Optimal preliminary design of electromechanical actuators

被引：29

作者：

Budinger, Marc ^{[1
]}

Reysset, Aurelien ^{[1
]}

El Halabi, Toufic ^{[1
]}

Vasiliu, Catalin ^{[2
]}

Mare, Jean-Charles ^{[1
]}

机构：

[1] Univ Toulouse, Inst Clement Ader, INSA UPS, F-31077 Toulouse, France

[2] Univ Politehn Bucuresti, Bucharest 060032, Romania

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2014年 / 228卷 / 09期

关键词：

Design exploration; electromechanical actuator; flight control; inverse problem; inverse simulation; Modelica; meta-models; response surface methodology; scaling laws; spoiler;

D O I：

10.1177/0954410013497171

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents a methodology for the optimal preliminary design of electro-mechanical actuators. The main design drivers, design parameters and degrees of freedom that can be used for preliminary design and optimization of electro mechanical actuator are described. The different types of models used for model-based design (estimation, simulation, evaluation and meta-model), and their associations are presented. The process preferred for its effectiveness in terms of flexibility, and computational time is then described and illustrated with the example of a spoiler electromechanical actuator. The proposed approach, based on meta-models obtained using the surfaces response methods and scaling laws models, is used to explore the influence of anchorage points and transmission ratio on the different design constraints and the overall mass of the actuator.

引用

页码：1598 / 1616

页数：19

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