Gas Turbine Engine Test Set Up Model TH 119

Sci-tech Gas Turbine Engine Test Set Up Model TH 119 includes engine as the compact turbine engine, comprising a single stage radial compressor, combustion chamber and an axial flow turbine. The engine has been mounted into a sturdy metal frame that holds it firmly. A tough, transparent polycarbonate screen is fitted for safety while the engine is running. Engine Thrust, Temperatures & Air flow rate are measured by high accuracy sensors.

SKU: 6b6ca470c5e2 Categories: ,

– Electronically controlled Axial Flow Gas Turbine, complete with Instruments.
– All safety instruments included.
– Complete aeronautical axial flow gas turbine engine
– Full instrumentation and sensors
– Full control by means of software and microprocessor controller
– Simple Electrical ignition system
– Data acquisition and educational software included
– Very small scale equipment minimises laboratory space needed
– An floor standing stand to house the unit together with its fuel tank and electronic console

* Gas Turbine: - Axial Flow Gas Turbine - Max. Thrust 80 N, - Max. 1,60,000 RPM, - Idle RPM. 50,000 RPM - Single stage radial compressor. - Exhaust Gas Temperature: @ 600 ˚C - Fuel: Jet A or Jet A1 or low sulphur paraffin - Oil: 5% Mobil JetOil, Aeroshell 500/550 and Exxon 2380 * Full instrumentation to measure RPM, Thrust and Temperature and Pressure at each stage of the jet engine * Data Acquisition Device: 16 channel Data Acquisition Device, 16 Bit, 250 kS/s, USB Based, Make National Instruments * LabVIEW based Data Acquisition Software for performance analysis. * A mounting frame for floor standing operation.