STAND FOR TESTING TWO-STAGE GAS TURBINE ENGINES

The proposed stand for testing two-stage gas turbine engines contains a drive for the tested engine, a switching unit, a set of measuring instruments, cable connection between the engine parameter transducer and the switching unit and between the switching unit and the measuring instruments, connect...

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Bibliographische Detailangaben
Hauptverfasser:	SMYRNOV STANISLAV IVANOVYCH, SPITSYN VOLODYMYR YEVHENIIOVYCH, MYKHAILOV OLEKSANDR BORYSOVYCH, ZHYRYTSKYI OLEKSANDR OLEHOVYCH, ZHYRYTSKYI OLEH HEORHIIOVYCH, KONTSEVYCH HEORHII YURIIOVYCH, MOLCHANOV IVAN SEMENOVYCH, FILONENKO OLEKSANDR OLEKSIIOVYCH, ISAKOV BORYS VOLODYMYROVYCH, MAIOROVYCH BORYS DAVYDOVYCH
Format:	Patent
Sprache:	eng
Schlagworte:	MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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Beschreibung
Zusammenfassung:	The proposed stand for testing two-stage gas turbine engines contains a drive for the tested engine, a switching unit, a set of measuring instruments, cable connection between the engine parameter transducer and the switching unit and between the switching unit and the measuring instruments, connectors, an adapter with thermal insulation, and a water cooler. The cable connections are installed in the conduit that id installed in the adapter. Air from the compressor of the engine passes through the adapter and the water cooler. The proposed stand is distinctive by its reliability and accuracy in measuring parameters of gas turbine engines.