Mostafa S. Abd Elwahabusers.encs.concordia.ca/~sedagha/researchgroup_website/mostafa_… · Mostafa...

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Mostafa S. Abd ElwahabMaster of Science in Mechanical Engineering

Teaching and Research AssistantDepartment of Mathematical Science

German University in Cairo (GUC)

Outline Definition of vibration.

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4546

!()(#

&% 7

* &*"#+

8'

9'

* "#+,#-

*

!()(#

8' /#'12),(

∂∂=

ttxw

CFd

9' "0/1

2),(

∂∂

ttxw

Fdα

*#.7

= dxFW dd UWd

πη

2= "

: :

&%%6

djEEE η+=*djGGG γ+=*

"

-

"

"%

;

" %

. /)((

"

,-

,

(

,-

#

&% &%"01$!2&)"2!2&

3)"

6 /1

/1

%!

3)"

"

,-

,

$/1

)()()()(

2

2tFtKw

dttdw

Cdt

twdm =++

# (

%<

% < % ))!)% % ) ! '

(

%% !

=

%% !

$

%% !

&( #$)>8)8?@A

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$)#

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&

8' !

9' !

at rest in bending vibration

4* ! 3)%5

' /1

0),(

)(),(

)( 4

4

2

2=

∂∂+

∂∂

x

txwEI

t

txwAρ

*

= " /1

7

!

%

at rest in bending vibration

4* ! 3)%5

' /1

0),(

)(),(

)(),(

)( 4

4

4

4

2

2=

∂∂+

∂∂+

∂∂

x

txwEIj

x

txwEI

t

txwA ηρ

*

= " /1

7

!

Undeformed Deformed

Rubberlike material

structure

' /1

% %

4* ! 3)%5

0),(

)(),(

)(),(

)( 4

4

4

4

2

2=

∂∂+

∂∂+

∂∂

x

txwEIj

x

txwEI

t

txwA ηρ

*

= " /1

7

Undeformed Deformed

Rubberlike material

structure

' /1

% %

0),(

)(

),()(

),()(

4

4

4

4

2

2

=∂

∂++

∂∂++

∂∂+

x

txwIEEIj

x

txwIEEI

t

txwAA

ddd

dddd

ηη

ρρ

*= "

/1

Merits: loss factor is not function in mode of vibration.

Limitations: Low loss factor ( 0.8*0.5) in best designs

dd

ddds IEEI

IE+

=ηη

4* ! 3)%5

7

Constraining layer

Structure

Damping layerNote the shear strain

h1h

2

h3

Undeformed Deformed

' ! / 1

=B "7

)1()2(1 2d

dsigYg

gY

ηηη

++++=

0),(),(),(

)1(),(

2

2

22

4

4

4

6

6=

∂∂−

∂∂∂+

∂∂+−

∂∂

t

txwDmg

tx

txwDm

x

txwYg

x

txw

tt

"%

.

% %$%

bIEIE

Dt3311 +

=

Merits: Better loss factor

Limitations: Mode dependency

4* ! 3)%5

6* $5

%$% % 6!

&% "$/!"$!/$7!

6* $5

"($(/"1-%$%%%

&% "$/!"$!/$7!

" "($(,""8--% $%%%

6* $5

" +- $%!

&% "$/!"$!/$7!

6* $5

&% "$/!"$!/$7!

%."

%'%

γp

Piezoelectric actuator(Constraining layer)

Vs

cV

Am

plifi

er

Viscoelastic layer

Piezoelectric sensor

Base beam

γc

$57(#

,$7#-

$57(#

,$7#-

cγp

Piezoelectric sensor

Base beam

Vs

cV

Am

plifi

er

Piezoelectric actuator(Constraining layer)Viscoelastic layer

γ

$57(#

,$7#-

=B"7

0),(),(),(

)1(),(

2

2

22

4

4

4

6

6=

∂∂−

∂∂∂+

∂∂+−

∂∂

t

txwDmg

tx

txwDm

x

txwYg

x

txw

tt

This equation is identical to the equation of the Beam/PCLD system

So, what is new in the technique of ACLD??

&%$%=C#-+C#*&*C#%

=% =C#-+C#&-C"&-&.+!=D)/8??E1

0<dtEd n

Total Energy of the Beam/ACLD system

ttxu

k agp ∂

∂−= ),(ε

$57(#

,$7#-

=

0),(),(),(

)1(),(

2

2

22

4

4

4

6

6=

∂∂−

∂∂∂+

∂∂+−

∂∂

t

txwDmg

tx

txwDm

x

txwYg

x

txw

tt

% %)% 7

0)(

)()(

)()()(

2

22

2 3

3

4

4

5

5

=

−+Ω−−+

Ω

ΩΩΩ

xW

dxxdW

YjQdx

xWdj

dx

xWd

dx

xWd

tDm

gtDm

gYQ

g

Qj

21hK

gYtDgKQ =

The proportional

Control gain2

312

hhhh

++=

Mode shape

Geometrical Parameter

tDKKhKK

Y)( 31

231

+=111 hEK =

333 hEK =

Shear Parameter

312

31 )(KKh

KKGg d +=

Exciting frequency

=B"7

=

=B

=B

=7

6'=

New Approach for Vibration Control in Elastic Structures

y

x

x

L

dx

w(x,t)

p(x,t)

F(x,t)=F0

F(x,t)=F0

&%% $9$71&+2/"#$"%&'+2/% %!

