, the lift the overall structure of the maximum amount of noise, major upgrade of the low-frequency sound insulation; For the three-layer composite structure, the situation is more complex, when the largest insulation material is placed near the sound source, the second largest amount of insulation material is placed in the far end of the sound source, the minimum amount of sound insulation material is placed in the middle, to enhance the amount of the overall structure of the maximum amount of noise, and also to enhance the low and intermediate frequency sound insulation. Contents of this paper to further improve the sound insulation properties of composite engineering has reference.

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    Influence of Friction Hysteresis of Leaf Springs on Ride Comfort
    2016, 36(4): 63-65.  DOI: 10.3969/j.issn.1006-1335.2016.04.013
    Abstract ( )   PDF (1215KB) ( )  

    In order to analyze the influences of leaf spring friction hysteresis on automotive ride comfort, An improved Bouc-Wen model parameters are identified with iterative least square method according to the measured values of the load and deflection of leaf spring. The relationship between the hysteretic force and inflection of leaf spring is obtained under the random loading. The improved Bouc-Wen model has been combined with a whole car model with 4DOFs to analyze the influence of hysteretic characteristic of leaf spring on ride comfort. The results show that the friction hysteresis of leaf spring increases the natural frequencies of acceleration of body, suspension dynamic inflection and tire dynamic load by approximate 12%, and increases the PSD amplitude value of body acceleration by 15.2%, which reduce the ride comfort. The PSD amplitude value of suspension dynamic inflection is decreased by 11.6%. The friction hysteresis of leaf spring has little influence on axle acceleration and tire dynamic load.

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    Effect of Swash Plate Compressor Clearance between Piston and Hemisphere on Vibration
    2016, 36(4): 66-69.  DOI: 10.3969/j.issn.1006-1335.2016.04.014
    Abstract ( )   PDF (1472KB) ( )  
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    Double-layer Vibration Isolation Experimental Equipment Based on Fx LMS Algorithm
    2016, 36(4): 70-73.  DOI: 10.3969/j.issn.1006-1335.2016.04.015
    Abstract ( )   PDF (1376KB) ( )  
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    Effect of Shaft Alignment on Stern-bearing Force Transmission Characteristics
    2016, 36(4): 74-79.  DOI: 10.3969/j.issn.1006-1335.2016.04.016
    Abstract ( )   PDF (1144KB) ( )  

    The transmitting of ship shaft lateral vibration to the ship body through stern bearings will induce the vibration of ship stern and noise, which is the major factor for ride comfort and safety. Ship shaft alignment must be conducted because of its own heavy weight and protection for bearings. The load of every bearing will be changed with the change of bearing height in the process of shaft alignment, which will also change the bearing stiffness and influence the shaft vibration characteristic and bearing transmitting force. In order to solve this problem, shaft alignment and lateral vibration are modeled by the transfer matrix method. According to a shaft example, line alignment and optimal alignment of minimum rear bearing static load are conducted respectively. The result shows: the bearing force responses of these two methods are narrowly different in the low frequency band, but have an obvious difference in high frequency band.

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    Noise Prediction and Acoustic Design Optimization of Spacecraft’s Equipment Cabins
    2016, 36(4): 80-83.  DOI: 10.3969/j.issn.1006-1335.2016.04.017
    Abstract ( )   PDF (1397KB) ( )  

    For a manned spacecraft, obtaining comfortable acoustic environment with limited weight cost is the main objective of acoustic design. For a spacecraft equipment cabin with disturbance hardware, the statistical energy analysis (SEA) model is built, sound pressure level (SPL) in the astronaut passage is predicted based on measured radiation characteristics of the disturbance sources, and noise reduction countermeasure is proposed. The thicknesses of honeycomb plates and the sound absorption layers are selected as design variables, and genetic algorithm (GA) optimization is employed to find the optimal acoustic design. The results indicate that, the maximum SPL in the astronaut passage is reduced by 3dB, making the acoustic requirement met, and the overall weight of each bay is reduced by 9%, which validates the application of GA in acoustic design optimization.

