Accession Number:

ADB017093

Title:

Turbine Engine Diagnostic Development. Phase I Report

Descriptive Note:

Formal rept.

Corporate Author:

NAVAL AIR PROPULSION TEST CENTER TRENTON NJ PROPULSION TECHNOLOGY AND PROJECT ENGINEERING DEPT

Personal Author(s):

Report Date:

1972-11-01

Pagination or Media Count:

76.0

Abstract:

A turbine engine diagnostic system utilizing a general purpose computer was developed and tested on a TF30-P-408 engine at sea level conditions. Forty-eight parameters, including vibration, oil and performance parameters, were monitored every 80 milliseconds. Forty-seven diagnostic messages were programmed and were displayed on a cathode ray tube. The system has not been fully debugged. Thirty-four diagnostic messages were demonstrated.

Subject Categories:

  • Aircraft
  • Test Facilities, Equipment and Methods
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE