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Aircraft Engine Control Unit (FADEC) Design Assessment for Extreme Vibration and Shock Loads

Author(s):

Preethi J , Dr. Ambedkar Institute of Technology, Bangalore; Dr. B. M Nandeeshaiah, Dr. Ambedkar Institute of Technology, Bangalore

Keywords:

Extreme Vibration & Shock Loads, FADEC

Abstract

Full Authority Digital Engine Control (FADEC) system consisting of an electronic engine controller and its related parts to control all aspects of aircraft engine. The main purpose of this analysis is to design engine control system for commercial aircraft jet engine and focuses on modeling of FADEC system, static and dynamic response of system under different loading condition. The objective of this analysis is to optimize design of FADEC and to allow the engine to perform at maximum efficiency for a given flight condition.

Other Details

Paper ID: IJSRDV4I60343
Published in: Volume : 4, Issue : 6
Publication Date: 01/09/2016
Page(s): 803-806

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