DESIGN AND DEVELOPMENT METHODOLOGY OF ADAPTIVE VIBRATION ABSORBER

Similar documents
DYNAMIC ANALYSIS OF CANTILEVER BEAM

VIBRATION ANALYSIS OF E-GLASS FIBRE RESIN MONO LEAF SPRING USED IN LMV

PERFORMANCE EVALUATION OF OVERLOAD ABSORBING GEAR COUPLINGS

INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING AND TECHNOLOGY (IJMET)

Finite Element Analysis of Piezoelectric Cantilever

The Analysis of Aluminium Cantilever Beam with Piezoelectric Material by changing Position of piezo patch over Length of Beam

Kaunadis [5] analyzed the vibration analysis of cantilever beam in free and forced condition. The cantilever beam was loaded at different locations.

OPTIMIZING VIBRATION REDUCTION IN 2DOF SYSTEM WITH CHANGE POSITION OF INDEPENDENT TRANSLATIONAL D-DVA

DEVELOPMENT OF ACTIVELY TUNED VIBRATION ABSORBER FOR WASHING MACHINE

Finite Element Analysis Lecture 1. Dr./ Ahmed Nagib

Measurement Techniques for Engineers. Motion and Vibration Measurement

Introduction to Mechanical Vibration

Chapter 5. Vibration Analysis. Workbench - Mechanical Introduction ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved.

2.003 Engineering Dynamics Problem Set 10 with answer to the concept questions

Cork Institute of Technology. Summer 2007 Mechanics of Machines (Time: 3 Hours)

EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF TORSIONAL EXCITATION OF VARIABLE INERTIA EFFECTS IN A MULTI-CYLINDER RECIPROCATING ENGINE

Stress Distribution Analysis in Non-Involute Region of Spur Gear

Chapter 4 Analysis of a cantilever

Experimental Modal Analysis of a Flat Plate Subjected To Vibration

Effect of Angular movement of Lifting Arm on Natural Frequency of Container Lifting Mechanism using Finite Element Modal Analysis

Chapter 23: Principles of Passive Vibration Control: Design of absorber

Dynamic (Vibrational) and Static Structural Analysis of Ladder Frame

MOOC QP Set 2 Principles of Vibration Control

Modal Analysis: What it is and is not Gerrit Visser

Dynamics of structures

Module 4: Dynamic Vibration Absorbers and Vibration Isolator Lecture 19: Active DVA. The Lecture Contains: Development of an Active DVA

LANMARK UNIVERSITY OMU-ARAN, KWARA STATE DEPARTMENT OF MECHANICAL ENGINEERING COURSE: MECHANICS OF MACHINE (MCE 322). LECTURER: ENGR.

Response Spectrum Analysis Shock and Seismic. FEMAP & NX Nastran

Design of an Innovative Acoustic Metamaterial

Simulation and Experimental Research on Dynamics of Low-Pressure Rotor System in Turbofan Engine

Varuvan Vadivelan. Institute of Technology LAB MANUAL. : 2013 : B.E. MECHANICAL ENGINEERING : III Year / V Semester. Regulation Branch Year & Semester

(Refer Slide Time: 1: 19)

Characterization of Fixture-Workpiece Static Friction

Engineering Science OUTCOME 2 - TUTORIAL 3 FREE VIBRATIONS

2. Materials and Methods The main function of the Tuneable Dynamic Vibration Absorber is to damp the undesirable vibration on the system

Introduction to Continuous Systems. Continuous Systems. Strings, Torsional Rods and Beams.

Crack detection in cantilever beam by frequency based method

Introduction to structural dynamics

Study & Analysis of A Cantilever Beam with Non-linear Parameters for Harmonic Response

Design And Analysis Of Vibration Exciter

Investigation of Circular Flexural Hinge Used in Compliant Mechanism Using FEA Tool.

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each. Q.1 Find the force (in kn) in the member BH of the truss shown.

