Civil aircraft airborne hydraulic accessory comprehensive test system

The utility model discloses a civil aircraft airborne hydraulic accessory comprehensive test system, which comprises a hydraulic pump station and a console, and the hydraulic pump station is connected with the console through a hose. The hydraulic pump station comprises an oil tank, an oil outlet of...

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Bibliographische Detailangaben
Hauptverfasser:	WANG XINKAI, LIU WEI, NI SHUQIAO, HU WAN, ZHANG ZHENGMAO, TIAN YE, QIAO DAN, GUAN HUA, XIE LIANGCONG
Format:	Patent
Sprache:	chi ; 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 utility model discloses a civil aircraft airborne hydraulic accessory comprehensive test system, which comprises a hydraulic pump station and a console, and the hydraulic pump station is connected with the console through a hose. The hydraulic pump station comprises an oil tank, an oil outlet of the oil tank is connected with a motor pump assembly through a guide pipe, the motor pump assembly is connected with a high-pressure hose through a guide pipe, and an oil return opening of the oil tank is connected with a low-pressure hose through a guide pipe. According to the civil aircraft airborne hydraulic accessory comprehensive test system, the output pressure can be adjusted through the first output pressure adjusting valve and the second output pressure adjusting valve, the oil outlet pressure of the first oil outlet pipe and the oil outlet pressure of the second oil outlet pipe are dynamically adjusted, and the dynamic performance side view of a tested product is achieved; meanwhile, a first bypass valve