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Published byLinette Dawson Modified over 9 years ago
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MECHANICAL VIBRATION MME4425/MME9510 Prof. Paul Kurowski
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TEXT BOOKS REQUIRED RECOMMENDED
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MME4425b web site Design Center web site
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Software used: SolidWorks Design and assembly of mechanisms and structures SolidWorks Simulation (add-in to SolidWorks) Structural analysis Motion Analysis (add-in to SolidWorks) Kinematic and dynamic analysis of mechanisms Excel
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SolidWorks 2012 installation and activation instructions:
Go to Use SEK-ID = XSEK12 Select release When prompted enter serial number for activation
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WHAT IS THE DIFFERENCE BETWEEN
DYNAMIC ANALYSIS AND VIBRATION ANALYSIS?
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DIFFERENCE BETWEEN A MECHANISM AND A STRUCTURE
Structure is firmly supported, mechanism is not. Structure can only move by deforming under load. It may be one time deformation when the load is applied or a structure can vibrate about its neutral position (point of equilibrium). Generally a structure is designed to stand still. Mechanism moves without deforming it components. Mechanism components move as rigid bodies. Generally, a mechanism is designed to move.
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DIFFERENCE BETWEEN A MECHANISM AND A STRUCTURE
STRUCTURES MECHANISMS
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RIGID BODY MOTION
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How many rigid body motions?
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DISCRETE SYSTEM VS. DISTRIBUTED SYSTEM
Mass, stiffness and damping are separated Distributed system Mass, stiffness and damping are NOT separated
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DISCRETE SYSTEM VS. DISTRIBUTED SYSTEM
1DOF.SLDASM DOF.SLDASM Discrete system Mass, stiffness and damping are separated Distributed system Mass, stiffness and damping are NOT separated
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swing arm 01.SLDASM swing arm 02.SLDASM Discrete system Mass, stiffness and damping are separated Distributed system Mass, stiffness and damping are NOT separated
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Discrete system Vibration of discrete systems can be analyzed by Motion Analysis tools such as Solid Works Motion or by Structural Analysis such as SolidWorks Simulation based on the Finite Element Analysis Distributed system Vibration of distributed systems must be analyzed by structural analysis tools such as SolidWorks Simulation based on the Finite Element Analysis.
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SINGLE DEGREE OF FREEDOM SYSTEM
LINEAR VIBRATIONS
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SINGLE DEGREE OF FREEDOM SYSTEM, LINEAR VIBRATIONS
Homogenous equation
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FINDING GENERAL SOLUTION OF HOMOGENEOUS EQUATION
By guessing solution How to solve this? We guess solution based on experience that the solution will be in the form: A – magnitude of amplitude Ф – initial value of sine function ωn – angular frequency
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FINDING GENERAL SOLUTION OF HOMOGENEOUS EQUATION
By guessing solution ωn – natural angular frequency found from system properties Where A and Ф are found from initial conditions
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FINDING GENERAL SOLUTION OF HOMOGENEOUS EQUATION
Using complex numbers method
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FINDING GENERAL SOLUTION OF HOMOGENEOUS EQUATION
Using complex numbers method We have found two solutions to equation and Since is linear, then the sum of two solutions is also a solution Using Euler’s relations: The equation can be re-written as: Where A and Ф are found from initial conditions
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FINDING GENERAL SOLUTION OF HOMOGENEOUS EQUATION
Using Laplace transformation Taking Laplace transform of both sides Using (5), (6)
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Laplace transformation
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Laplace transformation
Inman p 619
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QUANTITIES CHARACTERIZING VIBRATION
Average value of amplitude is But average value of is zero. Therefore, average value of amplitude is not an informative way to characterize vibration. for this reason we use mean-square value (variance) of displacement: Square root of mean square value is root mean square (RMS). RMS values of are commonly used to characterize vibration quantities such as displacement, velocity and acceleration amplitudes.
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QUANTITIES CHARACTERIZING VIBRATION
Displacement Velocity Acceleration These quantities differ by the order of magnitude or more, hence it is convenient to use logarithmic scales. The decibel is used to quantify how far the measured signal x1 is above the reference signal x0
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QUANTITIES CHARACTERIZING VIBRATION
Lines of constant displacement For a device experiencing vibration in the frequency range 2-8Hz: The maximum acceleration is 10000mm/s^2 The maximum velocity is 400mm/s Therefore the maximum displacement is 30mm Lines of constant acceleration Nomogram for specifying acceptable limits of sinusoidal vibration (Inman p 18)
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LINEAR SDOF
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LINEAR SDOF 10kg mass Linear spring 400000N/m Base SDOF.SLDASM
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Results of modal analysis
LINEAR SDOF Results of modal analysis
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Trigonometric relationship between the phase, natural frequency, and initial conditions.
Note that the initial conditions determine the proper quadrant for the phase.
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PENDULUM SDOF
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PENDULUM SDOF Galileo Galilei lived from 1564 to 1642.
Galileo entered the University of Pisa in 1581 to study medicine. According to legend, he observed a lamp swinging back and forth in the Pisa cathedral. He noticed that the period of time required for one oscillation was the same, regardless of the distance of travel. This distance is called amplitude. Later, Galileo performed experiments to verify his observation. He also suggested that this principle could be applied to the regulation of clocks.
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PENDULUM SDOF pendulum 02.SLDPRT
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PENDULUM SDOF Equations of motion method
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The energy method is suitable for reasonably simple systems.
The energy method may be inappropriate for complex systems, however. The reason is that the distribution of the vibration amplitude is required before the kinetic energy equation can be derived. Prior knowledge of the “mode shapes” is thus required.
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PENDULUM SDOF Energy method
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TORSIONAL SDOF
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TORSIONAL SDOF polar moment of inertia of cross-section disk 01.SLDPRT
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TORSIONAL SDOF
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ROLER SDOF roler.SLDASM Inman p 32
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ROLER SDOF
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ROLER SDOF Inman p 32 k = k1 + k2 = 2000N/m m = 75.4kg r = 0.1m
J = kgm2
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ROLER SDOF
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MASS AT THE END OF BEAM rotation.SLDASM
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MASS AT THE END OF BEAM mass 2.7kg cantilever.SLDPRT
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RING Ring.SLDASM
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HOMEWORK 1 Derive equation of motion of SDOF using energy method
Find amplitude A and tanΦ for given x0, v0 Find natural frequency of cantilever, l=400mm, Φ=5mm, E=2e11Pa, m=2.7kg. Confirm with SW Simulation Work with exercises in chapter 19 – blue book
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TORSONAL SDOF TRIFILAR
1060 alloy Model file trifilar.sldasm Configuration trifilar Model type solid Material as shown Supports as shown Objectives Find the natural frequency of trilifar Fixed support Custom material E = 10MPa ρ = 1kg/m3 very soft, very low density 1060 alloy Restraint in radial direction to force torsional mode trifilar.SLDASM
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TORSIONAL SDOF BIFILAR
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TORSIONAL SDOF TRIFILAR
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TORSIONAL SDOF TRIFILAR
Using energy method:
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TORSIONAL SDOF TRIFILAR
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TORSONAL SDOF TRIFILAR
Trifilar can be used to find moments of inertia of objects placed on rotating platform
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spur gear.SLDPRT
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