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![]() ![]() 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
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. Contacts (sales) Contacts (after sales support) |
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