Analysis on propulsion shafting coupled torsional-longitudinal vibration under different applied loads

MOOC QP Set 1 Principles of Vibration Control

Due Date 1 (for confirmation of final grade): Monday May 10 at 11:59pm Due Date 2 (absolute latest possible submission): Friday May 14 at 5pm

Vibration analysis of a UAV multirotor frame

1330. Comparative study of model updating methods using frequency response function data

Journal of Chemical and Pharmaceutical Research, 2014, 6(7): Research Article

ScienceDirect. Response Spectrum Analysis of Printed Circuit Boards subjected to Shock Loads

The Design of a Multiple Degree of Freedom Flexure Stage with Tunable Dynamics for Milling Experimentation

DYNAMIC ANALYSIS OF ROTOR-BEARING SYSTEM FOR FLEXIBLE BEARING SUPPORT CONDITION

Analysis and Optimization of Engine Mounting Bracket

Cantilever Beam Crack Detection using FEA and FFT Analyser

IJSRD - International Journal for Scientific Research & Development Vol. 4, Issue 07, 2016 ISSN (online):

Broadband Vibration Response Reduction Using FEA and Optimization Techniques

VIBRATION ANALYSIS OF AN AUTOMOTIVE SILENCER

Experimental and Numerical Modal Analysis of a Compressor Mounting Bracket

Computational and Experimental Approach for Fault Detection of Gears

Structural Dynamics. Spring mass system. The spring force is given by and F(t) is the driving force. Start by applying Newton s second law (F=ma).

Modeling and Experimentation: Mass-Spring-Damper System Dynamics

DESIGN AND ANALYSIS OF VIBRATION AND HARSHNESS CONTROL FOR AUTOMOTIVE STRUCTURES USING FINITE ELEMENT ANALYSIS

OPTIMAL DESIGN OF CLUTCH PLATE BASED ON HEAT AND STRUCTURAL PARAMETERS USING CFD AND FEA

Random Eigenvalue Problems in Structural Dynamics: An Experimental Investigation

A Review On Methodology Of Material Characterization And Finite Element Modelling Of Rubber-Like Materials

WORK SHEET FOR MEP311

INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING AND TECHNOLOGY (IJMET)

4. SHAFTS. A shaft is an element used to transmit power and torque, and it can support

EVALUATING DYNAMIC STRESSES OF A PIPELINE

INTRODUCTION TO PIEZO TRANSDUCERS

MEMS Project 2 Assignment. Design of a Shaft to Transmit Torque Between Two Pulleys

DESIGN AND APPLICATION

DETC98/PTG-5788 VIBRO-ACOUSTIC STUDIES OF TRANSMISSION CASING STRUCTURES

e jωt = cos(ωt) + jsin(ωt),

8 Deflectionmax. = 5WL 3 384EI

Address for Correspondence

Vibration modelling of machine tool structures

Dynamic Vibration Analysis of an Isolator

Active elastomer components based on dielectric elastomers

A Study on the Tube of Integral Propeller Shaft for the Rear-wheel Drive Automobile Using Carbon Composite Fiber

An Analysis Technique for Vibration Reduction of Motor Pump

STUDY OF THE EFFECT OF COMPOSITE CONSTRAINED LAYERS IN VIBRATION DAMPING OF PLATES

Nonlinear Elastic Analysis of Structural Frame Under Dynamic Load Condition

Advanced Strength of Materials Prof S. K. Maiti Mechanical Engineering Indian Institute of Technology, Bombay. Lecture 27

Why You Can t Ignore Those Vibration Fixture Resonances Peter Avitabile, University of Massachusetts Lowell, Lowell, Massachusetts

Automated Spur Gear Designing Using MATLAB

Dynamic Analysis on Vibration Isolation of Hypersonic Vehicle Internal Systems

Solution to Multi-axial Fatigue Life of Heterogenic Parts & Components Based on Ansys. Na Wang 1, Lei Wang 2

Design and analysis of axle under fatigue life loading condition

Blade Group Fatigue Life Calculation under Resonant Stresses

DEVELOPMENT OF SEISMIC ISOLATION TABLE COMPOSED OF AN X-Y TABLE AND WIRE ROPE ISOLATORS

Design and Analysis of Adjustable Inside Diameter Mandrel for Induction Pipe Bender