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    Sound Transmission Loss Characters of Unidirectionally Reinforced Double-layer Plates in Whole Frequency Range
    2016, 36(4): 84-87.  DOI: 10.3969/j.issn.1006-1335.2016.04.018
    Abstract ( )   PDF (1147KB) ( )  
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    Modal Simulation Analysis and Experimental Verification of Automotive Fuel Tanks
    2016, 36(4): 88-91.  DOI: 10.3969/j.issn.1006-1335.2016.04.019
    Abstract ( )   PDF (1493KB) ( )  
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    Influence of Intermediate Frame Flexibility on the Vibration Isolation Characteristics of a Double Layer Vibration Isolation System
    2016, 36(4): 92-96.  DOI: 10.3969/j.issn.1006-1335.2016.04.020
    Abstract ( )   PDF (1511KB) ( )  

    For quantitative analysis the influence of flexible intermediate frame on the vibration isolation characteristics of double layer vibration isolation system of diesel power pack, to guide its optimization design, the finite element model of the middle frame is established and its mode is calculated. By comparing with the experimental modal, the correctness of the finite element model is verified. The coupled system dynamics model considered the flexible middle frame and multi-rigid-body system dynamics model treated the middle frame as a rigid body were established in ADAMS. Through the free vibration and the analysis of frequency sweep, obtained the influence of flexible intermediate frame on the vibration isolation characteristics of double layer vibration isolation system. The results show that flexible intermediate frame can reduce the system's natural frequency and the decoupling degree of the main modal direction, and make the amplitude response of the system produce the phenomenon of “frequency shift” and “increasing frequency”, the low frequency based on “frequency shift”, the high frequency based on “increasing frequency”, and two kinds of phenomena occur at the same time in the middle of the band. Relevant conclusions can provide a reference for vibration isolation design and effective control of coupled vibration.

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    Active Control Simulation for Torsional Vibration of a Hybrid Excavator Shafting System
    2016, 36(4): 97-102.  DOI: 10.3969/j.issn.1006-1335.2016.04.021
    Abstract ( )   PDF (1598KB) ( )  
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    Vehicle’s Low Frequency Noise Prediction and Body Panel’s Acoustic Contribution Analysis
    2016, 36(4): 103-107.  DOI: 10.3969/j.issn.1006-1335.2016.04.022
    Abstract ( )   PDF (1625KB) ( )  
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    Optimal Design of Powertrain Mount Systems of Electric Bus Motors
    2016, 36(4): 108-112.  DOI: 10.3969/j.issn.1006-1335.2016.04.023
    Abstract ( )   PDF (1303KB) ( )  

    In this paper, the rigid body dynamics model of an electric bus motor powertrain mount system was established. The excitation of the motor powertrain was then analyzed. With the use of software ADAMS, the modal and frequency response characteristics of mount system were analyzed. Through integrating the engineering optimization software Isight and MATLAB, the optimal design of motor powertrain mount system was conducted using the multi-island algorithm in Isight directly. The vibration isolation performance of the optimized mount system has been improved.

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    Cross-iterative Algorithm and Its Application to the Analysis of Vehicle-track Nonlinear Coupling Systems
    2016, 36(4): 113-119.  DOI: 10.3969/j.issn.1006-1335.2016.04.024
    Abstract ( )   PDF (1217KB) ( )  
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    Design Concept of Sound Insulation Windows of Noise-sensitive Buildings in the Area Affected by Aircraft Noise
    2016, 36(4): 120-123.  DOI: 10.3969/j.issn.1006-1335.2016.04.025
    Abstract ( )   PDF (972KB) ( )  

