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![Page 1: X.Sun.Presentation](https://reader035.fdocuments.net/reader035/viewer/2022062903/588a33941a28abc6168b5237/html5/thumbnails/1.jpg)
Cantilevered Piezoelectric Energy Harvester – Modeling and Simulation
XIANGZHEN SUN
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IntroductionResearch Topic: Harvesting Energy from ambient
Energy Source: Mechanical Vibration
Material Selection: Piezoelectric materials
Piezoelectric effect:
1. Generate an AC (alternating current) voltage when subjected to mechanical stress or vibration.
2. Vibrate when subjected to an AC voltage, or both.
Usage: Radio wave transmission, remote sensor, transducer, powering small electronic components
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Model Description
Electromechanical Modeling of cantilevered piezoelectric harvesterPZT: composite of piezoelectric and ceramic, improved mechanical properties, high temperature resistant Substructure: protection, vibration magnitude restraintVibration decomposition: small rotation and longitude translation Circuit Model: voltage source + load resistance
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Modeling Methods 1. Coupled Single Degree of Freedom (SDOF)
Transduction Mechanism of vibration – to – electric:
Electromagnetic, Electrostatic, Piezoelectric
• Magnetic seismic mass motion, w.r.t., Generator Housing
• 2 degree of freedom coupled
• Issue: Contradict to experimental result, can not be
governed by merely one equation
𝑚�̈�+𝑐 �̇�+𝑘𝑧=−𝑚�̈�
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Modeling Methods 2. Improved SDOF Energy Harvester Model
Core Idea: Motion Decomposition
Transverse Vibrations
Longitude Vibrations
Governing Equation:
Two correction factors, correcting the base excitation amplitude with a single mode dependent of the distributed mass.
𝑚�̈�+𝑐 �̇�+𝑘𝑧=−𝜇1𝑚 �̈�𝑚 �̈�+𝑐 �̇�+𝑘𝑧=− 𝜅1𝑚�̈�
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Modeling Methods Continue …
Pros:
As indicated, correction coefficient, representive of
the excitation amplitude, w.r.t., distributed mass,
has the right tendency.
Cons:
• Highly dependent on the accuracy of distributed
mass
• It is extremely hard to estimate distributed mass
accurately.
• Susceptible to estimation error
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Modeling Methods 3. Single-Mode Equation based on Distributed Parameter Solution
Core Idea: Instead of using ODE or ODE groups to approximate vibrations, this method makes use of the PDE w.r.t. length ‘x’ & time ‘t’ to govern the motion of vibration
Vibration states, determined by separation of variable (SOP):
Pros: Simplified PDE problem
Shape function along the cantilevered beam:
(x, t) W(x)e j tw
1cosh( ) cos( )
( ) {[cosh( x) cos( x)] [sinh( x) sin( x)]}sinh( ) sin( )
b b
b b
L LW x C
L L
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Modeling Methods Continue …
Time – average power generated:
2 2 2 2 231
2334(1 bL )
b h e AP RR
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Modeling Methods Distributed Parameter Electromechanical Model, with dimensionless modes
Still, SOP is used here to simplify PDE equation, however, the way to separate variables is far more advanced:
(represented by an absolutely and uniformly convergent series of the eigenfunctions)
This time, eigenvalues are governed by the following eigenfunction:
1
( , ) (x) (t)rel r rr
w x t
1( ) cosh( ) cos( ) (sinh( ) sin( )r r r rr rx x x x x
mL L L L L
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Modeling Methods Continue …
If we compare the eigenfuntions in these two successive methods:
(1)
(2)
We can see the form of eigenfunctions are similar, but the previous one only have one mode
, the latter one has numerous.
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Modeling Methods Continue …
Transcendental Trigonometry Equation of Characteristic:
How to solve it?
solve( )………………………………….. only one solution in a single region
fzero( )…………………………………… solution is randomly provided in a selected region
I used “variable steps method”:
//Pseudo codes//
Equ = cos(x) * cosh( x ) + 1;
cos( )cosh( ) 1 0
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Modeling Methods Continue …
x0 = 1.8; h = 0.001; h1 = 3; count = 0; error = 0.01;
For x = x0 – h1 : h : x0 + h1
count = count + 1;
If ( Abs (Equ) < = error )
X( i ) = x
If ( 50 < x < 120 )
x0 = x0 + 5
If ( x >= 120 )
x0 = x0 + 10
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Modeling Methods Dimensionless Frequency Number from equation:
We can see the solution of λ became repetitive from the 75th one, so I can use 75 modes to
approximate the dimensionless modes
cos( ) cosh( ) 1 0
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Modeling Methods To support my idea of using 75 modes to approximate the dimensionless modes, let’s have a look at the Dimensionless quotient in the eigenfunction formula:
, where
We can see from the figure that the
dimensionless quotient starts to slightly
fluctuate around 1 after the 4th value
There is no need to solve infinite solutions!
sinh( ) sin( )cosh( ) cos( )
r rr
r r
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Modeling Methods Mass Normalized Eigenfunction:
Observation:
fluctuation starts to be stable when length
of the beam exceeds 40 mm
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Modeling Methods How to get to the Power vs. frequency plot …
Observation:
When load resistance increases the natural
frequency of the system does not shift with it.
Several resonant frequency appears : not single
2 21
20
2 21
2( )1
2
wr r
r r r rj t
cr r
r r r r c
jmjv t
jjY ej
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Modeling Methods Simulation result, compared with single mode result:
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Thank you