Modal and Harmonic Analysis of Master Leaf Spring

EQUIVALENT SINGLE-DEGREE-OF-FREEDOM SYSTEM AND FREE VIBRATION

Chapter 10: Vibration Isolation of the Source

Structural Dynamics Model Calibration and Validation of a Rectangular Steel Plate Structure

Random vibration analysis and fatigue life evaluation of auxiliary heater bracket

Dynamic Behaviour of the Rubber Isolator Under Heavy Static Loads in Aerospace Systems

Natural vibration frequency of classic MEMS structures

Momin Muhammad Zia Muhammad Idris* *(SEM IV, M.E (CAD/CAM & Robotics), PIIT, New Panvel, India)

Mechatronics. MANE 4490 Fall 2002 Assignment # 1

Transcription:

International Journal of Design and Manufacturing Technology (IJDMT) Volume 7, Issue 3, Sep Dec 2016, pp. 1 11, Article ID: IJDMT_07_03_001 Available online at http://iaeme.com/ijdmt/issues.asp?jtype=ijdmt&vtype=7&itype=3 Journal Impact Factor (2016): 5.7682 (Calculated by GISI) www.jifactor.com ISSN Print: 0976 6995 and ISSN Online: 0976 7002 IAEME Publication DESIGN AND DEVELOPMENT METHODOLOGY OF ADAPTIVE VIBRATION ABSORBER Rushi Vyas, Rajan Zinzala and Hiren Prajapati Institute of Technology, Nirma University, Ahmedabad, Gujarat, India ABSTRACT The aim of this project is to how to reduce vibration through dual cantilever mass mechanism which is call adaptive vibration absorber that is different than the tune vibration absorber. Design incorporates the use of two concentrated masses cantilevered from two rods. The adaptive solution is achieved by moving the two masses along the length of the rod, producing a changing natural frequency for the absorber device. To do so we applied this system to frequency range of 30 to 80 Hz.For our design we take concentrated masses of 1.2 kg. When we change length from 81.5mm to 210 mm. So, our frequency range will be in range of 80 to 30 Hz (natural frequency).we would design the absorber for the setup having maximum acceleration at 50 Hz frequency and observe the amount of vibrations absorbed by it. Key words: Vibration Absorber and FFT Analysis Cite this Article: Design and Development Methodology of Adaptive Vibration Absorber, Rushi Vyas, Rajan Zinzala and Hiren Prajapati International Journal of Design and Manufacturing Technology 7(3), 2016, pp. 1 11. http://www.iaeme.com/ijdmt/issues.asp?jtype=ijdmt&vtype=7&itype=2 1. INTRODUCTION In an engineering application there may be one or multiple motion / power transferring elements. There may be linear, sliding or rotary elements. For any such element, while transferring power/motion there are certain amount of vibrations which are caused. The cause of vibrations may be: - Unbalance, configuration of the system itself, inaccurate machining, improper tolerances of dimensions etc. These vibrations may cause many problems in operation and it may lead to failures too. So it is very necessary to eliminate these vibrations in order to achieve a perfect stable system for power transmission. http://www.iaeme.com/ijdmt/index.asp 1 editor@iaeme.com

Rushi Vyas, Rajan Zinzala and Hiren Prajapati 1.1. Vibration elimination Vibrations can be eliminated completely or partially by attaching an additional system to our element. We can use various dampers, isolators or Absorbers. Damper is a system having very high damping, so the amplitude of vibration decreases by a large amount by adding such stiffness or damping element to our existing system. Isolators are the system which tries to isolate the element or the existing system in order to decrease or completely eliminate the vibrations in our element. While absorbers are the systems that decrease the amount of vibrations simply by using the concept of negative superposition. Superposition is the process of adding the existing vibrations with the vibrations caused by an external system. 1.2. Vibration absorbers As explained earlier the absorber is a system which tries to eliminate vibrations by negative superposition. Basically what happens is: Suppose the nature of my vibrations occurring on an element is X(t) = Asin(wt+Q) So, we can add a particular system which has same nature of vibration function by opposite nature: X (t)=-asin(wt+q) So: x(t)+x (t) = 0 From these example we can say that a perfect vibration absorber absorbs the vibration totally and makes the system vibration free. The variables to look for the vibrations are: Modes, Frequency and damping. The diagram below showss the nature and tendency of an ideal or perfect absorber: 1.1. Vibration elimination http://www.iaeme.com/ijdmt/index.asp 2 editor@iaeme.com

