General Engine specification Blog1.
It is a turboprop engine- free turbine .
This is an engine used in airplanes like
Compressor
It consist of 3 stage axial compressor and 1 stage centrifugal flow compressor.
Combustion
Annular reverse flow (right to left according to diagram above) combustion with 14 simplex burner (Glow plugs)
Turbine
1 stage free power turbine and 1 sage gas generator power turbine.(Left to right according to diagram above)
Other specs:
It is a turboprop engine- free turbine .
This is an engine used in airplanes like
- DHC-6 Twin Otter 300
- Harbin Y-12
- Beechcraft
Compressor
It consist of 3 stage axial compressor and 1 stage centrifugal flow compressor.
Combustion
Annular reverse flow (right to left according to diagram above) combustion with 14 simplex burner (Glow plugs)
Turbine
1 stage free power turbine and 1 sage gas generator power turbine.(Left to right according to diagram above)
Other specs:
- Fuel type: aviation kerosine
- Overall pressure ratio- 6.3:1
- Air mass flow: 5.3 lb/s
- Power to weight ration: 2.14 hp/lb
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