Accession Number : AD0776338
Title : Turbine Engine Diagnostic Development.
Descriptive Note : Rept. on Phase 2,
Corporate Author : NAVAL AIR PROPULSION TEST CENTER TRENTON N J PROPULSION TECHNOLOGY AND PROJECT ENGINEERING DEPT
Personal Author(s) : VanGelder,F. M.
Report Date : MAR 1974
Pagination or Media Count : 113
Abstract : Turbine engine diagnostic development was continued, and included testing on a TF30-P-408 turbofan engine at sea level static and ram conditions. The Phase I computer program was restructured, using new mode recognition logic and adding thermodynamic performance analysis. New hardware tested included a radiation pyrometer, internal accelerometer, charged particle probe, and a programmable cathode ray tube display. Fifty parameters were monitored and a total of 90 diagnostic messages were programmed and demonstrated. (Author)
Descriptors : *Turbofan engines, *Turbines, *Propulsion systems, Gas flow, Diagnosis(General), Computer programming, Cathode ray tubes, Display systems, Performance(Engineering)
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE