Electronic assembly structural analysis
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Transcript of Electronic assembly structural analysis
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Structural Analysis
Solidworks FEA Simulation Advanced Dynamics
Date: Jan 14, 2015
D. Blanchet
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Reference image Typical electronics Assembly
Lockheed Martin CEEU
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• Total Assembly weight = 152 lbs
• Material 6061-T4 Dip Brazed Aluminum
– Yield strength = 21,000 psi
– Ultimate strength = 35,000 psi
• Load Cases
– Random Vibration
– Shock
– Inertial Acceleration
• Nominal part dimensions are used in the analysis
Assumptions – custom assembly concept
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Simplified SW model Electronics Assembly
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Solidworks FEA meshed model (900,000 D.O.F.)
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Solidworks meshed model covers removed
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Backplane
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Solidworks FEA Detailed fine mesh
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High Stress Zone At Mounting Foot
Braze Joint
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Random Vibration test level D 8.92 Grms
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Applied individually to 3 axes.
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Random Vibration Results – stress side to side
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3 sigma Von Mises
Stress = 4,500 psi
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Random Vibration Results – displacement side to side
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3 sigma Displacement
.012 inches
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Random Vibration Results - Summary
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Direction input PSD
3 sigma Displacement
3 sigma Stress
psi
Factor Of
Safety*
Side-to-side 8.92 Grms .012 (plenum)
4,500 (foot)
4.6
Up - down 8.92 Grms
.014 (plenum)
6,000 (foot)
3.6
Front-to-back 8.92 Grms
.012 (IO cage cover)
3,900 (foot)
5.4
* Factor of safety based on a Yield Strength of 21,000 psi
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Shock input, 6 directions
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Shock response max stress @ mounting foot downward direction
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Conclusion: Stresses from Shock pulses
Are insignificant
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Shock Response max displacement downward shock
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Max displacement .002 inches
Plot magnification = 240,000 X
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Results: Acceleration / Simultaneous Inertial Loads G’s (m/sec sq)
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Load Case
Forward Up
Down Side Max Stress
Mounting Feet (psi)
Material Strength
(psi)
Factor of
Safety
Limit Load
2.0 (19.6)
3.07 (30.1)
- 1.7 (16.7)
2,500 21,000 8.4
Ultimate Load
3.0 (29.4)
4.6 (45.1)
- 2.5 (24.5)
3,250 35,000 10.8
Limit Load
2.0 (19.6)
- 6.0 (58.8)
1.7 (16.7)
4,500 21,000 4.7
Ultimate Load
3.0 (29.4)
- 9.0 (88.2)
2.5 (24.5)
7,800 35,000 4.5
side
up
forward
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Results: Acceleration / Simultaneous Inertial Loads G’s (m/sec sq)
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Load Case
Forward Up
Down Side Max Stress
Fiber Bracket
(psi)
Material Strength
(psi)
Factor of
Safety
Limit Load
2.0 (19.6)
3.07 (30.1)
- 1.7 (16.7)
250 11,000 44
Ultimate Load
3.0 (29.4)
4.6 (45.1)
- 2.5 (24.5)
350 27,000 77
Limit Load
2.0 (19.6)
- 6.0 (58.8)
1.7 (16.7)
450 11,000 24
Ultimate Load
3.0 (29.4)
- 9.0 (88.2)
2.5 (24.5)
675 27,000 40
side
up
forward Max displacement = .002 inches
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Results: mounting bolt analysis 8 places
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• The electronics assembly design concept is structurally adequate for the specified environments.
• The maximum stresses and displacements occur during combined acceleration.
• The stresses are below the yield point of 6061-T4 for all load cases.
• Shock Load stresses are Insignificant.
• The assembly main mounting bolts need to have a yield strength >= 100,000 psi
Conclusions
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