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Mechanische trillingen
LES 9 – MODALE ANALYSE Patrick Guillaume Tel.: 02/ 11/27/2018 MECHANISCHE TRILLINGEN, LES 9, 2005
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Random Excitation Random sequence with Gaussian distribution
Random amplitudes and phases Averaging is needed Converge to flat amplitude spectrum Remark: Force is not flat in general due to interaction with the structure Signal processing errors (leakage errors) Effect of nonlinearities is reduced by averaging MECHANISCHE TRILLINGEN, LES 9, 2005
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Random Noise MECHANISCHE TRILLINGEN, LES 9, 2005
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Uniform Window MECHANISCHE TRILLINGEN, LES 9, 2005
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Hanning Window MECHANISCHE TRILLINGEN, LES 9, 2005
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Burst Random MECHANISCHE TRILLINGEN, LES 9, 2005
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Burst Random with Uniform Window
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Exponential Window MECHANISCHE TRILLINGEN, LES 9, 2005
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Periodic Random / Pseudo-Random Excitation
No leakage errors (periodic signal) in steady-state conditions Averaging is required Pseudo random Constant amplitudes and random phases Averaging is not required MECHANISCHE TRILLINGEN, LES 9, 2005
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Impact Excitation Force transducer and tip Advantages Easy to use
No interaction with structure Force is flat in useful frequency range Relatively inexpensive MECHANISCHE TRILLINGEN, LES 9, 2005
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Impact Excitation Disadvantages Large crest factor
Nonlinearities Limited control of amplitude spectrum MECHANISCHE TRILLINGEN, LES 9, 2005
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Force Window Force window (or transient window)
Remove noise Effect of “Double Hits” MECHANISCHE TRILLINGEN, LES 9, 2005
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Response Window Lightly damped structure Heavily damped structure
Leakage errors Heavily damped structure Remove noise MECHANISCHE TRILLINGEN, LES 9, 2005
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Overzicht EMA EMA = Experimentele Modale Analyse
Stap 1: Experimentele opstelling Stap 2: Opmeten van de FRF’s Stap 3: Bepalen van de modale parameters door bvb. curve fitting Stap 4: Validatie van de resultaten Stap 5: Toepassingen MECHANISCHE TRILLINGEN, LES 9, 2005
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Step 1: Setting Up the Modal Test
Choosing DOFs Suspension Choice of excitation Position/connection of force transducer Mounting the response transducers Transducer conditioning and calibration Setting up the analyzer Range setting Frequency band FRF estimator MECHANISCHE TRILLINGEN, LES 9, 2005
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Step 2: Making the Measurements
Checking the quality of the measurements Noise Nonlinearities? MECHANISCHE TRILLINGEN, LES 9, 2005
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Rigid Body Modes MECHANISCHE TRILLINGEN, LES 9, 2005
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Step 3: Modal Parameter Estimation
SDOF Uncoupled modes MDOF Coupled modes MECHANISCHE TRILLINGEN, LES 9, 2005
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Curve-Fitters for Modal Analysis – MDOF
Two step approach Poles are global parameters Time MDOF (LSCE) Freq. MDOF (PolyMAX) Mode shape vectors are local parameters LSFD MECHANISCHE TRILLINGEN, LES 9, 2005
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Stabilization Diagram
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Least Squares Frequency Domain – LSFD
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Residual terms – LR, UR MECHANISCHE TRILLINGEN, LES 9, 2005
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Step 4: Checking the Model
Synthesized FRF Modal Assurance Criteria MAC MECHANISCHE TRILLINGEN, LES 9, 2005
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PZL Mielec Skytruck (FLiTE Project)
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Stabilization Diagrams
LSCE LSCF (PolyMAX) MECHANISCHE TRILLINGEN, LES 9, 2005
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Mode Shapes (3.17 Hz, 1.62 %) MECHANISCHE TRILLINGEN, LES 9, 2005
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Mode Shapes (8.39 Hz, 1.93 %) MECHANISCHE TRILLINGEN, LES 9, 2005
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Computer Simulations: What if?
Modification simulation Design optimization Response simulation Acoustic noise calculations Fatigue analysis … MECHANISCHE TRILLINGEN, LES 9, 2005
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Dynamic Modelling Process
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FE Model Updating MECHANISCHE TRILLINGEN, LES 9, 2005
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Structural Dynamic Modifications
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Slat Track Optimisation
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Forced Response Simulation
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