Aero-engine multiple parameter small integral test device

The utility model discloses an aero-engine multiple parameter small integral test device, and aims to realize engine total state malfunction elimination real-time test experiments. The device is composed of a rotation speed signal conditioning module (1), a pressure transmitter (2), an electricity-d...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HAN DI, TIAN JINGUANG, WU YING
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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