Gas-turbine technologies for transport, defense and energy industries
 Home / Products / 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

X close
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

X close
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.



Contact us
Contacts (products and services)
More information request




АО «Объединенная двигателестроительная корпорация» (ОДК)

Страница в сети Интернет, предоставляемая распространителем информации на рынке ценных бумаг


VKontakte RSS news RSS press Russian Engineering Union Sitemap

© PJSC «UEC-Saturn» 2006-2022