ONBOARD MONITORING SYSTEM OF AIRCRAFT ENGINE AT LIMITED TEMPERATURE, PRESSURE AND THRUST

FIELD: aircraft instrumentation engineering; monitoring of gas-turbine engines. ^ SUBSTANCE: proposed monitoring system makes it possible to check aircraft engine working in standard, off-standard and augmented power rating modes. Monitoring is based on use of information received from sensors of ai...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: STEPANJAN N.M, FURMAKOV E.F, MASLOV JU.V, PETROV O.F
Format: Patent
Sprache:eng ; rus
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