DESIGN AND CALCULATION OF HYDRAULIC POWER SMALL PASSENGER AICRAFT TO TAKE-OFF WEIGHT 2000 kg

Abstract

Aircraft hydraulic power system is used to control the movement of aircraft on the ground but in the air. Hydraulic system of the each aircraft consists of one or two main lines of constant pressure which are connected to individual work areas. Task provides a comprehensive insight into the design and functionality of the principle of individual work streams. Work is an introduction clarify the issue of hydraulic systems, describe the basic concepts, cutting hydraulic systems and their advantages and disadvantages. The core of this work is the proposal itself and a description of the circuit constant pressure, work streams chassis control, flaps and wipers glasses.