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Engines for trainer aircraft AL-55/I

AL-55/I

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

[imgx class="block" src="img/editifr/2015/68_0_s1.jpg"]
Design features

• 3-stage low pressure compressor

• 5-stage high pressure compressor

• annular combustor

• 1-stage high pressure turbine

• 1-stage low pressure turbine


Specification

Engine AL-55I
Maximum mode thrust, kgf 1 760
Inlet diameter, m 0.462
Length, m 1.950

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

[imgx class="block" src="img/editifr/2016/68_0_AL-55_Primenenie.jpg"]
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.



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