DIAGNOSTICS OF RD-33 ENGINES
Abstract
The article is dealing with the diagnostics of the RD-33 aviation turbojet engine. The focus is on the description of actual state of diagnostics of the engine by the SDK-88 system and in the description of the detection of failures, such as intake of foreign objects, presence of impurities inoil and engine vibration during operation.
Keywords
diagnostics of the turbojet engine; impurities in oil; engine vibrations
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