A Quantitative Method of Tailoring Input Spectra for Random Vibration Screens
Abstract
This report presents a rational method by which an effective random vibration screen may be developed efficiently and quantitatively. In summary, a Flaw Precipitation Threshold (FPT) was derived from measurements of vibration response at known flaw locations. Responses were measured on a variety of modern electronic and electro-mechanical equipment, manufactured by five different manufacturers, during ongoing vibration screens. A vibration screen can be tailored for a piece of equipment by performing a global vibration response survey and adjusting the input spectra so that the responses fall within the FPT.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1987
- Accession Number
- ADA182479
Entities
People
- Allen J. Curtis
- Richard D. Mckain
Organizations
- Hughes Aircraft Company