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Dynamic Vibration Absorber
Dynamic Absorber
F(t)
x1(t)
m1
k1 k2
m2
x2(t)
Primary
system
Secondary
system
Figure: Absorber
www.mechanical-engineering.name
Dynamic Vibration Absorber
Differential equations of motion
From free body diagrams of the masses m1 and m2
m1¨x1 = −k1x1 − k2 (x1 − x2) + Feqsinωt
m2¨x2 = k2 (x1 − x2)
. (1)
Rearranging the Eq.(1)
m1¨x1 + (k1 + k2) x1 − k2x2 = Feqsinωt
m2¨x2 + k2x2 − k2x1 = 0
. (2)
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Dynamic Vibration Absorber
Formulas
For steady state solution, assume solution x1 = X1 sin ωt and
x2 = X2 sin ωt. Substituting for x1 and x2 and their second time
derivatives in Eq.(2), we obtain
k1 + k2 − mω2 X1 − k2X2 sin ωt = Feqsinωt
−k2X1 + k2 − m2ω2 X2 sin ωt = 0 .
(3)
Collecting out common terms and also because sin ωt = 0 at all
time, we get
k1 + k2 − mω2 X1 − k2X2 = Feq
−k2X1 + k2 − m2ω2 X2 = 0 .
(4)
www.mechanical-engineering.name
Dynamic Vibration Absorber
Cramer’s rule
Solving for X1 and X2 using Cramer’s rule, we obtain
X1 =
Feq −k2
0 k2 − m2ω2
∆ω
, X2 =
k1 + k2 − mω2 Feq
−k2 0
∆ω
(5)
The frequency equation is given by
∆ω =
k1 + k2 − mω2 −k2
−k2 k2 − m2ω2 (6)
which semplifies to
∆ω = 0 ⇒ m1m2ω4
− [(k1 + k2) m2 + k2m1] ω2
+ k1k2 = 0 (7)
www.mechanical-engineering.name
Dynamic Vibration Absorber
Frequency equation
Dividing out Eq. (7) by k1k2
m1m2
k1k2
ω4
−
k1 + k2
k1
m2
k2
+
m1
k1
ω2
+ 1 = 0 . (8)
In Eq.(8) the natural frequency of the
main system is ω11 = k1/m1;
auxiliary system is ω22 = k2/m2.
The Eq.(8) may be rewritten as
ω
ω11
2
ω
ω22
2
− 1 +
k2
k1
ω
ω22
2
+
ω
ω11
2
+ 1 = 0 .
(9)
www.mechanical-engineering.name
Dynamic Vibration Absorber
Dynamic Absorber
When the main system and auxiliary system have same natural
frequency ω11 = ω22, let
ω
ω11
= r
ω
ω22
= r . (10)
Letting m2/m1 = µ, Eq.(10) reduces to
r4
− (2 + µ) r2
+ 1 = 0 . (11)
www.mechanical-engineering.name
Dynamic Vibration Absorber
Dynamic Absorber
The new resonance frequencies of tuned system depend on
the mass ratio µ. Let us assume that the resonance occurs at
r ≡ r1 =
ω
ω11
r ≡ r2 =
ω
ω22
. (12)
where the two roots are given by
r2
1 , r2
2 =
2 + µ
2
±
1
2
(2 + µ)2
− 4 . (13)
or
r2
1 , r2
2 = 1 +
µ
2
± 1 +
µ
2
2
− 1 . (14)
When ω11 = ω22, the natural frequencies are given by
ω
ω11
2
= 1 +
µ
2
± 1 +
µ
2
2
− 1 . (15)
www.mechanical-engineering.name
Dynamic Vibration Absorber
Tuned condition
Solving the determinants in Eq.(5) we have



X1 =
Feq k2 − m2ω2
∆ω
=
Feq k2 − m2ω2
k1 + k2 − m1ω2 k2 − m2ω2 − k2
2
X2 =
Feqk2
∆ω
=
Feqk2
k1 + k2 − m1ω2 k2 − m2ω2 − k2
2
.
(16)
www.mechanical-engineering.name
Dynamic Vibration Absorber
Tuned condition
Under tuned condition, substituting k2 = m2ω2, the Eq.(16)
gives



X1 =
Feq · 0
k1 + k2 − m1ω2 · 0 − k2
2
= 0
X2 =
Feqk2
k1 + k2 − m1ω2 · 0 − k2
2
= −
Feq
k2
.
