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

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.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1966
Accession Number
AD0637159

Entities

People

  • Albert L. Preston
  • John G. Mcmillan

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Altitude
  • Army Aviation
  • Combustion
  • Combustion Chambers
  • Contracts
  • Detection
  • Detectors
  • Feasibility Studies
  • Flameout
  • Fluidic Amplifiers
  • Gas Turbines
  • Jet Aircraft
  • Sea Level
  • Test And Evaluation
  • Turbines
  • Turbojet Engines

Readers

  • Integrated Circuit Design and Technology.
  • Internal Combustion Engine (ICE) Technology.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems