Knowledge Management System of Institue of Mechanics, CAS
| 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
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| Source Publication | Science China-Technological Sciences
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| 2011 | |
| Volume | 54Issue:2Pages:395-402 |
| ISSN | 1674-7321 |
| Abstract | 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. |
| Keyword | Piezoelectric Actuator Piezoelectric Fiber Composite Shape Control Aerodynamic Characteristics Morphing Wing |
| Subject Area | Engineering ; Materials Science |
| DOI | 10.1007/s11431-010-4212-0 |
| URL | 查看原文 |
| Indexed By | SCI ; EI |
| Language | 英语 |
| WOS ID | WOS:000286936400018 |
| WOS Research Area | Engineering ; Materials Science |
| WOS Subject | Engineering, Multidisciplinary ; Materials Science, Multidisciplinary |
| Funding Organization | 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). |
| Department | LMFS海洋环境与工程(LEM) |
| Classification | 二类/Q2 |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/45000 |
| Collection | 环境力学重点实验室(2009-2011) |
| Corresponding Author | Chen, WM (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Environm Mech, Beijing 100190, Peoples R China |
| Recommended Citation 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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| SCI-J2011113.pdf（819KB） | 开放获取 | -- | View Application Full Text | |||
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