(17)
X2 = −
Feq
k2
⇒ −X2k2 = Feq . (18)
Fspring = Fexternal
www.mechanical-engineering.name
Dynamic Vibration Absorber
Application
A machine runs at 5500 rpm. Its forcing frequency is very
near to its natural frequency.
If the nearest frequency of the machine is to be at least 20
per cent from the forced frequency, design a suitable
vibration absorber for the sistem.
Assume the mass of the machine as m1 = 30 kg.
www.mechanical-engineering.name
Dynamic Vibration Absorber
Application
The natural frequency of the system at 478 rpm is
ωn = 2π
478
60
≈ 50 rad/s . (19)
For 20 per cent variation, we obtain
r1 =
ω
ωn
= 0.8 r2 =
ω
ωn
= 1.2 . (20)
From Eq. (11) we have
0.84
− (2 + µ) 0.82
+ 1 = 0 ⇒ µ = 0.202 . (21)
Mass of auxiliary system is
m2 = µ ⇒ m1 = 0.202 × 30 = 6.06 kg . (22)
Stiffness values
k1 =ω2
n × m1 = 502
× 30 = 75000 N/m
⇒ k2 = ω2
n × m2 = 502
× 6.06 = 15150 N/m . (23)
www.mechanical-engineering.name
Dynamic Vibration Absorber
Matlab: Main
tspan = 0 : 0.05 : 10;
y0 = [0; 0; 0; 0];
[t, y] = ode23( Dabsorber , tspan, y0);
subplot(211);
plot(t, y(:, 1));
xlabel( t(Solid line : x1(t)Dotted line : xd1(t)) )
holdon;
plot(t, y(:, 2), −− );
subplot(212);
plot(t, y(:, 3));
xlabel( t(Solid line : x2(t)Dotted line : xd2(t)) );
hold on;
plot(t, y(:, 4), −− );
www.mechanical-engineering.name
Dynamic Vibration Absorber
Matlab: Function
function f = Dabsorber(t, y)
m1 = 30;
m2 = 0.202 ∗ m1;
omegan = 50;
k1 = omegan ∗ omegan ∗ m1;
k2 = omegan ∗ omegan ∗ m2;
omega = 15 ∗ 2 ∗ pi;
Feq = 10;
F = Feq ∗ sin(omega ∗ t);
f = zeros(4, 1);
f(1) = y(2);
f(2) = F/m1 − ((k1 + k2)/m1) ∗ y(1) + (k2/m1) ∗ y(3);
f(3) = y(4);
f(4) = (k2/m2) ∗ y(1) − (k2/m2) ∗ y(3);
www.mechanical-engineering.name
Dynamic Vibration Absorber
Matlab: FRF
clear all
clc
m1 = 30;
m2 = 0.202 ∗ m1;
omegan = 50;
k1 = omegan ∗ omegan ∗ m1;
k2 = omegan ∗ omegan ∗ m2;
Feq = 10;
k = 31;
X1 = zeros(k, 1);
X2 = zeros(k, 1);
omega = zeros(k, 1);
www.mechanical-engineering.name
Dynamic Vibration Absorber
Matlab: FRF
for m = 1 : k
omega(m) = m;
Deltaomega = m1 ∗ m2 ∗ omega(m)4 − ((k1 + k2) ∗ m2 + k2 ∗
m1) ∗ omega(m)2 + k1 ∗ k2;
X1(m) = Feq ∗ (k2 − m2 ∗ omega(m)2)/Deltaomega;
X2(m) = Feq ∗ k2/Deltaomega;
end
plot(omega, X1, omega, X2); legend( X1, X2); grid;
xlabel( Frequency ); ylabel( Amplityde );
title( Frequency Response Functions );
www.mechanical-engineering.name
Dynamic Vibration Absorber
Time history
0 2 4 6 8 10
−10
−5
0
5
10
t(Solidline: x1(t) Dottedline: xd1(t))
0 2 4 6 8 10
−100
−50
0
50
100
t(Solidline: x2(t) Dottedline: xd2(t))
Figure: Time history
www.mechanical-engineering.name
Dynamic Vibration Absorber
Time history
0 2 4 6 8 10
−2
−1.5
−1
−0.5
0
0.5
1
1.5
2
primary system
secondary system
Figure: Time history
www.mechanical-engineering.name
Dynamic Vibration Absorber
FRF
0 50 100 150 200
−5
0
5
10
x 10
−3
Frequency [rad/s]
Amplityde
Frequency Response Functions
X1
X2
Figure: Frequency Response Function
www.mechanical-engineering.name

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Concrete Mix Design - IS 10262-2019 - .pptxConcrete Mix Design - IS 10262-2019 - .pptx
Concrete Mix Design - IS 10262-2019 - .pptx
 

Dynamic Vibration Absorber Design and Analysis

  • 1. Dynamic Vibration Absorber Dynamic Absorber F(t) x1(t) m1 k1 k2 m2 x2(t) Primary system Secondary system Figure: Absorber www.mechanical-engineering.name
  • 2. Dynamic Vibration Absorber Differential equations of motion From free body diagrams of the masses m1 and m2 m1¨x1 = −k1x1 − k2 (x1 − x2) + Feqsinωt m2¨x2 = k2 (x1 − x2) . (1) Rearranging the Eq.(1) m1¨x1 + (k1 + k2) x1 − k2x2 = Feqsinωt m2¨x2 + k2x2 − k2x1 = 0 . (2) www.mechanical-engineering.name
  • 3. Dynamic Vibration Absorber Formulas For steady state solution, assume solution x1 = X1 sin ωt and x2 = X2 sin ωt. Substituting for x1 and x2 and their second time derivatives in Eq.(2), we obtain k1 + k2 − mω2 X1 − k2X2 sin ωt = Feqsinωt −k2X1 + k2 − m2ω2 X2 sin ωt = 0 . (3) Collecting out common terms and also because sin ωt = 0 at all time, we get k1 + k2 − mω2 X1 − k2X2 = Feq −k2X1 + k2 − m2ω2 X2 = 0 . (4) www.mechanical-engineering.name
  • 4. Dynamic Vibration Absorber Cramer’s rule Solving for X1 and X2 using Cramer’s rule, we obtain X1 = Feq −k2 0 k2 − m2ω2 ∆ω , X2 = k1 + k2 − mω2 Feq −k2 0 ∆ω (5) The frequency equation is given by ∆ω = k1 + k2 − mω2 −k2 −k2 k2 − m2ω2 (6) which semplifies to ∆ω = 0 ⇒ m1m2ω4 − [(k1 + k2) m2 + k2m1] ω2 + k1k2 = 0 (7) www.mechanical-engineering.name
  • 5. Dynamic Vibration Absorber Frequency equation Dividing out Eq. (7) by k1k2 m1m2 k1k2 ω4 − k1 + k2 k1 m2 k2 + m1 k1 ω2 + 1 = 0 . (8) In Eq.(8) the natural frequency of the main system is ω11 = k1/m1; auxiliary system is ω22 = k2/m2. The Eq.(8) may be rewritten as ω ω11 2 ω ω22 2 − 1 + k2 k1 ω ω22 2 + ω ω11 2 + 1 = 0 . (9) www.mechanical-engineering.name
  • 6. Dynamic Vibration Absorber Dynamic Absorber When the main system and auxiliary system have same natural frequency ω11 = ω22, let ω ω11 = r ω ω22 = r . (10) Letting m2/m1 = µ, Eq.(10) reduces to r4 − (2 + µ) r2 + 1 = 0 . (11) www.mechanical-engineering.name
  • 7. Dynamic Vibration Absorber Dynamic Absorber The new resonance frequencies of tuned system depend on the mass ratio µ. Let us assume that the resonance occurs at r ≡ r1 = ω ω11 r ≡ r2 = ω ω22 . (12) where the two roots are given by r2 1 , r2 2 = 2 + µ 2 ± 1 2 (2 + µ)2 − 4 . (13) or r2 1 , r2 2 = 1 + µ 2 ± 1 + µ 2 2 − 1 . (14) When ω11 = ω22, the natural frequencies are given by ω ω11 2 = 1 + µ 2 ± 1 + µ 2 2 − 1 . (15) www.mechanical-engineering.name
  • 8. Dynamic Vibration Absorber Tuned condition Solving the determinants in Eq.(5) we have    X1 = Feq k2 − m2ω2 ∆ω = Feq k2 − m2ω2 k1 + k2 − m1ω2 k2 − m2ω2 − k2 2 X2 = Feqk2 ∆ω = Feqk2 k1 + k2 − m1ω2 k2 − m2ω2 − k2 2 . (16) www.mechanical-engineering.name
  • 9. Dynamic Vibration Absorber Tuned condition Under tuned condition, substituting k2 = m2ω2, the Eq.(16) gives    X1 = Feq · 0 k1 + k2 − m1ω2 · 0 − k2 2 = 0 X2 = Feqk2 k1 + k2 − m1ω2 · 0 − k2 2 = − Feq k2 . (17) X2 = − Feq k2 ⇒ −X2k2 = Feq . (18) Fspring = Fexternal www.mechanical-engineering.name
