Helicopter Component Environmental Vibration Testing - The Poor Man's Fatigue Test -

VFS-F35-048

5/21/1979

Authors
Abstract
Content

Helicopter component environmental vibration testing experience gained during the UTTAS and AAH development programs, various PIP programs, and inventory modernization programs have proven current component vibration qualification test procedures to be deficient in many respects. Specifically, Mil Standard 810 based test procedures lack the realism necessary to develop equipment that is optimized with respect to both weight and function. The 810 based qualification tests do not complement an orderly helicopter component development program. The Systems Development and Qualification Division of AVRADCOM, in conjunction with several manufacturers, has recently developed specific component environmental vibration qualification tests for major pieces of equipment. These tests were derived from the results of preliminary flight testing of these components.

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DOI
https://doi.org/10.4050/VFS-F35-048
Citation
Crews, S., "Helicopter Component Environmental Vibration Testing - The Poor Man's Fatigue Test -," Forum 35 - Washington, D.C. 1979, Washington, D.C., May 21, 1979, https://doi.org/10.4050/VFS-F35-048.
Additional Details
Publisher
Published
5/21/1979
Product Code
VFS-F35-048
Content Type
Technical Paper
Language
English