    Based upon the aircraft noise of Beijing capital international airport,The design of sound insulation window was investigated for noise-sensitive buildings affected by aircraft noise。 One hour equivalent A-weighted sound pressure level LAeq was finally used for the evaluation value of design of sound insulation window,and LAeq was corrected according to person annoyance level associated with the different type of noise and period。The sound insulation values of window that is designed with the corrected LAeq can basically satisfy the requirement of environmental protection 。

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    Analysis of Aerodynamic Noise Induced by Rotating Blades of  an Axial Fan
    2016, 36(4): 124-128.  DOI: 10.3969/j.issn.1006-1335.2016.04.026
    Abstract ( )   PDF (1476KB) ( )  

    Abstract: In views of the aerodynamic noises generated by axial fan, a three-dimensional model of this kind of fan is built. Lighthill acoustic analogy theory, FW-H acoustic wave equation and FLUENT numerical simulation are used to analyze the characteristics of aerodynamic noises arisen from the axial fan’s rotating blades. The simulation result shows that the static pressure of rotating blades is mainly distributed on the front side of blades. However, the fluctuating pressure is distributed on both sides and mainly in the margin of blades, which is caused by the severe air turbulence from the vortexes in the outer edge of blades. The acoustic power of blades is also distributed in the margin of blades, but its characteristic of distribution is different from that of fluctuating pressure, indicating that the aerodynamic noises of rotating blades are not all produced by fluctuating pressure. In addition, the faster the blades rotate or the larger the blade’s diameter is, the more intense the aerodynamic noise is.

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    Numerical and Experimental Analysis of the Vibration Characteristics of the Elevated Box Girders in Urban Mass Transit
    2016, 36(4): 129-134.  DOI: 10.3969/j.issn.1006-1335.2016.04.027
    Abstract ( )   PDF (1826KB) ( )  

    Abstract: In order to study the vibration response of the elevated box girders in urban mass transit subjected to the train, 3D vibration model of simply supported girder are established by FEM. Thus the dynamic response of the box girder can be obtained, with the train at a velocity of 60, 80, 100 and 120km h-1. And the dynamical characteristics of elevated box girder are investigated by field tests. The theoretical calculation results and test data can keep consistent in the frequent rang of 20~400Hz. The maximum deviation is 9.6dB and this show the calculation model can meet accuracy requirement. The modal analysis results show that mode shapes of which natural frequencies is higher than 10Hz present a deformation in section, and the vibration pattern of box girder appear as the bending vibration of composed plate element gradually. The time domain analysis result shows that when the same train pass, the vibration amplitude of measuring point vibration will increase with the vehicle’s speed and for different train pass with very close speed, the impact on bridges are different because of vehicle-track coupled action. The vibration levels of rail, slab, deck, flange, web and bottom plate range of 140~160dB, 110~120dB, 110~120dB, 115~130dB, 110~125dB and 105~115dB respectively, and increase with the improvement of train speed.

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    Improved Local Mean Decomposition Method and Its Application to Fault Diagnosis of Reciprocating Compressor Bearings
    2016, 36(4): 135-139.  DOI: 10.3969/j.issn.1006-1335.2016.04.028
    Abstract ( )   PDF (1348KB) ( )  
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    Malfunction Analysis of Blades Deflection for an Aero-engine Axial Impeller
    2016, 36(4): 140-143.  DOI: 10.3969/j.issn.1006-1335.2016.04.029
    Abstract ( )   PDF (1343KB) ( )  

    An aero-engine declined in efficiency and appeared whistling during the ground test. Successfully found the engine first stage axial flow impeller blade deformation by the analysis of the noise and the vibration signal. At home and abroad, about the noise of the rotor blade deformation research less. Based on the detailed analysis of the fault, it is concluded that the characteristics of the noise spectrum.

