ba 7679-13, 1 structural dynamics testing on pulse using me'scope
TRANSCRIPT
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BA 7679-13, 1
Structural Dynamics Testing on PULSE using ME'scope
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Structural Dynamic Testing Term differentiating it from Static Analysis and Testing Modal Analysis and Modal Testing Operational Deflection Shapes
Objectives What is Modal Testing Why do Modal Testing How to do Modal Testing Brüel & Kjær Solution to Modal Testing
Structural Dynamic Testing
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Modal Analysis vs Operational Deflection Shapes
Modal Analysis
– artificial excitation (hammer, 1 or more shakers)
– input force is well known (“under our control”)
Operational Deflection Shapes
– investigation (visualisation) of structure behaviour under “running conditions”
– input forces not known and complicated to describe
Structural Dynamic Testing
Input
Output
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Present day demands Increasing speed in transportation Higher fuel economy Both demands achieved by reducing the mass of structures
Consequences Structures become inherently weak Resonances move down into frequency regions of excitation
forces Structures fail because of dynamic loads Statics studied for over a century
Introduction to Modal Testing
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Modal Testing
What
Why
How
Brüel & Kjær Solution
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Definition of Modal Testing
To construct a mathematical model of the vibrational properties and behaviour of a
structure by experimental means
Natural Frequency
Modal Damping
Residues
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Modal Parameters
Theoretician Eigenvalue Percent Damping Eigenvector
Experimentalist Natural Frequency Loss Factor Mode Shape
Frequency
Distance
Amplitude
Frequency Domain ViewModal
Domain
V
iew
FirstMode Second
ModeThirdMode
Force
Beam
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Modal Testing
What
Why
How
Brüel & Kjær Solution
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Frequency Response Function
Trouble Shooting
Vibration responseduring operation
High responses
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What if … scenarios
Structural Dynamics ModificationMass
Stiffness
Tuned absorber
Move resonance frequency
Forced Response Simulation
How will a structure behave when one or more forces are applied?
SDM and FRS (Assumes validated Modal Model)
High response Low responsePreviousresponse
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Why do Modal Testing
Trouble shooting– To reduce excessive vibration levels
FE-modelling– To ensure resonances are away from excitation frequency
– Validation by testing on prototypes
– Refinement of the mathematical model through inclusion of damping
– Prerequisite in aircraft industry
– Today also commonly used in automotive industry Structural assembly analysis
– To predict the dynamic behaviour of assembled sub-components Simulation of “what if” scenarios
– Determination of forces
– Response to complex excitation
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What
Why
How
Brüel & Kjær Solution
Modal Testing
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How to do Modal Testing
Modeling Geometry Degree of Freedom definition X or XYZ direction
Measurements Frequency Response Functions Hammer or shaker excitation Coherence Function for validation
Curve fitting Frequency Damping Residues
Validation MAC (Modal Assurance Criteria) Modal Confidence Factor Phase Scatter ........
1
2
3
4
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ExcitationResponse
ForceMotion
InputOutput
H() = = =
Determination of the inherent properties of the system
Excitation of the system by a known force Measurement of the Output Relating the Output to the Input
Frequency Response Function:
The FRF shows the inherent properties of a dynamic system — independent of the excitation force and type
System Analysis
Input
Output
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Frequency Response Function
Input
Output Time DomainFrequency Domain
Frequency Response H1(Response,Excitation) - Input (Magnitude)Working : Input : Input : FFT Analyzer
0 200 400 600 800 1k 1,2k 1,4k 1,6k
100m
10
[Hz]
[(m/s²)/N]Frequency Response H1(Response,Excitation) - Input (Magnitude)Working : Input : Input : FFT Analyzer
0 200 400 600 800 1k 1,2k 1,4k 1,6k
100m
10
[Hz]
[(m/s²)/N]
Autospectrum(Excitation) - InputWorking : Input : Input : FFT Analyzer
0 200 400 600 800 1k 1,2k 1,4k 1,6k
100u
1m
10m
100m
1
[Hz]
[N] Autospectrum(Excitation) - InputWorking : Input : Input : FFT Analyzer
0 200 400 600 800 1k 1,2k 1,4k 1,6k
100u
1m
10m
100m
1
[Hz]
[N]
Autospectrum(Response) - InputWorking : Input : Input : FFT Analyzer
0 200 400 600 800 1k 1,2k 1,4k 1,6k
1m
10m
100m
1
10
[Hz]
[m/s²] Autospectrum(Response) - InputWorking : Input : Input : FFT Analyzer
0 200 400 600 800 1k 1,2k 1,4k 1,6k
1m
10m
100m
1
10
[Hz]
[m/s²]
