Upload
janna-pierce
View
42
Download
2
Tags:
Embed Size (px)
DESCRIPTION
Unit 18. Force Vibration Response Spectrum. Introduction. SDOF systems may be subjected to an applied force Modal testing, impact or steady-state force Wind, fluid, or gas pressure Acoustic pressure field Rotating or reciprocating parts Rotating imbalance Shaft misalignment Bearings - PowerPoint PPT Presentation
Citation preview
Vibrationdata
1
Unit 18
Force Vibration Response Spectrum
Vibrationdata
2
Introduction
SDOF systems may be subjected to an applied force Modal testing, impact or steady-state force Wind, fluid, or gas pressure Acoustic pressure field Rotating or reciprocating parts
Rotating imbalance
Shaft misalignment
Bearings
Blade passing frequencies
Electromagnetic force, magnetostriction
VibrationdataSDOF System, Applied Force
3
m = mass
c = viscous damping coefficient
k = stiffness
x = displacement of the mass
f(t) = applied force
)t(fkxxcxm
Governing equation of motion
VibrationdataRayleigh Peak Response Formula
4
Tfnln2nc
nc
5772.0ncnC
nnC Maximum Peak
fn is the natural frequency
T is the duration
ln is the natural logarithm functionis the standard deviation of the oscillator responsen
Consider a single-degree-of-freedom system with the index n. The maximum response can be estimated by the following equations.
VibrationdataSteady-State Response to Sine Force
5
222 21
1
F
xk
The normalized displacement is
nf/f
The natural frequency fn is
1 kfn
2 m
f is the applied force frequency
fn is the natural frequency
where F is the applied force magnitude
VibrationdataSteady-State Response to Sine Force (cont)
6
The transmitted force to ground ratio is
222
2t
21
21
F
F
where
Ft is the transmitted force magnitude
F is the applied force magnitude
nf/f,
The transmitted force ratio is the same as that for the acceleration response to base excitation.
Vibrationdata
7
0.01
0.1
1
10
20
0.1 1 10
Q = 10Q = 2Q = 1
FREQUENCY ( f / fn )
DIS
PL
AC
EM
EN
T M
AG
NIT
UD
E [
k x
/ F
]
SDOF STEADY-STATE RESPONSE TO APPLIED SINUSOIDAL FORCE
Low Freq Resonance High Freq
Stiffness Damping Mass
Control by Frequency Domain
Vibrationdata
8
0.01
0.1
1
10
20
0.1 1 10
Q = 10Q = 2Q = 1
FREQUENCY ( f / fn )
TR
AN
S F
OR
CE
MA
G
| F
t / F
|SDOF STEADY-STATE TRANSMITTED FORCE
VibrationdataExercise
9
vibrationdata > Miscellaneous Functions >
SDOF Response: Steady-State Sine Force or Acceleration Input
Practice some sample calculations for applied force using your own parameters.
Try resonant excitation and then +/- one octave separation between the excitation and natural frequencies.
VibrationdataSDOF Response to Force PSD, Miles Equation
10
4/3
k
14/1
m
12/1
8
Ax RMS
m is the mass
k is the stiffness
is viscous damping ratio
Ais the amplitude of the force PSD in dimensions of [force^2 / Hz] at the natural frequency
The overall displacement x is
where
Miles equation assumes that the PSD is white noise from 0 to infinity Hz.
VibrationdataMiles Equation, Velocity & Acceleration
11
RMSRMS xx nThe overall velocity is
• An accelerance FRF curve is shown for a sample system in the next slide
• The normalized accelerance converges to 1 as the excitation frequency becomes much larger than the natural frequency
• The acceleration response would be infinitely high for a white noise force excitation which extended up to an infinitely high frequency
• A Miles equation for the acceleration response to a white noise applied force cannot be derived
Vibrationdata
Miles Equation, Acceleration
12
0.001
0.01
0.1
1
10
100
1 10 100 1000
EXCITATION FREQUENCY (Hz)
AC
CE
LE
RA
NC
E (
m
/se
c2
/ N
)
ACCELERANCE MAGNITUDE ( ACCELERATION / FORCE )SDOF SYSTEM: mass= 1 kg fn = 100 Hz Damp = 0.05
VibrationdataSDOF Response to Force PSD, General Method
13
Displacement
Velocity
N
1iiiPSD
2i
22i
nRMS f)f(F
21
1
k
1,fx
N
1iiiPSD
2i
22i
2i
nRMS f)f(F
21
f
k
2,fx
nii f/f,
VibrationdataSDOF Response to Force PSD, General Method
14
Acceleration
Transmitted Force
N
1iiiPSD
2i
22i
2i
nRMS f)f(F
21
21,ftF
nii f/f,
N
1iiiPSD
2i
22i
4i
2
nRMS f)f(F
21
f
k
4,fx
Vibrationdata
Force PSD
15
Frequency (Hz)
Force (lbf^2/Hz)
10 0.1
1000 0.1
Duration = 60 sec
The same PSD was used for the time domain calculation in Webinar 17.
VibrationdataSDOF Example
16
Mass = 20 lbm, Q=10,
Natural Frequency = independent variable
Apply the Force PSD on the previous slide to the SDOF system.
Duration = 60 seconds (but only affects peak value)
Vibrationdata
SDOF Response to Force PSD, Acceleration
17
vibrationdata > Power Spectral Density > Force > SDOF Response to Force PSD
Response at 400 Hz agrees with time domain result in previous webinar unit.
fn (Hz)
Accel (GRMS)
100 0.80
200 1.0
400 1.3
Vibrationdata
18
SDOF Response to Force PSD, Transmitted Force
Vibrationdata
Acceleration VRS
19
vibrationdata > Power Spectral Density > Force > Vibration Response Spectrum (VRS)
fn (Hz)
Accel (GRMS)
100 0.80
200 1.0
400 1.3
Vibrationdata
Velocity VRS
20
Vibrationdata
Displacement VRS
21
Vibrationdata
Transmitted Force VRS
22
VibrationdataHomework
23
Repeat the examples in the presentation using the Matlab scripts