Kinematic Motion System and Structural Analysis of Aileron Actuator Using FEM

被引：0

作者：

Kim, Byeong Sam ^{[1
]}

Park, Kyoungwoo

Park, JungHyun

Jang, KiWon ^{[2
]}

Kim, SangBeom ^{[2
]}

Kim, DaeHyun ^{[2
]}

机构：

[1] Hoseo Univ, Dept Automot Engn, Asan 336795, Cheongnam, South Korea

[2] Hanwha Corp Aerosp R&D Ctr, Asan, South Korea

来源：

MECHANICAL, INDUSTRIAL, AND MANUFACTURING ENGINEERING | 2011年

关键词：

D O I：

暂无

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

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. Using kinematic analysis program Sim Design(motion platform), applied in aileron force acting on the joints. It is feasible to change torque the layout of aileron requirements. A finite element representation of the mechanism as a structure is developed. Using the predicted aerodynamic loads, a structural analysis is performed. These results are beneficial for the next phase of model development of the mechanis

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页码：319 / +

页数：2

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