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    Analysis of Vibration Fault of an Air-conditioner Compressor Bracket in a Roller
    2016, 36(4): 144-147.  DOI: 10.3969/j.issn.1006-1335.2016.04.030
    Abstract ( )   PDF (1406KB) ( )  
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    Analysis and Control of Interior Whistling Noises Caused by Frequency Modulation of Gears
    2016, 36(4): 148-150.  DOI: 10.3969/j.issn.1006-1335.2016.04.031
    Abstract ( )   PDF (1435KB) ( )  

    A front-mounted rear-drive model creates obvious indoor howling when accelerating. After experimental analysis, it is confirmed that the high order harmonic frequency of the main deceleration gear mesh frequency caused by gear mesh of main decelerator is carrier frequency. The frequency of active gear shaft of main decelerator is vibration modulation phenomenon of modulation frequency.

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    Application of Wavelet Analysis to Vehicle AC-ON Abnormal Sound Diagnosis
    2016, 36(4): 151-155.  DOI: 10.3969/j.issn.1006-1335.2016.04.032
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    Study on Fault Diagnosis Method for Diesel Engines Based on Instantaneous Speed and Impact Signal
    2016, 36(4): 156-160.  DOI: 10.3969/j.issn.1006-1335.2016.04.033
    Abstract ( )   PDF (2197KB) ( )  

    This paper established a three-dimensional solid model of Multi-cylinder diesel engine, simulating the instantaneous speed waveform under normal and abnormal combustion situation, analyzing and studying the failure characteristics. Using the WP10.340E32 diesel engine to build a diesel engine fault simulation test-bed and an on-line monitoring system to simulate and capture misfire fault of diesel engine. Comparing the normal signals with the abnormal signals from the acquired instantaneous speed and cylinder vibration signals to analyze the internal relations between the failure and the characteristics. The simulation and experimental data all proved that the instantaneous speed combined with the vibration signals could be effectively used to the identification of misfire fault of diesel engine, and could also locate the faulty cylinder accurately, simplified the diagnostic process.

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    Intelligent Control of Nonlinear Torsional Vibration of Rolling Mills based on Neural Network and Fuzzy PID
    2016, 36(4): 161-164.  DOI: 10.3969/j.issn.1006-1335.2016.04.034
    Abstract ( )   PDF (1242KB) ( )  
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    Separation of Ocean Wave Sound from the Underwater Sound Signals Collected by the Buoy
    2016, 36(4): 165-168.  DOI: 10.3969/j.issn.1006-1335.2016.04.035
    Abstract ( )   PDF (1401KB) ( )  
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    10.3969/j.issn.1006-1335.2016.04.036
    2016, 36(4): 169-173. 
    Abstract ( )   PDF (1746KB) ( )  
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    Application of Flexibility Curvature Method in Damage Detection of Transmission Towers
    2016, 36(4): 174-177.  DOI: 10.3969/j.issn.1006-1335.2016.04.037
    Abstract ( )   PDF (1472KB) ( )  

    In the structure of fingerprint identification and damage identification method based on flexibility method can used to identify the damage location and degree. Therefore, the flexibility curvature method and the flexibility curvature matrix difference method is introduced to the damage identification of transmission tower to. Using ANSYS to establish the model of 51 meters high glass type transmission tower, two methods are used to identify the single damage and multi damage of different degrees of structure. The results show that can only use the flexibility matrix of the vertical component of the structure to structure damage identification,When identifying, two kinds of indexes have good effect, but the flexibility curvature method for small damage does not recognize; flexibility matrix curvature difference method can better identify the little damage to the set.

