Shock Pulse Meter Analysis.

Abstract

This report contains Shock Pulse data on the tailrotor hanger bearing, the forty-two degree gearbox, and the ninety degree gearbox. Also this report contains a preliminary study of using the shock pulse technique on the OH-58A and on determining the condition of gears in the 42 degree gearbox. The Shock Pulse technique works on the principle that a discrete fault, such as a pit or a spall, will cause repetitive impacts of short duration. These impacts will cause shock waves to propagate through the bearing structure causing a pulse displacement input to an accelerometer, suitably, attached to the bearing structure. The output of the accelerometer passes through a high gain amplifier tuned at the resonant frequency of the accelerometer (this amplifier then acts as a sharp band-pose filter). After the signal is processed the output is displayed on a counter which provides the frequency of peaks above any desired peak amplitudes.

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Document Details

Document Type
Technical Report
Publication Date
Oct 15, 1974
Accession Number
ADA060069

Entities

People

  • Edward F. Covill
  • J. Thomas Harrington
  • John A. George
  • Timothy C. Mayer

Tags

Communities of Interest

  • Air Platforms
  • Biomedical
  • Sensors

DTIC Thesaurus Topics

  • Accelerometers
  • Aircrafts
  • Airframes
  • Airports
  • Ball Bearings
  • Degradation
  • Engineering
  • Frequency
  • Generators
  • Helicopters
  • High Gain
  • International Airports
  • Measurement
  • Resonant Frequency
  • Test And Evaluation
  • Test Fixtures
  • United States

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Electrical Engineering
  • Tribology (the study of the boundary interaction between sliding surfaces, lubrication, wear and friction).