Gas turbine transients with controlled variable geometry
JR Barbosa, C Bringhenti… - … Expo: Power for …, 2012 - asmedigitalcollection.asme.org
A small 5-kN thrust gas turbine, designed and manufactured having in mind a thorough
source of validation data, serves as basis for the study. The engine is an uncooled turbine, 5:
1 pressure ratio axial flow compressor, delivering 8.1 kg/s air mass flow, whose control is
made by a FADEC. Cold runs of the jet engine version have already been completed. The
engine characteristics are being developed using the technology indicated in the paper.
Accelerations and decelerations from idle to full power in a prescribed time interval and …
source of validation data, serves as basis for the study. The engine is an uncooled turbine, 5:
1 pressure ratio axial flow compressor, delivering 8.1 kg/s air mass flow, whose control is
made by a FADEC. Cold runs of the jet engine version have already been completed. The
engine characteristics are being developed using the technology indicated in the paper.
Accelerations and decelerations from idle to full power in a prescribed time interval and …
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