RU2741685C1
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Gas turbine engine compressor rotor impeller
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RU2742321C1
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Method of operating aircraft gas turbine engine based on technical state thereof
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RU2741824C1
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Hydrodynamic damper of bearing support of turbomachine rotor
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RU2745820C1
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Diagnostic method for technical state of gas turbine engine
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RU2746365C1
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Method for reducing vibratory stresses in working blades of turbomachine
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RU2746294C1
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Two-engined aircraft power plant and power plant control method
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RU2742320C1
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Adjustable turbojet engine nozzle
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RU2742849C1
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Front support of low-pressure turbine rotor of two-shaft gas turbine engine
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RU2742848C1
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Aircraft gas turbine engine test system in ground conditions
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RU2741686C1
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Engine operation method as per technical state thereof
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RU2741995C1
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Gas turbine plant
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RU2746757C1
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Stand for testing fuel collectors
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RU2746378C1
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Test method for aircraft gas turbine engine
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RU2739463C1
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Method of preparing adhesive composition before deposition on working surface
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RU2741747C1
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Flame detection ionisation sensor
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RU2730630C1
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Device for connection of internal and external housings of turbomachine
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RU2732531C1
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Cooled blade of gas turbine
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RU2730581C1
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Method of controlling supply of fuel to gas turbine engine and system for its implementation
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RU2730380C1
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Device for fixing elements of turbomachines during fatigue tests on vibration test bench
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RU2726317C1
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Gas turbine installation remote monitoring system
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