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    Study on Acoustic Characteristics of the Impedance Composite Muffler with a Triangular Cross-section Inner Tube
    2016, 36(4): 178-182.  DOI: 10.3969/j.issn.1006-1335.2016.04.038
    Abstract ( )   PDF (1426KB) ( )  
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    Experimental Research on Impact Characteristics of a Rubber Steel Wire Isolator
    2016, 36(4): 183-187.  DOI: 10.3969/j.issn.1006-1335.2016.04.039
    Abstract ( )   PDF (1446KB) ( )  

    Impact stiffness and damping are important parameters of vibration isolator, which play an important role in the design of vibration isolation system. The impact stiffness and damping of the rubber steel wire isolator were tested. The acceleration time curve of load mass is transformed into the hysteresis loop of the isolator to solve the impact stiffness and the equivalent damping, and the impact stiffness is fitted by polynomial. Data results under different conditions shows: in the case of small deformation, the elastic restoring force and the vibration isolator's deformation of the rubber steel wire isolator basically has the linear relationship, and it has cubic function with the increase of the impact displacement; the equivalent impact stiffness of the impact process is proportional to the initial impulse; but the damping increases first and then decreases with the maximum deformation. The above conclusions can guide the engineering selection and application of rubber steel wire vibration isolator.

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    Active Vibration Control of a Conical Shell Using Piezoelectric Ceramics
    2016, 36(4): 188-192.  DOI: 10.3969/j.issn.1006-1335.2016.04.040
    Abstract ( )   PDF (1456KB) ( )  
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    Performance Analysis of the Vibration Isolation Platform for Multi-DOF Passive Airborne Radars in Failure State
    2016, 36(4): 193-197.  DOI: 10.3969/j.issn.1006-1335.2016.04.041
    Abstract ( )   PDF (1562KB) ( )  

    According to the analysis of the requirements of a certain type of airborne radar, a multi-DOF passive vibration isolation platform based on parallel mechanism with redundancy protection ability is designed to meet the requirement. The principle design of the vibration isolation platform is introduced, and the six degrees of freedom of the vibration isolation is proved. The capability of damping vibration of the platform is simulated in the case of possible failure based on the design of redundancy protection. The simulation proved that the vibration isolation platform under the failures can protect the radar from over vibrating, what can improve the survivability of the radar.

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    Influence of Constraint Condition on the Results of High-frequency Vibration Test of Rubber
    2016, 36(4): 198-201.  DOI: 10.3969/j.issn.1006-1335.2016.04.042
    Abstract ( )   PDF (1116KB) ( )  

    The coherence of the different restrict modes and the vibration properties of the damping beam were compared by transfer function method during 2000Hz ~ 6000Hz . Vibration damping tests under different restrict modes of the beam were simulated by the finite element method. Compared the simulation result of the speed transfer rate of the intermediate nodes of the most formants with the experimental result, The result show that the simulation result is more identical with the test result when the damping beam clamped at both ends than one end. It provides reference for selection of restrict modes in the high-frequency vibrations of rubber vibrating beam.

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    Design of a Low Frequency Vibrator and Analysis of its Shock Response Experiment
    2016, 36(4): 202-205.  DOI: 10.3969/j.issn.1006-1335.2016.04.043
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    Method for Vibration Stress Monitoring of Engine Fan Blades
    2016, 36(4): 206-209.  DOI: 10.3969/j.issn.1006-1335.2016.04.044
    Abstract ( )   PDF (1438KB) ( )  
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    Optimization of Car’s Rear Drum Sound Improvement Scheme
    2016, 36(4): 210-213.  DOI: 10.3969/j.issn.1006-1335.2016.04.045
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    Thermal Analysis of Satellite Spot Beam Antennas in Orbit
    2016, 36(4): 214-220.  DOI: 10.3969/j.issn.1006-1335.2016.04.046
    Abstract ( )   PDF (1118KB) ( )  

    During the running of the satellite in orbit, the temperature of the satellite antennaschanges with the heat flux and the radiation exchange.Satellite components such as antenna reflectors which aresensitive to the temperature change are prone to thermally induced vibrations which thus affect their normal function. Thermal analysis of the satellite antennas running in orbit provides temperature datafor the thermal control design of satellite antennas and the prediction of thermally induced vibrations. Firstly the paper established the physical model of certain type of satellite antenna system, and then analyzed the transient heat in orbit space by the software of UG-TMG. Lastly we followed and analyzed the result of temperature of antenna reflectors.

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