The Engine Pressure Ratio (EPR) system provides an indication of the inlet to exhaust pressure ratio and is used as the primary thrust setting indicator. The Turbine Gas Temperature (TGT) indicating system displays the temperature of the exhaust gases entering the LP 1 nozzle guide vanes. Three %RPM indicating systems are provided one for each engine rotating spool.
This blog documents a project to build a functional Lockheed L-1011 cockpit replica using real flight hardware, NI labVIEW and the x-Plane software platform.
Wednesday, June 6, 2012
L-1011 Engine: EPR Indicating System
The Engine Pressure Ratio (EPR) system provides an indication of the inlet to exhaust pressure ratio and is used as the primary thrust setting indicator. The Turbine Gas Temperature (TGT) indicating system displays the temperature of the exhaust gases entering the LP 1 nozzle guide vanes. Three %RPM indicating systems are provided one for each engine rotating spool.
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