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RU2583318C1
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Method of operating aircraft gas turbine engine
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RU2578926C1
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Turbomachine rotor support
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RU2578783C1
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Unit for connection of power cylinder drive of guide vanes with gas turbine engine intermediate housing
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RU2578933C1
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Radial-end seal of turbomachine rotor
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RU2583490C1
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Method of operating gas turbine engine in ground plants
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RU2579373C1
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Radial roller bearing
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RU2578780C1
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Aircraft turbojet engine control method
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RU2583485C1
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Method of controlling aircraft bypass turbojet engine
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RU2578931C1
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Method of controlling operation of aircraft gas turbine engine
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RU2578940C1
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Sectional air-to-air heat exchanger of turbine cooling system
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RU2578762C1
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Centrifugal gear-type oil pump
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RU2578766C1
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Barostatic double acting control valve
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RU2578939C1
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Radial-end seal of turbomachine rotor
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RU2578840C1
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Sliding bearing with nanostructured functional-gradient antifriction coating
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RU2581990C1
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Impeller blade of rotor of compressor of low-pressure gas turbine engine
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RU2581987C1
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Impeller blade of rotor of compressor of low-pressure gas turbine (versions)
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RU2581980C1
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Impeller blade of rotor of compressor of low-pressure gas turbine (versions)
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RU2581981C1
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Impeller blade of rotor of compressor of low-pressure gas turbine (versions)
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RU2578944C1
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Adjustable supersonic nozzle of turbojet engine
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RU2579286C1
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Coupling assembly between compressor rotors and turbine of a gas turbine engine
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