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0 - 100kN turbofan AL-55/I
for light aircraft

0 - 100kN turbofan
0 - 100kN turbofan
0 - 100kN turbofan
0 - 100kN turbofan
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Characteristics

Thrust
0 - 100kN
Applications
for light aircraft

Description

The AL-55/I - turbofan engine, designed for new generation trainer aircraft. Responsibility • UEC-Saturn: core, final assembly, power plant integration, ground and flight tests; leading contractor of engine development; associate contractor of licensed production • UEC-UMPO (UEC): low pressure spool; associate contractor of engine development; leading contractor of licensed production Design features • 3-stage low pressure compressor • 5-stage high pressure compressor • annular combustor • 1-stage high pressure turbine • 1-stage low pressure turbine Advantages • possibility of engine use for single-engine aircraft • engine modular design provides high maintainability and low operating cost • up-to-date digital engine control system with backing up hydromechanical channel provides flight safety and high diagnostic capability • integrated starter-generator provides engine start and electric power supply for aircraft systems • single AL-55 HP Core enables development of engine family for various applications, incl. afterburning and thrust vectoring modifications Application The family of engines based on the AL-55 HP core destined for basic and advanced trainer and other types of aircraft. On the base of AL-55 HP Core, UEC-Saturn has created the АL-55I engine for basic trainer aircraft developed by foreign Customer.
*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.