General Science and Philosophy

   

Life Prediction of Aileron Actuator Using Finite Element Analysis

Authors: Byeong-Sam Kimi, Kyoungwoo Park, Hyeon-Hee Kim

The presented paper describes the application of a modern fatigue prediction tool based on FE-analysis results to highly specific to aerospace industry, fatigue life prediction a problem on a actuator system. The wings are mounted inside the actuator system in order to needs of aileron design and kinematic motion system and structural analysis, to ensure the structural safety analysis results are presented. FE Analysis can provide the estimation of the crack growth curves with sufficient accuracy, even in case of complicated aileron actuator structures which are crucial for preserving aileron integrity and which participate in transfer of load. Probability of crack detection or any other damage detection is a result of many factors.

Comments: 8 Pages.

Download: PDF

Submission history

[v1] 2012-08-19 10:40:54

Unique-IP document downloads: 542 times

Articles available on viXra.org are pre-prints that may not yet have been verified by peer-review and should therefore be treated as preliminary and speculative. Nothing stated should be treated as sound unless confirmed and endorsed by a concensus of independent qualified experts. In particular anything that appears to include financial or legal information or proposed medical treatments should not be taken as such. Vixra.org will not be responsible for any consequences of actions that result from any form of use of any documents on this website.

Add your own feedback and questions here:
You are equally welcome to be positive or negative about any paper but please be polite. If you are being critical you must mention at least one specific error, otherwise your comment will be deleted as unhelpful.

comments powered by Disqus