Small turbojet engine of the aircraft Reynolds

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.

 

Description

Specifications

 


Description:

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.

 


Specifications:

Features The value
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
Fuel kerosene
Starting fuel kerosene
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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