Design and Development Methodology of Adaptive Vibration Absorber An ideal absorber: Absorbers all vibrations, consumes minimum power, has minimum material and cost. 1.3. Types of vibration absorbers Basically there are categories based on nature of frequency and dynamic characteristic of vibration absorbers. On the basis of Nature of frequency the vibration absorber may be Dynamic vibration absorber or static vibration absorber (Tuned vibration absorber). The basic difference between both of these are: In Dynamic vibration absorber the absorbing system senses the vibrations, gives actuating signal accordingly and absorbs vibration in a very high range of frequencies. While for tuned vibration absorber: It is only tuned for a particular frequency and it cannot be used for wide range of frequencies. In the classification based on the dynamic characteristic of vibration absorber may be of: 1) Active vibration absorber, 2) Passive vibration absorber. Active vibration absorber -In active vibration absorber the actuating signal is given to the system that is all masses -In this absorber more power is consumed to actuate -Vibrations of the object may increase or decrease -It may produce negative or positive damping -Forced frequency is applied in this case Passive vibration absorber - In passive vibration type only the actuating signals given is in the form of waves. - Power consumed is less. -Vibration can only decrease in magnitude in this case -It only produces positive damping -Natural frequency is used in this case. In passive type dynamic absorber system there is one more advantage that is we only get positive damping and not the negative damping in order to achieve only decrease in vibration magnitude. So, our design is based on: Adaptive passive dynamic tuned vibration absorber. 2. CONCEPTUALISATION 2.1. Our concept of design The design approach for the adaptive passive tuned dynamic vibration absorber is to make it of the design of double cantilever type. We designed it based on strength and further the length of the cantilever beams are designed based on the natural frequency to be obtained. The double cantilever structure is attached to several other components to make it sense the vibration and actuate thereafter. As shown in the figure, there is a column that supports two cantilever beams containing two point masses each of 1200 gram. http://www.iaeme.com/ijdmt/index.asp 3 editor@iaeme.com

Rushi Vyas, Rajan Zinzala and Hiren Prajapati The point masses suspended creates a bending and due to that there is also a stiffness of this structure. Due to this stiffness there is a natural frequency of the structure itself and thus we can calculate various lengths in order to damp a vibrating system. There are two point masses at the two extreme points of the rods. Two rods are being used one is threadedd and another one is normal rod to constraint the rotational motion of the point mass when the threaded rod is given actuation using motors. For complete vibration absorption we must assure that the vibration absorber system is vibrating on its 1 st mode. There may be several modes in which the system may be vibrating. These are as follows: 2.1. Modes of the structure 2.2. Overall design The overall design consists of the various elements like sensor: In our case we have used the accelerometer ADXL335 sensor, the actuator which is our double cantilever structure, the processor which in our case is the Arduino Uno R3 which can be programmed to get a certain output and there is a stepper motor whichh is used for the actuation purpose connected with Arduino and the mechanical setup. The input of arduino is from the sensor accelerometer ADXL335. http://www.iaeme.com/ijdmt/index.asp 4 editor@iaeme.com

Design and Development Methodology of Adaptive Vibration Absorber 2.3. FFT analysis readings 2.2. Design of vibration absorber 2.3 FFT readings The curve above shows the curve of acceleration v/s frequency which gives magnitude of maximum acceleration at a particular frequency which means maximum force at a particular frequency which is at 50 Hz so that frequency to be damped at is at 50 Hz and corresponding acceleration is to be damped. So the natural frequency of the adaptive tuned dynamic vibration absorber must be equal to the frequency of structure equal to 50 Hz to eliminate the vibrations. http://www.iaeme.com/ijdmt/index.asp 5 editor@iaeme.com

