Design and Analysis of Hydraulic Actuator in a Typical Aerospace vehicle
Author(s):
G.Karthik , Indur Institute of Engineering & Technology; R.Venkatesh, Indur Institute of Engineering & Technology; V.Upender, Indur Institute of Engineering & Technology; Neeraj Kumar, Indur Institute of Engineering & TechnologyKeywords:
Piston, Eyeend, Solid Works, Finite Element MeshingAbstract:
An Aerospace Vehicle is capable of flight both within and outside the sensible atmosphere. An Actuation System is one of the most important Systems of an Aerospace vehicle. This paper study involves detailed study of various controls Actuation System and Design of a typical Hydraulic Actuation Systems. An actuator control system concerned with electrical, electronic or electro mechanical. Actuator control systems may take the form of extremely simple, manually-operated start-and-stop stations, or sophisticated, programmable computer systems. Hydraulic Actuation System contains Electro Hydraulic Actuators, Servo Valves, Feedback Sensing elements, Pump Motor package, Hydraulic Reservoir, Accumulator, various safety valves, Filters etc. The main objective of this study involves design of Hydraulic Actuator and selection of various other components for the Actuation Systems of an Aerospace Vehicle. Design of the system includes design of Hydraulic actuator and also the Modeling and Analysis of actuator using sophisticated Software.
Other Details:
| Manuscript Id | : | J4RV4I2003 |
| Published in | : | Volume : 4, Issue : 2 |
| Publication Date | : | 01/05/2018 |
| Page(s) | : | 7-16 |