  • 10. Dynamic Vibration Absorber Application A machine runs at 5500 rpm. Its forcing frequency is very near to its natural frequency. If the nearest frequency of the machine is to be at least 20 per cent from the forced frequency, design a suitable vibration absorber for the sistem. Assume the mass of the machine as m1 = 30 kg. www.mechanical-engineering.name
  • 11. Dynamic Vibration Absorber Application The natural frequency of the system at 478 rpm is ωn = 2π 478 60 ≈ 50 rad/s . (19) For 20 per cent variation, we obtain r1 = ω ωn = 0.8 r2 = ω ωn = 1.2 . (20) From Eq. (11) we have 0.84 − (2 + µ) 0.82 + 1 = 0 ⇒ µ = 0.202 . (21) Mass of auxiliary system is m2 = µ ⇒ m1 = 0.202 × 30 = 6.06 kg . (22) Stiffness values k1 =ω2 n × m1 = 502 × 30 = 75000 N/m ⇒ k2 = ω2 n × m2 = 502 × 6.06 = 15150 N/m . (23) www.mechanical-engineering.name
  • 12. Dynamic Vibration Absorber Matlab: Main tspan = 0 : 0.05 : 10; y0 = [0; 0; 0; 0]; [t, y] = ode23( Dabsorber , tspan, y0); subplot(211); plot(t, y(:, 1)); xlabel( t(Solid line : x1(t)Dotted line : xd1(t)) ) holdon; plot(t, y(:, 2), −− ); subplot(212); plot(t, y(:, 3)); xlabel( t(Solid line : x2(t)Dotted line : xd2(t)) ); hold on; plot(t, y(:, 4), −− ); www.mechanical-engineering.name
  • 13. Dynamic Vibration Absorber Matlab: Function function f = Dabsorber(t, y) m1 = 30; m2 = 0.202 ∗ m1; omegan = 50; k1 = omegan ∗ omegan ∗ m1; k2 = omegan ∗ omegan ∗ m2; omega = 15 ∗ 2 ∗ pi; Feq = 10; F = Feq ∗ sin(omega ∗ t); f = zeros(4, 1); f(1) = y(2); f(2) = F/m1 − ((k1 + k2)/m1) ∗ y(1) + (k2/m1) ∗ y(3); f(3) = y(4); f(4) = (k2/m2) ∗ y(1) − (k2/m2) ∗ y(3); www.mechanical-engineering.name
  • 14. Dynamic Vibration Absorber Matlab: FRF clear all clc m1 = 30; m2 = 0.202 ∗ m1; omegan = 50; k1 = omegan ∗ omegan ∗ m1; k2 = omegan ∗ omegan ∗ m2; Feq = 10; k = 31; X1 = zeros(k, 1); X2 = zeros(k, 1); omega = zeros(k, 1); www.mechanical-engineering.name
  • 15. Dynamic Vibration Absorber Matlab: FRF for m = 1 : k omega(m) = m; Deltaomega = m1 ∗ m2 ∗ omega(m)4 − ((k1 + k2) ∗ m2 + k2 ∗ m1) ∗ omega(m)2 + k1 ∗ k2; X1(m) = Feq ∗ (k2 − m2 ∗ omega(m)2)/Deltaomega; X2(m) = Feq ∗ k2/Deltaomega; end plot(omega, X1, omega, X2); legend( X1, X2); grid; xlabel( Frequency ); ylabel( Amplityde ); title( Frequency Response Functions ); www.mechanical-engineering.name
  • 16. Dynamic Vibration Absorber Time history 0 2 4 6 8 10 −10 −5 0 5 10 t(Solidline: x1(t) Dottedline: xd1(t)) 0 2 4 6 8 10 −100 −50 0 50 100 t(Solidline: x2(t) Dottedline: xd2(t)) Figure: Time history www.mechanical-engineering.name
  • 17. Dynamic Vibration Absorber Time history 0 2 4 6 8 10 −2 −1.5 −1 −0.5 0 0.5 1 1.5 2 primary system secondary system Figure: Time history www.mechanical-engineering.name
  • 18. Dynamic Vibration Absorber FRF 0 50 100 150 200 −5 0 5 10 x 10 −3 Frequency [rad/s] Amplityde Frequency Response Functions X1 X2 Figure: Frequency Response Function www.mechanical-engineering.name