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.

Item Description

– 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

Technical Specifications

* 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.