An endurance test of the AR318 single shaft turboprop engine has been carried out in order to verify the integrity of the engine and the degradation of performance for a more severe take-off rating with an increased Turbine Entry Temperature (T.E.T.). The paper deals with the activities performed and with the numerical computer codes developed and set up for processing the experimental data obtained by hangar test bed. Results of calculations for controlling the reliability of data, for engine simulation, for performance monitoring and for diagnostic are shown.
Endurance ground testing of the AR318 turboprop engine
Dauerfestigkeitspruefung des Turbopropmotors AR318
AIAA-Papers ; Jul ; 1-10
1988
10 Seiten, 22 Bilder, 11 Quellen
Conference paper
English
Endurance ground testing of the AR318 turboprop engine
AIAA | 1988
|SAE Technical Papers | 1955
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