Publication Date:
2016-06-07
Description:
The hardware and software development of the A-10/TF34 turbine engine monitoring system (TEMS) is described. The operation and interfaces of the A-10/TF34 TEMS hardware are discussed with particular emphasis on function, capabilities, and limitations. The TEMS data types are defined and the various data acquisition modes are explained. Potential data products are also discussed.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA. Lewis Res. Center Aircraft Engine Diagnostics; p 271-283
Format:
application/pdf
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