Aerospace | |
Decamber Morphing Concepts by Using a Hybrid Trailing Edge Control Surface | |
Yavuz Yaman1  İlhan Ozan Tunçöz1  Yosheph Yang1  Pınar Arslan1  Uğur Kalkan1  Harun Tıraş1  Ercan Gürses1  Melin ᗪhin1  Serkan Özgen1  | |
关键词: camber morphing; hybrid control surface; structural analysis; finite element method; | |
DOI : 10.3390/aerospace2030482 | |
来源: mdpi | |
【 摘 要 】
The idea of morphing is drawing extensive attention in aerospace technologies. Several different approaches like span, camber, twist, and sweep are finding applications. In this work, the concept of a trailing edge control surface which is capable of performing decamber morphing is explained. The upper and lower parts of the control surface undergo different chordwise elongations and the difference between these displacements gives rise to either camber or decamber morphing. The necessary force is achieved by the help of servo actuators. During the design, the structural analyses were done to determine the best viable options for the number of servo actuators, the location of the servo actuators, and the material properties used in the control surface. The control surface was designed of aluminum, composite and compliant materials hence was called a hybrid one. The structural analyses were conducted by using ANSYS® Workbench v14.0 package program. After finding the best viable design, which was made for
【 授权许可】
CC BY
© 2015 by the authors; licensee MDPI, Basel, Switzerland.
【 预 览 】
Files | Size | Format | View |
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RO202003190008452ZK.pdf | 3531KB | download |