shock special topics unit 42 vibrationdata 1.accidental drop shock 2.half-sine shock on drop tower...
TRANSCRIPT
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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 via Wavelets
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The Drop Seen Around the World Vibrationdata
First person to buy an iPhone 6 drops It on live TV, Perth, Australia, Sep 18, 2014
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Introduction Vibrationdata
• Drop shock is a very messy, nonlinear problem with potential plastic deformation, cracking, etc.
• Making test measurements is probably more effective than analysis
• The orientation of the item as it strikes the ground is one of several challenges for both measurement and analysis
• But we can do some very simple modeling as a first approximation
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Assumptions Vibrationdata
1. The object can be modeled as a single-degree-of-freedom system subjected to initial velocity
2. The object is dropped from rest
3. There is no energy dissipation
4. The collision is perfectly elastic
5. The object remains attached to the floor via the spring after initial contact
6. The object freely vibrates at its natural frequency after contact
7. The system has a linear response
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SDOF Model Vibrationdata
Dropped from rest at initial height
k
x
m
k
x
m
Attaches to ground upon initial contact
where m is mass, and k is stiffness
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where is the drop height above the ground, and g is gravity acceleration
Next, solve the undamped, free vibration problem with the initial velocity given above. Also, initial displacement is zero.
Some High School Physics Vibrationdata
The initial velocity of the object as it strikes the ground can be found by equating the change in kinetic energy with the change in potential energy:
hmgxm2
1 2
h
hg20x
0xkxm
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Solve Equation of Motion for Peak Responses Vibrationdata
,0xkxm hg20x ,00x
The resulting displacement is
The velocity is
The acceleration is
m/kn
n
hg2)t(x
hg2)t(x
hg2)t(x n
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Miscellaneous > Shock > Accidental Drop Shock
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Peak Response Values Vibrationdata
Natural Freq (Hz)
Displacement (in)
Velocity(in/sec)
Acceleration(G)
200 0.133 167 543
600 0.044 167 1630
1000 0.027 167 2710
Drop height = 36 inches
• 100 in/sec is “severity threshold” per some references• Drop height of 13 inches yields 100 in/sec
• See Webinar 29, Gaberson’s papers, MIL-STD-810E, etc.
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platform
base
Classical pulse shock testing has traditionally been performed on a drop tower
The component is mounted on a platform which is raised to a certain height
The platform is then released and travels downward to the base
The base has pneumatic pistons to control the impact of the platform against the base
In addition, the platform and base both have cushions for the model shown
The pulse type, amplitude, and duration are determined by the initial height, cushions, and the pressure in the pistons
Shock Testing
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Half-Sine Shock Concerns Vibrationdata
Consider total velocity change, net velocity and displacements
Drop Towers can ideally be configured for 0% to 100% rebound
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50 G, 11 msec Half-Sine Pulse Vibrationdata
Assumes zero initial velocity and zero initial displacement
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Miscellaneous > Shock > Half-Sine Shock Text
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50 G, 11 msec, Half-Sine Pulse Vibrationdata
Total velocity change is 135 in/sec in either case (area under the acceleration half-sine curve)
Rebound Peak Velocity (in/sec)
Peak Displacement (in)
0% 135 0.74
100% 67.6 0.24
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Half-Sine Shock on Shaker Table Vibrationdata
Must have:
zero net velocity zero net displacement
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Use Pre and Post-Pulses to Control Velocity and Displacement Vibrationdata
Image from vendor (poor quality but still instructive)
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Read ASCII File: shaker_halfsine.txt
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vibrationdata > Integrate or Differentiate > Double Integrate Acceleration to Displacement
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(48.1 G, -15.2 G)
(76.7 in/sec, -76.7 in/sec)
(0.24 in, -0.66 in)
Max & Min
Goal: 50 G, 11 msec, Half-Sine Shock for Shaker Test
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SRS Comparison Vibrationdata
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SRS Comparison (cont) Vibrationdata
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Shuttle Solid Rocket Booster Splashdown Vibrationdata
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Shuttle Solid Rocket Booster Splashdown Vibrationdata
• IEA boxes were recovered and flown on other missions
• IEA boxes thus needed to withstand multiple splashdown shock events
• Use flight accelerometer data to derive splashdown “time replication” shock test for the IEA electronic box to be performed on shaker table
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Import Shuttle Flight Accelerometer Data Vibrationdata
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Integrate to Velocity & Displacement
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SRB IEA Shock Data Vibrationdata
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Time History > Shock Response Specturm
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Wavelet Modeling Vibrationdata
• There are several approaches to rendering the measured acceleration waveform suitable for a shaker test
• Use wavelet reconstruction for “elegance”
• Previously used wavelet reconstruction for damped sine synthesis in Webinar 27
• The quality of the measured data is a concern due to the:
velocity and displacement drift in the time domaindifferences between positive & negative SRS curves
• So do not expect “exact replication”
• The following method can also be used for correcting or filtering signal by removing saturation effects, etc.
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Time History > Wavelet Reconstruction > Decompose Time History into Wavelet Table
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Acceleration Comparison Vibrationdata
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Acceleration Vibrationdata
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Velocity Vibrationdata
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Displacement Vibrationdata
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Shock Response Spectrum Vibrationdata