Damping Material

Damping Material

BeamBase

Technique used for generating axial uniform damping force

New Approach for Vibration Control in Elastic Structures

Damping Material

Damping Material

BeamBase

Technique used for generating axial uniform damping force

New Approach for Vibration Control in Elastic Structures

Damping Material

Damping Material

BeamBase

Technique used for generating axial uniform damping force

New Approach for Vibration Control in Elastic Structures

Damping Material

Damping Material

BeamBase

0),( FtxF =

0),( FtxF =

Technique used for generating axial uniform damping force

New Approach for Vibration Control in Elastic Structures

This technique is called Pre-Tensioned Layer Damping

(PTLD)

7

New Approach for Vibration Control in Elastic Structures

6 %

=

EIt

txw(

),() 2

2+

∂∂

0),(

) 4

4=

∂∂

x

txwAρ(

*= "

/1

ηEIj(+4

4 ),()

x

txw

∂∂

7

New Approach for Vibration Control in Elastic Structures

6 A %$ %

0),(

2 2

2

0 =∂

∂+x

txwFEI

t

txw(

),() 2

2+

∂∂

4

4 ),()

x

txw

∂∂Aρ(

*= "

/1

ηEIj(+4

4 ),()

x

txw

∂∂

6 %

7

New Approach for Vibration Control in Elastic Structures

%$% /%! 1

%$ /=B1dη

0),(

)(),(

)(),(

)( 4

4

4

4

2

2=

∂∂++

∂∂++

∂∂+

x

txwIEEIj

x

txwIEEI

t

txwAA ddddddd ηηρρ

*= "

/1

6 %

7

New Approach for Vibration Control in Elastic Structures

6 %

0),(

)(),(

)(),(

)( 4

4

4

4

2

2=

∂∂++

∂∂++

∂∂+

x

txwIEEIj

x

txwIEEI

t

txwAA ddddddd ηηρρ

*= "

/1 :2

2

0),(

2x

txwF

∂∂+

00 εdd AEF =

)1( dd jE η+

* %$%%6)%%

%

9A

7

New Approach for Vibration Control in Elastic Structures

6 %

* %$%%6)%%

%

0),(

)(),(

)(),(

)( 4

4

4

4

2

2=

∂∂++

∂∂++

∂∂+

x

txwIEEIj

x

txwIEEI

t

txwAA ddddddd ηηρρ

*= "

/1 :2

2

02

2

0),(

2),(

2x

txwAEj

x

txwAE ddddd ∂

∂+∂

∂ ηεε

9A

-7

New Approach for Vibration Control in Elastic Structures

-/-1

[ ]∞

=

++Ω−++=Ω

1222222

)()(

),(n

nfddfdn

n

xWj

mLP

xωωηωωω

α

mLCAE ndd

f02 2 εω =

Main Effect

Secondary Effect

-7

New Approach for Vibration Control in Elastic Structures

-/-1%4

[ ]∞

=

++Ω−++=Ω

1222222

)()(

),(n

nfddfdn

n

xWj

mLP

xωωηωωω

α

mLCAE ndd

f02 2 εω =

7

New Approach for Vibration Control in Elastic Structures

ndnd

d

ndnd

d

s

CALIEE

I

CALI

04

04

2)2(

2)2(

εβ

εβηη

++

+=

-7

New Approach for Vibration Control in Elastic Structures

-/-1%6

FFT Analyser

CH 1CH 2Source

Disk drive hp ploter

Power Amp.

Shaker

Moving Base

AccelerometerInductive Pickup

Fixed Base

Charge Amp.

Voltage Amp.

Beam

HPIB CableHPIB Cable

y(t)b

by(t)..

by(t)

y

y

y

(Dual channel)

Harmonic signal generator

plotter

Experimental Implementation of the PTLD Technique

• Schematic drawing of test set-up and instrumentation

• Experimental set-up

Experimental Implementation of the PTLD Technique

Experimental Implementation of the PTLD Technique

002.00 =ε

Experimental Implementation of the PTLD Technique

008.00 =ε

Experimental Implementation of the PTLD Technique

016.00 =ε

Effectiveness of the New Technique

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