NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Demonstrating the Effect of Particle Impact Dampers on the Random Vibration Response and Fatigue Life of Printed Wiring AssembliesIn a recent experimental study, small Particle Impact Dampers (PID) were bonded directly to the surface of printed circuit board (PCB) or printed wiring assemblies (PWA), reducing the random vibration response and increasing the fatigue life. This study provides data verifying practicality of this approach. The measured peak strain and acceleration response of the fundamental out of plane bending mode was significantly attenuated by adding a PID device. Attenuation of this mode is most relevant to the fatigue life of a PWA because the local relative displacements between the board and the supported components, which ultimately cause fatigue failures of the electrical leads of the board-mounted components are dominated by this mode. Applying PID damping at the board-level of assembly provides mitigation with a very small mass impact, especially as compared to isolation at an avionics box or shelf level of assembly. When compared with other mitigation techniques at the PWA level (board thickness, stiffeners, constrained layer damping), a compact PID device has the additional advantage of not needing to be an integral part of the design. A PID can simply be bonded to heritage or commercial off the shelf (COTS) hardware to facilitate its use in environments beyond which it was originally qualified. Finite element analysis and test results show that the beneficial effect is not localized and that the attenuation is not due to the simple addition of mass. No significant, detrimental reduction in frequency was observed. Side-by-side life testing of damped and un-damped boards at two different thicknesses (0.070" and 0.090") has shown that the addition of a PID was much more significant to the fatigue life than increasing the thickness. High speed video, accelerometer, and strain measurements have been collected to correlate with analytical results.
Document ID
20130013858
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Knight, Brent
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Montgomery, Randall
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Geist, David
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hunt, Ron
(Bevilacqua Research Corp. Huntsville, AL, United States)
LaVerde, Bruce
(Engineering Research Consultants, Inc. Huntsville, AL, United States)
Towner, Robert
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Date Acquired
August 27, 2013
Publication Date
April 8, 2013
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
M12-2110
Report Number: M12-2110
Meeting Information
Meeting: AIAA Aerospace Design and Structures Event
Location: Boston, MA
Country: United States
Start Date: April 8, 2013
End Date: April 11, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available