Sci-tech Gas Turbine Engine Test Set-up Model GFM 85 includes engine that is 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.
The engine is controlled from software, which provides users with a friendly graphical interface for real time monitoring and operation.
The engine can produce maximum Thrust of 80 N & maximum speed 160,000 RPM. The unit is provided with data display and acquisition system with necessary instrumentation. The engine runs on different fuels like Jet A / Jet A1 / Paraffin.
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
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.
Study operation of Axial Flow Gas Turbine.
Determination of fuel consumption.
Air and fuel ratio.
Recording the turbine characteristic.
Determination of the specific thrust.
Determination of the efficiency of the turbine.
Electric Supply 230 V AC, 50 Hz, Single Phase, Earthed.