Accession Number : AD0637159

Title :   FEASIBILITY STUDY OF AN IN-FLIGHT FLAMEOUT AND ENGINE-OUT DETECTION SYSTEM

Descriptive Note : Final technical rept.

Corporate Author : HONEYWELL INC MINNEAPOLIS MN AERONAUTICAL DIV

Personal Author(s) : MCMillan, John G ; Preston, Albert L

PDF Url : AD0637159

Report Date : Jun 1966

Pagination or Media Count : 47

Abstract : The document is the final report of a feasibility study to develop a flameout monitor for a gas turbine engine. During the course of the study, it was determined that two different systems, one fluidic and one electronic, should be investigated and tested. Both systems were breadboarded and tested on a J85-7 turbojet engine. Test results described in this document show that both systems meet contract specifications for response time and that each has certain inherent advantages.

Descriptors :   *FLAMEOUT, *FLIGHT INSTRUMENTS, *JET ENGINES, *MONITORS, CIRCUITS, FEASIBILITY STUDIES, FLUID AMPLIFIERS, PROBES, RELIABILITY, TEMPERATURE SENSITIVE ELEMENTS, ULTRAVIOLET EQUIPMENT

Subject Categories : Flight Control and Instrumentation
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE