Study to Determine the Application of Aircraft Ignition-Source Control Systems to Future Army Aircraft

Abstract

The report presents the results of a program that was conducted to provide design information applicable to future Army aircraft relative to crash sensors, ignition-source suppression systems, and circuitry for the automatic activation of the suppression systems. The program involved a comprehensive literature search, the development of requirements for the initiating subsystem of the overall ignition source control system, and the consideration and comparison of several illustrative activating circuits. The development of a workable ignition-source suppression system was found to be feasible. Several systems have already been developed to cool hot surfaces, to inert atmospheres, and to de-energize electrical systems. The areas of the ignition-source control problem which require development are: the selection and the degree of redundancy of crash sensors, the locations of the sensors on the aircraft, and the complexity of the activating and control circuitry.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1971
Accession Number
AD0729870

Entities

People

  • John K. Drummond

Tags

Communities of Interest

  • Air Platforms
  • Sensors

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Army Aircraft
  • Combustion
  • Control Systems
  • Electrical Circuits
  • Electrical Equipment
  • Fixed Wing Aircraft
  • Helicopters
  • Ignition Lag
  • Jet Aircraft
  • Military Aircraft
  • Rotary Wing Aircraft
  • Safety Engineering
  • Turbojet Engines

Fields of Study

  • Engineering

Readers

  • Applied Combinatorial Optimization and Logic Circuit Design.
  • Joint Military Operations and Doctrine.
  • Life Cycle Cost Analysis