About this document
Hydraulic Test Rig Design for Aircraft by Ahmed Eldessouky is a document available to read on EtoBox.
This document describes the design of a universal test rig for testing hydraulic elements used in aircraft. The test rig allows pre-installation checks of line replacement units that transfer hydraulic pressure and fluid from pumps to actuators for flight control systems and other aircraft functions. It consists of a hydraulic power unit, electrical power supply, and three test stands to mount and test hydraulic valves, electrically operated valves, and landing gear components. The test rig is designed to t
- Author
- Ahmed Eldessouky
- Language
- EN