Hydraulic fluid oscillation reduction mechanism for use in hydraulic system of airplane, has actuator arranged in hydraulic line of hydraulic system for producing pressure pulses intended to compensate pressure pulses of pump

摘要

The mechanism has an actuator (5) arranged in the hydraulic line (3) of a hydraulic system for producing pressure pulses intended to compensate the pressure pulses of the pump (2) of the hydraulic system. The pump is driven by a motor (1) to promote fluid under pressure through the hydraulic line.