Aeroengine Condition Monitoring System Based on Non-Interference Discrete-Phase Compressor Blade Vibration Measuring Method

Abstract

Described method is of great importance for flight safety and may be recommended as a completion of the existing systems of diagnostic of turbine engines. 2. By using the discrete non-contact method of measuring blades vibration and numerical analysis of blade vibration spectrum it is possible to conduct complex, monitoring of technical state of major engine components like: - compressor blades - fuel system - bearing system.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2001
Accession Number
ADP011156

Entities

People

  • Ryszard Szczepanik

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Amplitude
  • Compressor Blades
  • Compressors
  • Cracks
  • Data Analysis
  • Engines
  • Frequency
  • Fuel Consumption
  • Fuel Systems
  • Identification
  • Jet Engines
  • Military Aircraft
  • Numerical Analysis
  • Turbines
  • Vehicles

Readers

  • Aerospace Engineering
  • Computational Fluid Dynamics (CFD)
  • Mathematical Modeling and Probability Theory.