| 摘要 |
<p>The invention relates to an engine-driven hydraulic pump for an aircraft, comprising a first and a second pump unit (11, 12), each having an adjustable swash plate and a piston assembly coupled thereto driven by a pump shaft (13, 14), with a controller (19) for adjusting the swash plate inclination and a driveshaft (15), by means of which the hydraulic pump may be driven to generate hydraulic pressure at an output line (18) by an engine of the aircraft. According to the invention, the pump units (11, 12) are arranged in parallel and each have a pump shaft (13, 14) coupled by means of a common gearbox (16) to the driveshaft (15).</p> |
