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

doi:10.1007/s11431-010-4212-0

IMECH-IR > 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); Chen, WM (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Environm Mech, Beijing 100190, Peoples R China
发表期刊	Science China-Technological Sciences
	2011
卷号	54 期号:2 页码:395-402
ISSN	1674-7321
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.
关键词	Piezoelectric Actuator Piezoelectric Fiber Composite Shape Control Aerodynamic Characteristics Morphing Wing
学科领域	Engineering ; Materials Science
DOI	10.1007/s11431-010-4212-0
URL	查看原文
收录类别	SCI ; EI
语种	英语
WOS记录号	WOS:000286936400018
WOS研究方向	Engineering ; Materials Science
WOS类目	Engineering, Multidisciplinary ; Materials Science, Multidisciplinary
项目资助者	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).
课题组名称	LMFS海洋环境与工程(LEM)
论文分区	二类/Q2
引用统计	被引频次：21[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/45000
专题	环境力学重点实验室(2009-2011)
通讯作者	Chen, WM (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Environm Mech, Beijing 100190, Peoples R China
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,&Chen, WM .(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.

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