Bendix Flameout Sensor for Turbine Engine Aircraft

Format:

Conference/Event

Author/Creator:

Welch, H. C., author.

Conference Name:

SAE World Congress & Exhibition (1964-01-01 : Detroit, Michigan, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1964

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

640389

Access Restriction:

Restricted for use by site license