Using Fatigue to Compare Sine and Random Environments

Slides:



Advertisements
Similar presentations
Extending Steinberg’s Fatigue Analysis
Advertisements

ASSIGNMENT 4 Problem 1 Find displacement and stresses in the crankshaft when engine runs at the first natural frequency of the crankshaft.
Review. 2 TEST A 1.What is the single most important property of vibrating structure? 2. What happens when structure is vibrating in resonance? 3.What.
Unit 3 Vibrationdata Sine Sweep Vibration.
Rainflow Cycle Counting for Random Vibration Fatigue Analysis
Shock Special Topics Unit 42 Vibrationdata 1.Accidental Drop Shock 2.Half-Sine Shock on Drop Tower 3.Half-Sine Shock on Shaker Table 4.Waveform Reconstructions.
Vibrationdata 1 Unit 22 Integration and Differentiation of Time Histories & Spectral Functions.
1 Sine Vibration Vibrationdata Unit 2. 2 Vibrationdata Sine Amplitude Metrics.
Unit 41 PSD Special Topics Vibrationdata Band-Splitting
Rainflow Cycle Counting for Random Vibration Fatigue Analysis
Vibrationdata 1 Unit 4 Random Vibration. Vibrationdata 2 Random Vibration Examples n Turbulent airflow passing over an aircraft wing n Oncoming turbulent.
Vibrationdata 1 Non-Gaussian Random Fatigue and Peak Response Unit 36.
Unit 40 Shock Fatigue Vibrationdata
Multi-degree-of-freedom System Shock Response Spectrum
SRS Synthesis Special Topics
NESC Academy 1 Acoustic Fatigue By Tom Irvine Webinar 37.
NESC Academy 1 Unit 27 SRS Synthesis 1. Wavelets 2. Damped Sinusoids.
Circuit Board Fatigue Response to Random Vibration Part 2
Sine-on-Random Vibration
Integration and Differentiation of Time Histories
MODULE 12 RANDOM VIBRATION.
Vibrationdata 1 SDOF Response to Power Spectral Density Base Input Unit 13.
Learning from the Past, Looking to the Future An Alternate Damage Potential Method for Enveloping Nonstationary Random Vibration Tom Irvine Dynamic Concepts,
General Method for Calculating the Vibration Response Spectrum
Dynamic Concepts, Inc. Huntsville, Alabama
Leakage & Hanning Windows
RESPONSE SPECTRUM METHOD
Vibrationdata 1 Unit 5 The Fourier Transform. Vibrationdata 2 Courtesy of Professor Alan M. Nathan, University of Illinois at Urbana-Champaign.
Power Spectral Density Function
Michel Olagnon RAINFLOW COUNTS and composite signals.
Two computations concerning fatigue damage and the Power Spectral Density Frank Sherratt.
Vibrationdata 1 Unit 17 SDOF Response to Applied Force Revision A.
85th Shock and Vibration Symposium 2014
Vibrationdata 1 Unit 15 SDOF Response to Base Input in the Frequency Domain.
Fatigue life estimation from bi-modal and tri-modal PSDs Frank Sherratt.
Vibrationdata 1 Unit 5 The Fourier Transform. Vibrationdata 2 Courtesy of Professor Alan M. Nathan, University of Illinois at Urbana-Champaign.
Vibrationdata 1 Unit 9 White Noise FFT. Vibrationdata 2 Fourier Transform, Sine Function A Fourier transform will give the exact magnitude and frequency.
Unit 14 Synthesizing a Time History to Satisfy a Power Spectral Density using Random Vibration.
Glenn Research Center at Lewis Field Random Vibration Testing of Hardware Tutorial 1 Fatigue Life Assessment William O. Hughes/7735 Mark E. McNelis/7735.
George Henderson GHI Systems, Inc. San Pedro, CA
Vibrationdata 1 Unit 15 SDOF Response to Base Input in the Frequency Domain.
NESC Academy Response to Classical Pulse Excitation Unit 23.
Vibrationdata 1 Unit 6a The Fourier Transform. Vibrationdata 2 Courtesy of Professor Alan M. Nathan, University of Illinois at Urbana-Champaign.
Vibrationdata 1 Unit 32 Circuit Board Fatigue Response to Random Vibration.
1 1 bd Systems, Inc. Advanced Technology Division Waveform Reconstruction via Wavelets October 2005 Revision B bd Systems, Inc. Advanced Technology Division.
Power Spectral Density Functions of Measured Data
Vibrationdata 1 Unit 20 Digital Filtering, Part 2.
Michel Olagnon RAINFLOW COUNTS From fatigue to finance ?
Vibrationdata Synthesizing a Time History to Satisfy a Power Spectral Density using Random Vibration Unit 14 1.
Vibrationdata 1 Power Spectral Density Function PSD Unit 11.
Michel Olagnon RAINFLOW COUNTS and composite signals.
NESC Academy 1 Rainflow Cycle Counting for Continuous Beams By Tom Irvine Unit 34.
Vibrationdata 1 Unit 18 Force Vibration Response Spectrum.
RAINFLOW COUNTS and composite signals Michel Olagnon.
Force Vibration Response Spectrum
Unit 9 White Noise FFT.
Unit 3 Vibrationdata Sine Sweep Vibration.
SDOF Response to Applied Force Revision A
Rectangular & Circular Plate Shock & Vibration
Unit 5 The Fourier Transform.
Integration and Differentiation of Time Histories & Spectral Functions
Unit 44 Vibrationdata Sine Filtering.
FDS, Kurtosion and Reliability Testing
Leakage Error in Fourier Transforms
Equivalent Static Loads for Random Vibration
Unit 2 Vibrationdata Sine Vibration.
Nastran FEA Base Excitation with Multiple Response Spectrum Inputs
FEA PSD Response for Base Excitation using Femap, Nastran & Matlab
Nastran FEA Frequency Response Function for Base Input Revision B
Two-Degree-of-Freedom Systems
Presentation transcript:

