RU2392599C1
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Ring test device
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RU2391749C1
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Aircraft power unit using fuel cells
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RU2400679C1
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Electric air heater
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RU2395039C1
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Front device of annular combustion chamber of gas-turbine engine
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RU2395795C1
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Generator of high-enthalpy airflow and method of its operation
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RU2395760C1
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Ice tray
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RU2389008C1
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Tune-up method of gas turbine engine with augmentor
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RU2393451C1
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Method of operating aircraft engine based on technical state thereof
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RU2377529C1
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Bench for testing of mechanical properties of materials in gas flow
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RU2382995C1
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Device for measurement of temperature field of gas flow at outlet of combustion chamber
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RU2382910C1
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Compressor impeller
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RU2382911C1
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Fan hollow blade
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RU2386082C1
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Device for preparing air-and-fuel mixture to be supplied to combustion chamber
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RU2387848C1
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Two-stroke turbo diesel air cooling system
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RU2396441C2
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Silencer
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RU2391642C2
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Estimation method of friction in junctions of cylinder-piston and crank-and-rod groups of piston engine, and device for its implementation
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RU2383001C1
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Method of debugging of gas turbine engine with afterburner
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RU2383761C1
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Thermo force post of power unit actuating medium circuit
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RU2381417C1
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Burner and burner operation method (versions)
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RU2374615C1
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Method of diagnosing turbomachine impeller vibration
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