Application of piezoelectric fiber composite actuator to aircraft wing for aerodynamic performance improvement

CORC > 力学研究所 > 中国科学院力学研究所 > 环境力学重点实验室(2009-2011)

	Application of piezoelectric fiber composite actuator to aircraft wing for aerodynamic performance improvement
	Li M; Yuan JX; Guan D; Chen WM(陈伟民)
刊名	Science China-Technological Sciences
	2011
通讯作者邮箱	wmchen@imech.ac.cn
卷号	54 期号:2 页码:395-402
关键词	Piezoelectric Actuator Piezoelectric Fiber Composite Shape Control Aerodynamic Characteristics Morphing Wing
ISSN号	1674-7321
通讯作者	Chen, WM (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Environm Mech, Beijing 100190, Peoples R China
产权排序	[Chen WeiMin] Chinese Acad Sci, Inst Mech, Key Lab Environm Mech, Beijing 100190, Peoples R China; [Li Min; Yuan JunXian; Guan De] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
合作状况	国内
中文摘要	The application of actuator made of piezoelectric material, particularly the advanced piezoelectric fiber composite due to the rapid development of smart materials and structures and active control technology in aviation and aerospace industry, to aircraft for performance enhancements such as flight control, aerodynamic force optimization, structure weight reduction, and overall aircraft design represents a new challenge to researches. It is considered as one of the key technologies for developing future flight vehicle. An approach with virtual control surface instead of conventional control surface to control aerodynamic force distribution and flight performance by use of piezoelectric fiber composite actuators distributed on wing surface is presented here. Particularly, the design and implementation of increasing lift force, providing roll maneuver, decreasing induced drag and wing root moment in different flight environments by the same structure control platform are studied. The control effect and sensitivity are examined quantitatively. Generally speaking, better control effect can be obtained by making better use of aeroelastic character to enlarge the actuation strain produced by piezoelectric material.
学科主题	Engineering; Materials Science
分类号	二类/Q2
类目[WOS]	Engineering, Multidisciplinary ; Materials Science, Multidisciplinary
研究领域[WOS]	Engineering ; Materials Science
收录类别	SCI ; EI
资助信息	This work was supported by the Fundamental Research Funds for the Central Universities (Grant No. YWF-10-01-B05), the National Natural Science Foundation of China (Grant No. 10772183) and the Intellectual Innovation Project of the Chinese Academy of Sciences (Grant No. KJCX2-YW-L07).
原文出处	http://dx.doi.org/10.1007/s11431-010-4212-0
语种	英语
WOS记录号	WOS:000286936400018
公开日期	2012-04-01
内容类型	期刊论文
源URL	[http://dspace.imech.ac.cn/handle/311007/45000]
专题	力学研究所_环境力学重点实验室(2009-2011)
推荐引用方式 GB/T 7714	Li M,Yuan JX,Guan D,et al. Application of piezoelectric fiber composite actuator to aircraft wing for aerodynamic performance improvement[J]. Science China-Technological Sciences,2011,54(2):395-402.
APA	Li M,Yuan JX,Guan D,&陈伟民.(2011).Application of piezoelectric fiber composite actuator to aircraft wing for aerodynamic performance improvement.Science China-Technological Sciences,54(2),395-402.
MLA	Li M,et al."Application of piezoelectric fiber composite actuator to aircraft wing for aerodynamic performance improvement".Science China-Technological Sciences 54.2(2011):395-402.