Development of an active wing for flight machines using macro fiber composites

被引：0

作者：

Ha, Kil seong ^{[1
]}

Huang, Ya-Wen ^{[1
]}

Nagata, Yoshinori ^{[1
]}

Ming, Aiguo ^{[1
]}

机构：

[1] Univ Electrocommun, Dept Mech Engn & Intelligent Syst, 1-5-1 Chofugaoka, Chofu, Tokyo 1828585, Japan

来源：

IEEE ICMA 2006: PROCEEDING OF THE 2006 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION, VOLS 1-3, PROCEEDINGS | 2006年

关键词：

flight machine; active wing; macro fiber composites; flapping; feathering;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Macro Fiber Composites (MFC) is a new type of piezoelectric material with softness and big displacement, developed by NASA recently. It can be used for actuating, sensing and power generating. The purpose of our work is to develop a new and intelligent flight machine by utilizing the features of the MFC. In this paper, the concept of such flight machine and the driving method of a MFC-combined structure are proposed. The feasibility of flight by using the MFC-combined structure is discussed by simulations. Based on the simulation results, an active wing capable of flapping and feathering motions has been developed. The elementary performance of the wing is investigated by an aerodynamics experiment.

引用

页码：261 / +

页数：2

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