Small turbojet engine for Reynolds unmanned aircraft ultralight class.
Small turbojet engine Reynolds R 500 is designed for UAVs with a takeoff weight of 200 to 500 kilograms. Is more effective in comparison with analogues.
Small turbojet engine Reynolds R 500 is designed for UAVs with a takeoff weight of 200 to 500 kilograms. These machines belong to the ultralight class.
Turbojet engine Reynolds R 500 has a fairly large overhaul period is 300 hours, which is 5-6 times greater than TBO analogues, and also high efficiency – the specific consumption of fuel is 1.2 kilograms per kilogram-force per hour. Turbojet engine Reynolds more economical than their counterparts by 20-40 %. Brushless starter-generator of the engine is located on the same shaft with the engine.
Turbojet engine Reynolds R 500 is available for outdoor placement, internal placement, and also has a shortened version.
|Length of engine for external placement, internal placement, short of execution, see||490, 464, 339|
|The diameter of the engine, see||197|
|Thrust of engine, N||500|
|The weight of the engine with the harness, kg||7,5|
|Overhaul life, h||300|
|Capacity starter-generator, W||400|
|The shaft rotation frequency, Rev/min||75000|
|The air flow through the engine, kg/s||1|
|The pressure ratio in the compressor||4,5|
|The gas temperature before the turbine, To||1150|
|Specific consumption of fuel for maximum thrust, kg/kgf/h||1,2395|
Note: the description of technology in example of the turbojet engine Reynolds R 500.
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