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Turbojet Trainer With Reheat

Turbojet Trainer With Reheat

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Product Description

TURBOJET TRAINER WITH REHEAT  

A self-contained, fully instrumented, educational single shaft gas turbine. Powered by kerosene, the experimental abilities of this high-quality apparatus enable comprehensive practical investigations into the principles, and performance of single-shaft gas turbines. Air passes into an air box, into a compressor, then into the combustion chamber. A pump transfers fuel from the fuel tank to spray through a special nozzle into the combustion chamber. A high-energy spark ignites the air and fuel mixture that flows to radial now turbine, then a variable area propelling nozzle. The exhaust gases then discharge to a suitable exhaust system. The combustion chamber gives excellent combustion, low pressure loss and good flame stability over a wide range of conditions. A fuel flow control valve on the instrumentation and control panel regulates the speed. 

  • Effect on thrust generation by variation in rotational speed and propelling nozzle area 
  • Isentropic, polytropic and mechanical efficiencies of compressor, combustion chamber and turbine 
  • Pressure ratios of turbine. compressor and non-dimensional characteristics 
  • Combustion chamber pressure losses and combustion efficiencies 
  • Specific fuel consumption. thermal efficiency, air standard cycle, work ratio and heat balance
  • Programming software included PC be included and all necessary accessories for operation 

 


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