To provide desired engine restart capability and limit ignition operating time to a minimum, it was considered desirable to develop a flameout sensor. The compressor discharge pressure (CDP) was used as the most desirable sensing parameter to obtain positive indication of flameout.Diagrams of the sensor and a brief description of its operation are given in this paper. Flight testing of the flameout sensor has proved its reliability.
Bendix Flameout Sensor for Turbine Engine Aircraft
Sae Technical Papers
SAE World Congress & Exhibition ; 1964
1964-01-01
Conference paper
English
Bendix flameout sensor for turbine engine aircraft
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