Time(Excitation) - InputWorking : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-200
-100
0
100
200
[s]
[N] Time(Excitation) - InputWorking : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-200
-100
0
100
200
[s]
[N]
Time(Response) - InputWorking : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-80
-40
0
40
80
[s]
[m/s²] Time(Response) - InputWorking : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-80
-40
0
40
80
[s]
[m/s²]
FFT
FFT
Impulse Response h1(Response,Excitation) - Input (Real Part)Working : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-2k
-1k
0
1k
2k
[s]
[(m/s²)/N/s]Impulse Response h1(Response,Excitation) - Input (Real Part)Working : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-2k
-1k
0
1k
2k
[s]
[(m/s²)/N/s]
InverseFFT
ExcitationResponse
ForceMotion
InputOutput
H() = = =
FrequencyResponseFunction
ImpulseResponseFunction
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Modal Model – Global Parameters
Natural Frequency and Modal Damping
0 = 2f0
FrequencyT
Time
Frequency Domain Time Domain
Damping Ratio:
Natural Frequency: Natural Frequency:
Damping Ratio:
3dB
0
0
T
1f0
3 dB bandwidth= 2
Decay Rate =1
0
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Modal Model – Local Parameters Residues
Residue: The “strength” of the mode
Frequency
H(0)
Frequency
Distance
Amplitude
Frequency Domain ViewModal
Domain
V
iew
FirstMode Second
ModeThirdMode
ForceBeam
Residue: R = H(0) ·
Driving point Residue: Riir = a · ir2
General Residue: Rijr = a · ir · jr
The Driving point Residue scales the Mode Shape
0
2
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Excitation TechniqueShaker excitation
Small homogenous structures Quick Polyreference technique Fast method - no fixtures required
......................
......................
......................
...H......HH
H
n11211
.............H
...................
.............H
.............H
H
1n
21
11
Out
In Out
In
Multichannel response orresponse points may be moved
Large or complex structures Various excitation signals possible Time consuming - installation work
to be done
Hammer excitation
Excitation moved
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Curve Fitting
Single Degree of Freedom (SDOF) Simple structure Few and widely spaced modes
Multi Degree of Freedom (MDOF) Multiple modes Many and close modes
Local Based upon one single DOF
Global Based upon multiple DOF’s
Polyreference Symmetric structures exhibit multiple modes at the same frequency One single peak does not necessarily mean one mode
Frequency Response H1(Response,Excitation) - Input (Magnitude)Working : Input : Input : FFT Analyzer
0 200 400 600 800 1k 1,2k 1,4k 1,6k
100m
10
[Hz]
[(m/s²)/N]Frequency Response H1(Response,Excitation) - Input (Magnitude)Working : Input : Input : FFT Analyzer
0 200 400 600 800 1k 1,2k 1,4k 1,6k
100m
10
[Hz]
[(m/s²)/N]
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How to do Modal TestingModeling Geometry Degree of Freedom definition X or XYZ direction
Measurements Frequency Response Functions Hammer or shaker excitation
Curve fitting Frequency Damping Residues
Validation MAC (Modal Assurance Criteria) Modal Confidence Factor Phase Scatter ........
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Modal Testing
What
Why
How
Brüel & Kjær Solution
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The Brüel & Kjær Solution
PULSE
Modal TestConsultant
ModalSoftware
VibrationData
FileTransfer
PULSE
inside
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Brüel & Kjær Solution
Predefined projects for typical hammer, shaker tests
Contains predefined measurement setup trigger conditions, weighting functions, multi-buffer
Easy data display using workbook layouts Time, Autospectra, FRF H1, H2, H3, Coherence FRF Display of Magnitude and Phase, Real and
Imaginary, Nyquist plot
PULSE Software
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PULSE Modal Test Consultant
Features and Benefits Geometry driven measurement
– with the option of importing geo- metry from CAD data
Intuitive graphic control of analyzer parameters
Cuts your setup and measurement time in half
Modal data acquisition your way – comprehensive choice of Modal
Post-processing packages
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PULSE Modal Test Consultant
The Modal Test Consultant based on PULSE gives the user:
Brüel & Kjær PULSETM
OLE Automation
Openness
Scalability
Modularity
Productivity
Ease of use
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Setting up measurements
Transducer mounting guided by geometry model on screen
Graphic supported set-up of
measurement parameters
Audio and visual notification of measurement status
Automatic DOF labeling
– label while measuring
PULSE Modal Test Consultant
Mounting the transducer
Geometry model on screen
Time weighting
Overload indication
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Easy Scaling and Set-up of Hammer Excitation
1 Autorange or select Input Range
2 Select Trigger Level
3 Choose Time Weighting
4 Set Pre-trigger
Hit the test object in a number of different places and …..
