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RU2614458C1
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Method of diagnosing forms of resonance vibrations of turbomachinery impeller blades
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RU2620764C1
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Device for determination of the turbo machine hollow bodies cross-section parameters at bench testing
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RU2620736C1
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Method of organising working process in turbojet engine with continuously-detonating combustion chamber and device for its implementation
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RU2614460C1
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Air flow control system for cooling turbine of bypass turbojet engine
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RU2614908C1
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Vibration diagnostics method of bearings supports in gas-turbine engines on the rotar frequency peak-to-peak amplitude change
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RU2614453C1
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Cooled high-pressure turbine
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RU2614909C1
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Cooled high-pressure turbine
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RU2612666C1
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Regulated guide vanes of axial compressor of turbine machine
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RU2612668C1
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Air-to-air heat exchanger
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RU2614469C1
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Axis driven centrifugal breather
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RU2613047C1
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Method of vibration diagnostics of bearing supports as part of gas turbine engines using technical microphone
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RU2623672C2
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Gas turbine engine rotary breather
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RU2618993C1
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Dual-flow turbojet engine
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RU2620769C2
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Device for measurement of pipeline parameters
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RU2614904C1
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Turbomachine rotor radial end seal
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RU2618990C2
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Nozzle apparatus of high-pressure turbines
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RU2631850C2
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Turbine engine axial compressor working wheel
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RU2612547C1
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Device to lubricate journal bearing of twin-rotor turbomachine
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RU2614903C1
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Adjustable supersonic nozzle of gas turbine engine
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RU2612546C1
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High-pressure turbine support
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