Accession Number:

ADA359658

Title:

Engine Health Monitoring System for Advanced Diagnostic Monitoring for Gas Turbine Engines

Descriptive Note:

Final rept. 13 Nov 95-20 Feb 98

Corporate Author:

STRESS TECHNOLOGY INC ROCHESTER NY

Personal Author(s):

Report Date:

1998-02-01

Pagination or Media Count:

91.0

Abstract:

A prototype USAF engine health management EHM system was developed and ground tested during this Phase II SBIR program. The EHM system is capable of real-time mechanical monitoring and diagnostics, aero-thermal performance monitoring and diagnostics, and engine signature based life accumulation. For the first time, state-of-the-art anomaly detection, monitoring, diagnosis and advanced life prediction analysis were integrated together in a single real-time engine health monitoring system. Additionally, the EHM system was developed to assist the 2-level maintenance concept and IHPTET initiatives.

Subject Categories:

  • Aircraft
  • Jet and Gas Turbine Engines
  • Computer Programming and Software

Distribution Statement:

APPROVED FOR PUBLIC RELEASE