Aviation hydraulic test system

The invention provides an aviation hydraulic test system. The aviation hydraulic test system comprises an interface panel unit, a returned oil test unit, a dynamic pressure component unit, a static pressure test unit and a pump station unit. The interface panel unit is connected with the returned oi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	MENG WENHUI, LIU JUELING, HE DAN, CHEN HUAIYU, SHEN BINGLONG, WANG JIANMIN
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR FLUID-PRESSURE ACTUATORS FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS HEATING HYDRAULICS OR PNEUMATICS IN GENERAL LIGHTING MECHANICAL ENGINEERING SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	The invention provides an aviation hydraulic test system. The aviation hydraulic test system comprises an interface panel unit, a returned oil test unit, a dynamic pressure component unit, a static pressure test unit and a pump station unit. The interface panel unit is connected with the returned oil test unit, the dynamic pressure component unit and the static pressure test unit through pipelines and used for providing hydraulic test input, output and adjustment; the pump station unit is connected with the returned oil test unit, the dynamic pressure component unit and the static pressure test unit through pipelines and used for providing continuous fuel oil. The aviation hydraulic test system can reduce the labor cost to the greatest extent, high in accuracy and suitable for testing at various sites, moves conveniently and can measure various kinds of hydraulic pressure including static pressure, dynamic pressure and returned oil. The aviation hydraulic test system is convenient to use and easy to operate.