Rushi Vyas, Rajan Zinzala and Hiren Prajapati 3. DESIGN BASED ON STRENGTH The setup which is explained above has some mechanical parts and some electronic part. For the mechanical part we have to provide a sturdy design so as to assure the safe application of the whole setup in action. So the various mechanical elements of the system are designed based on strength. Basically, various iterations are carried out based on the values of diameter of rod and the point mass attached at the end of rod. The factor of safety considered for the design is: 3.5 The point mass is decidedd based on iterations using software MS excel is 600 grams, and the diameter of rod is found out as 4.732 mm which is rounded off as 4.8 mm. The point masses apply the bending on the threaded rods as shown in the figure below. 2.4. Free body diagram of threaded rod So, the forces applied at the centre of the rod is as shown above so it has to be designed based on fatigue because when the setup will be kept on the working conditions there would be vibrations which may cause the mass to go from up and down so it is a case of pure fatigue loading. Pure reversed bending conditions. The first and foremost approximation is the approximation regarding the point masses that we will be using in the apparatus. The weight of each point mass is 1.2 kg. This acts at the extremity of the threaded rod. First component to design is the rod. Rod is designed based on Fatigue criteria. Various derating factors (Ka,Kb,Kc,Kd,Ke) are found out based on the various parameters and the endurance limit is found out from which the diameter of rod is found out and its length is found out using the frequency ranges. Ka = surface finish factor, Kb= size factor, Kc= reliability factor (which is taken as 90%), Kd = Load factor. Factor of safety taken is 3..5. Threaded rods are having less strength than normal rods, so for threaded rod the internal diameter is taken as the diameter obtained based on strength. We have assumed the range of frequency as 30 Hz to 80 Hz and based on that the lengths are also found out using Dunkerley s rule as shown below: http://www.iaeme.com/ijdmt/index.asp 6 editor@iaeme.com

Design and Development Methodology of Adaptive Vibration Absorber 3.1. Analysis part For the analysis purpose we can follow several approaches. The approach may be of discrete type or continuous type. We are following the discrete type approach for ease of analysis and calculations. The assumption we made here is that the threaded rod is fixed from between so each side behaves as a cantilever beam. Thus it is considered as the double cantilever beam for analysis point of view. Dunkerley s rule is applied on it as follows: The two masses at the end as considered as the point masses and the threaded rod is also considered as a cantilever beam. wb of a cantilevered beam of mass, m1 Total stiffness by two rods: Kt = K1 + K2 Where, I= Moment of inertia of rod E = modulus of elasticity of rod L = length of cantilever m= mass due to rod element= (density) X (volume) Due to point mass attached at the end in the cantilever the natural frequency is Where, m is the total mass = 600 g+600 g= 1.2 kg E=modulus of Elasticity of rod L=length at which masses are suspended from middle http://www.iaeme.com/ijdmt/index.asp 7 editor@iaeme.com

Rushi Vyas, Rajan Zinzala and Hiren Prajapati I = moment of inertia From this by keeping a certain value like in our case: Mass (m) = 0.6 kg, E = 200 GPa, L= 150 mm Frequency obtained is 47.56 Hz 3.2. Reasons for consideration of various elements The reason we considered the accelerometer ADXL335 is that the maximum acceleration we obtained using FFT curve was 15 m/s 2 and from the data book of electronics available on internet we found out that the sensor ADXL335 can sense the acceleration of upto +3g to -3g. So it is in our desired range of vibrations and vibrations cannot increasee more than this. The actuator we are using to actuate the point masses in our double cantilever structure is the stepper motor. The reason for using stepper motor is the cost consideration and the signals that can be input in it which are in steps so an exact amount of displacement of the masses can be achieved simply by knowing the least count of actuation of the stepper motor and the pitch of the threads of the threaded rod of double cantilever structure. For programming purpose the controller that we have used is the arduino UNO R3 for its 3.1. Closed loop of the system Cost effectiveness and the serve of our purpose. The mechanical and electric circuit must further become a closed loop system for constant monitoring and correction which can be done by considering this closed circuit. 3.3. Solidworks modelling of the setup For the modelling in the CAD modelling software we have used the software Solidworks for the modelling and we have considered the setup to be completely made up of a column which supports two threaded rods and two point masses attached at the end of the threaded rods. As we know from the analysis part that the length we obtain for 50 Hz frequency is 110 mm so we have kept the massess at 110 mm to import it for analysis purpose. http://www.iaeme.com/ijdmt/index.asp 8 editor@iaeme.com