Using Fatigue to Compare Sine and Random Environments Unit 35 Using Fatigue to Compare Sine and Random Environments

Comparing Different Environments in Terms of Damage Potential Base Input is Navmat P9492 PSD, 60 sec Duration SDOF Response fn=300 Hz, Q=10 Assume fatigue exponent of 6.4 (Steinberg's value for electronic equipment) What is equivalent sine level in terms of fatigue damage?

NAVMAT P9492 Synthesized Time History Save as: accel_input

Synthesized Time History Histogram

Synthesized Time History PSD Verification

SDOF Response to Synthesis, Narrowband Random Acceleration Response absolute peak = 64.7 G overall = 13.9 GRMS Std dev = 13.9G (for zero mean) Peak response = 4.6 sigma Save as: accel_resp

Statistical Relation  = standard deviation [ RMS ] 2 = [  ] 2 + [ mean ]2 RMS =  assuming zero mean

SDOF Response to Synthesis, Narrowband Random, Histogram

Damage Index for Relative Comparisons between Environments A damage index D can be calculated using where is the response amplitude from the rainflow analysis is the corresponding number of cycles b is the fatigue exponent

Rainflow Cycles for SDOF (fn=300 Hz, Q=10) Response to PSD, Exponent=6

Equivalent Sine Level What is equivalent Sine Input Level at 300 Hz for 60 second duration? Again, SDOF Response fn=300 Hz, Q=10 Assume fatigue exponent of 6.4 Modified Relative Damage Index for Steady-state Sine Response is the response f Excitation Frequency T Duration Y Base Input Acceleration Q Amplification Factor b Fatigue Index

Equivalent Sine Level (cont) f 300 Hz T 60 sec Q 10 b 6.4 D 2.6e+13 Y=2.7 G (Sine Base Input at 300 Hz) (QY) =27 G (Sine Response) Random Response overall = 13.9 GRMS = 13.9 G (1-sigma) for zero mean) Equivalent Sine Response Amplitude  2-sigma Random Response Repeat analysis for other Q and b values as needed. Run additional PSD synthesis cases for statistical rigor.

Equivalent Sine Level (cont) vibrationdata > fatigue toolbox > Miscellaneous > Equivalent Sine Input for Given Damage Level

Histogram Comparison, Base Inputs Random, Normal Distribution Sine, Bathtub Curve Even though histograms differ, we can still do equivalent damage calculation for engineering purposes. This is Engineering not Physics!

Converting a Sine Tone to Narrowband PSD Assume a case where the base input is a sine tone which must be converted to a narrowband PSD The conversion will be made in terms of the acceleration response of the mass to each input Assume Q and fatigue exponent Calculate fatigue damage for sine tone Select frequency limits for narrowband PSD One-twelfth octave band is used for this example Assume initial PSD level of 1 G^2/Hz Calculated SDOF response to narrowband PSD Calculate narrowband damage using Dirlik method Scale PSD level to match sine damage

Converting a Sine Tone to Narrowband PSD vibrationdata > fatigue toolbox > Miscellaneous > Equivalent Narrowband Random PSD for Sine Input

Converting a Sine Tone to Narrowband PSD 18 G, 100 Hz, Sine Tone converted to One-twelfth Octave band PSD Q b PSD (G^2/Hz) 10 4 19.9 6.4 15.0 9 12.0 30 31.7 23.9 19.1 Highest Q and lowest b give most conservative PSD level