Brushless DC Motor for Primary Flight Surface Actuator

被引：0

作者：

D'Andrea, M. ^{[1
,2
]}

Di Domenico, G. ^{[3
]}

Macera, D. ^{[4
]}

Di Leonardo, L. ^{[5
]}

Villani, M. ^{[6
,7
]}

机构：

[1] UmbraGroup, Res Ctr Designing Brushless Motors & Electromech, Foligno, PG, Italy

[2] UmbraGroup, Elect Design Unit, Foligno, PG, Italy

[3] UMBRAGRP Spa, R&D Dept, Foligno, PG, Italy

[4] UMBRAGRP, R&D Dept, Albanella Res Ctr, Foligno, PG, Italy

[5] Univ Aquila, Dept Ind & Informat Engn & Econ, Laquila, Italy

[6] Univ Dresden, Dresden, Germany

[7] Nagasaki Univ, Nagasaki, Japan

来源：

2020 INTERNATIONAL CONFERENCE ON ELECTRICAL MACHINES (ICEM), VOL 1 | 2020年

关键词：

More Electric Aircraft; Flight Surfaces; BLDC Motor; Permanent Magnet Motor; Concentrated winding; FE Analysis; Thermal analysis; Lubricant; ELECTRIC AIRCRAFT; DESIGN;

D O I：

10.1109/icem49940.2020.9270696

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This paper presents the design and the verification of a brushless DC motor integrated in an actuator for aircraft application and can be inserted in the field of so called More Electric Aircraft line of though. Main challenge of More Electric Aircraft concepts is the complete substitution of traditional actuator with Electro-Mechanical Actuator, ensuring the same performance and reliability. In this paper, a brushless DC motor for primary flight surface actuator has been designed and analyzed and the comparison on performance of different motor solutions has been presented. Before the sizing of the motor, an accurate selection of the active material has been performed the actuator architecture has been deeply evaluated to identify the best compromise between performance and reliability. After the electromagnetic design, a thermal analysis has been carried out in order to verify the brushless DC motor temperatures during its operation

引用

页码：409 / 414

页数：6

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