Tesca Jet Engine Gas Turbine 32465 test set up included engine 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 167 N & maximum speed 1,20,000 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.

Specifications

• Gas Turbine:
• Axial Flow Gas Turbine
• Max. Thrust 167 N,
• Max. 1,20,000 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.

Experiments

• 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