Design and Development Methodology of Adaptive Vibration Absorber 3.2. Solidworks 3-D modelling 3.4. Ansys vibrational analysis results The model we made on solidworks is imported in Ansys software and the modal analysis of that particular system is done using the numerical FEA method. The figure below shows the meshed model of ansys 3.3. Meshing of model elements The boundary conditions are given as: The base of the structure is fixed. The weight applied is only the masses on the rods. Modal analysis is carried out and displacement and frequency probe are used Mesh size: 5mm Analysis: Finite element method http://www.iaeme.com/ijdmt/index.asp 9 editor@iaeme.com

Rushi Vyas, Rajan Zinzala and Hiren Prajapati Material: For rods: Steel Density: 7850 kg/m3 E = 200 Gpa For column: Cast iron (no need of properties) Boundary conditions: Weight of masses and Fixed support at the bottom. The results of ansys numerical analysis are as follows: 3.4. Ansys solutions The natural frequency obtained in this analysis is 45.39 Hz 3.5. Comparison of analytical and numerical results As shown in the approach above the analytical results show nearly 47.56 Hz and numerical results show as 45.39 Hz Analysis type Natural frequency %error Analytical method 47.56 Hz 4.54 % compared to Numerical method 45.399 Hz analytical The probable reasons for the difference may be: Meshed elements are not that high to get nearer to accurate results, still the error is very less so we can build this structure as it comes nearly equal in analytical and numerical analysis and it satisfactorily matches with the frequency of the base. http://www.iaeme.com/ijdmt/index.asp 10 editor@iaeme.com

Design and Development Methodology of Adaptive Vibration Absorber 4. CONCLUSIONS Adaptive passive tuned dynamic vibration absorber is a very important type of vibration eliminator. It can replace several tuned vibration absorbers just by applying a single unit of it. Design of it is quite complex but it can be implemented to a very high range of varying frequency. Analysis based on analytical method and numerical method using ansys gives almost same results by error of just about 4% Error in both the analysis may be due to the following reasons : Numbers of mesh are very less. Some approximations in case of analytical methods for simplification REFERENCES 1. Design of an adaptive dynamic vibration absorber - Christopher Ting-Kong 2. Ansys structural analysis guide 3. University of Alberta tutorials : Modal analysis of a cantilever beam 4. Modeling of Material Damping Properties in ANSYS by C. CAI, H. Zheng, M. S. Khan and K. C. Hung 5. Experimental Modal Analysis A Simple Non-Mathematical Presentation Peter Avitabile, University of Massachusetts Lowell, Lowell, Massachusetts 6. Fundamentals of modal testing: Agilent technologies 7. Irshad M. Momin, Dr. Ranjit G. Todkar, Design and Development of A Pendulum Type Dynamic Vibration Absorber For A SDOF Vibrating System Subjected To Base Excitation. International Journal of Mechanical Engineering and Technology (IJMET), 6(12), 2015, pp. 36 59. 8. Nattadon Pannucharoenwong and Chawisorn Phukapak, The Performance of Heat Absorber from Zinc on The Efficiency of Double Slope Solar Still. International Journal of Mechanical Engineering and Technology (IJMET), 6(12), 2015, pp. 36 59. 9. A. Nagaraju and Prof. B. Uma Maheswar Gowd, Nusselt Number and Friction Factor Correlations for Solar Air Heater Duct Having Triangular Protrusions as Roughness Elements on Absorber Plate. International Journal of Mechanical Engineering and Technology (IJMET), 6(4), 2015, pp. 35 44. http://www.iaeme.com/ijdmt/index.asp 11 editor@iaeme.com