Hit the test object once and …..
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Create Test Model from geometry
Geometry creation Import geometry via DXF and
UFF file format Easy-to-use geometry
drawing tools
Test Model Assign DOFs to geometry
Export Geometry model DOF information
PULSE Modal Test Consultant
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PULSE Modal Test Consultant
Measurements are guided by a geometrical model
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Set up of signal parameters using tables*
PULSE Test Consultant for Modal
* The tables can be customizer to suit individual needs
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Auto-ranging signals using graphic support
Set up Measurement conditions
PULSE Test Consultant for Modal
Time weighting Transient Exponential Hanning, ...
Automated TransducerCalibration
Trigger conditions Trigger level (impact test) Pre-trigger
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Data transfer to modal software
Data transfer of geometry model and DOF
information measurement data
Via file transfer Universal File ASCII Universal File Binary Star Binary SDF
Via OLE automation Automatic transfer to ME´scope
PULSE Modal Test Consultant
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Via file transfer Universal File ASCII Universal File Binary Star Binary SDF
Via OLE automation Automatic transfer to ME´scope
(Bridge to ME’scope)
Measurement data transfer to modal software
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PULSE Modal Test Consultant
Automatic Data Transfer to modal software
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PULSE Modal Test Consultant
The Modal Test Consultant link PULSE to major modal analysis post processing tools
File Transfer
Brüel & Kjær PULSETMOLE Automation
ME’scopeTM
OLEAutomation
STAR, I-DEASTM
Reuse of existing software Post-processing of modal data as an integral part of
Modal Testing
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Create test model from geometry Set up measurement conditions Perform measurements Transfer data to modal software
Geometry driven reliable Modal Testing results
PULSE Modal Test Consultant
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Brüel & Kjær PULSETM ME’scopeTM
PULSE Bridge to ME’scope
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Automatic Measurement Data Transfer
Load PULSE Project Export to MEScope
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Modal Software
Available through Brüel & Kjær:
STAR (Spectral Dynamics)
The STAR SystemTM Modal and Structural Analysis - Type 7750
ME’scopeTM (Vibrant Technology, Inc)
Brüel & Kjær ME’scope - Type 7754
I-DEASTM Master Series (MTS) I-DEAS Test
Openness to other software:
ICATS (Imperial College, London)
LMS
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Modal Analysis software
Beyond Modal Testing
Obtain modal parameters Natural Frequency Modal Damping Residues (Mode shape)
Validate modal parameters Phase Scatter MAC Modal Confidence Factor
Simulations Add mass Change stiffness Tuned absorbers
Validate FEM Models
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Conclusion to Modal Testing
Obtain Modal Model
Trouble shooting, FE Modeling, Structural assembly analysis, SDM and FRS
Modeling, System Analysis Measurements,Curve fitting, Validation of Modal Model
PULSE Modal Bridge to ME’scope Modal Test Consultant
Brüel & Kjær Solution
Why
How
What
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Investigation (visualisation) of structure behaviour under “running conditions”
Powerfull trouble-shooting tool
Phase information needed Data to be measured:
– phase assigned spectra (f.ex.between response point and tacho (reference))
or
– FRF between response point / reference point
or
– Cross spectra
No Curve - fitting
Operational Deflection Shapes
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Via file transfer Universal File ASCII Universal File Binary Star Binary SDF
Via OLE automation Automatic transfer to ME´scope
(Bridge to ME’scope)
Measurement data transfer to ODS /modal sw
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Literature for Further Reading
Frequency Analysis by R.B.Randall(Brüel & Kjær Theory and Application Handbook BT 0007-11)
Modal Analysis of Large Structures - Multiple Exciter Systems by K. Zaveri(Brüel & Kjær Theory and Application Handbook BT 0001-12)
Modal Testing: Theory and Practice by D.J. Ewins(Brüel & Kjær Theory and Application Handbook BT 0015-12)
Dual Channel FFT Analysis by H. Herlufsen(Brüel & Kjær Technical Review No. 1 & 2, 1984)
Structural Testing, Part 1: Mechanical Mobility Measurement by O. Døssing
(Brüel & Kjær Theory and Application Booklet BR 0458-12)
Structural Testing, Part 2: Modal Analysis and Simulation by O. Døssing
(Brüel & Kjær Theory and Application Booklet BR 0507-11)