DocumentCode
691313
Title
Dynamics modeling of piezoelectric control for the aircraft wings in aerodynamic thermal environment
Author
Hong-hao Yue ; Lei Wang ; Jing Jiang ; Xi-tao Song ; Zheng-wang Yu
Author_Institution
Sch. of Mechatron. Eng., Harbin Inst. of Technol., Harbin, China
fYear
2013
fDate
25-27 Oct. 2013
Firstpage
1
Lastpage
4
Abstract
In this paper, the aircraft wings are simplified as the cantilever beam structure. Piezoelectric actuator is used to eliminate the effects in the thermal environment. Mathematical modeling of cantilever beam in the temperature field are built. Simulation of the accessional control by piezoelectric film model show the feasibility of the control method preliminarily. And our purpose is enhance the performance of the structures on the base of general materials by using smart material and effective control methods in the future.
Keywords
aerodynamics; aerospace components; aircraft; beams (structures); cantilevers; piezoelectric actuators; aerodynamic thermal environment; aircraft wings; cantilever beam structure; dynamics modeling; piezoelectric actuator; piezoelectric control; Aircraft wing; Piezoelectric control; Thermal environment;
fLanguage
English
Publisher
ieee
Conference_Titel
Piezoelectricity, Acoustic Waves and Device Applications (SPAWDA), 2013 Symposium on
Conference_Location
Changsha
Print_ISBN
978-1-4799-3289-4
Type
conf
DOI
10.1109/SPAWDA.2013.6841100
Filename
6841100
Link To Document