
AL-55/Э Dual-Circuit Turbojet Engine for Enhanced Training Aircraft Performance
Manufacturer:PJSC "ODK-SATURN"
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FOB, CIF & EXW terms available
Description
AL-55 is a twin-circuit turbojet engine designed for a new generation of training aircraft.
Design Features:
- 3-stage low-pressure compressor
- 5-stage high-pressure compressor
- annular combustion chamber
- 1-stage high-pressure turbine
- 1-stage low-pressure turbine
Benefits:
- the engine can be used on single-engine aircraft
- modular engine design ensures high operational manufacturability and low operating costs
- modern digital engine control system with hydromechanical redundancy provides piloting safety and ease of maintenance
- starter-generator provides engine start-up and power supply to aircraft systems
- unified gas generator AL-55 allows to create modifications equipped with a nozzle with controlled thrust vector and afterburner
Design Features:
- 3-stage low-pressure compressor
- 5-stage high-pressure compressor
- annular combustion chamber
- 1-stage high-pressure turbine
- 1-stage low-pressure turbine
Benefits:
- the engine can be used on single-engine aircraft
- modular engine design ensures high operational manufacturability and low operating costs
- modern digital engine control system with hydromechanical redundancy provides piloting safety and ease of maintenance
- starter-generator provides engine start-up and power supply to aircraft systems
- unified gas generator AL-55 allows to create modifications equipped with a nozzle with controlled thrust vector and afterburner
Specifications
Length, m
1.95 m
Diameter at motor inlet, m
0.462 m
Thrust at maximum mode, kgf
1760
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