PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Development of a shape memory alloy wire actuator to operate a morphing wing

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
DSC tests were performed on several types of SMAs to verify the phase-transformation temperatures, and then experiments to examine their characteristics were carried out. An electric-current was supplied to the SMA wire to measure the appropriate operational cur- rent range. The force generated by the SMA wire increased according to the supplied current, but it diminished when the over-current was supplied because thermo-mechanical properties of the wire started to degrade. The appropriate stress range for effective actuation charac- teristics was also investigated. The SMA wire actuator was designed to operate a morphing wing. Experiments for the wing were conducted to verify its characteristics and it was smo- othly deformed.
Rocznik
Strony
519--531
Opis fizyczny
Bibliogr. 12 poz., rys., tab.
Twórcy
autor
  • KAIST, School of Mechanical, Aerospace and Systems Engineering, Daejeon, Korea
autor
  • University of South Carolina, Department of Mechanical Engineering, Columbia, USA
autor
  • KAIST, School of Mechanical, Aerospace and Systems Engineering, Daejeon, Korea
autor
  • KAIST, School of Mechanical, Aerospace and Systems Engineering, Daejeon, Korea
Bibliografia
  • 1. Bowman J., Sanders B., Cannon B., Kudva J., Joshi S., Weisshaar T., 2007, Development of next generation morphing aircraft structures, Proc. 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conf. (SDM), AIAA-2007-1730
  • 2. Cloyd J.S., 1998, Status of the United States Air Force’s more electric aircraft initiative, IEEE Aerospace and Electronic Systems Magazine, 13, 4, 17-22
  • 3. Diaconu C.G., Weaver P.M., Mattioni F., 2008, Concepts for morphing airfoil sections Rusing bi-stable laminated composite structures, Thin-Walled Structures, 46, 6, 689-701
  • 4. Duerig T., Pelton A., Stockel D., 1999, An overview of nitinol medical applications,Materials Science and Engineering, A, 273/275, 149-160
  • 5. Joshi S.P., Tidwell Z., Crossley W.A., Ramakrishnan S., 2004, Comparison of morphing wing strategies based upon aircraft performance impacts, Proc. 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conf. (SDM), AIAA-2004-1722
  • 6. Kang W.R., Kim E.H., Jeong M.S., Lee I., 2012, Morphing wing mechanism using a SMA wire actuator, International Journal of Agricultural and Soil Science, 13, 1, 58-63
  • 7. Lee H.J., Lee J.J., Huh J.S., 1999, A simulation study on the thermal buckling behavior of laminated composite shells with embedded shape memory alloy (SMA) Wires, Composite Structures, 47, 1/4, 463-469
  • 8. Mattioni F., Gatto A., Weaver P.M., Friswell M.I., Potter K.D., 2006, The application of residual stress tailoring of snap-through composites for variable sweep wings, Proc. 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf. (SDM), AIAA-2006-1972
  • 9. Otsuka K., Wayman C.M., 1998, Shape Memory Materials, Cambridge University Press
  • 10. Sanders B., Estep F.E., Forster E., 2003, Aerodynamic and aeroelastic characteristics of wings with conformal control surfaces for morphing aircraft, Journal of Aircraft, 40, 1, 94-99
  • 11. Sanders B., Reich G.W., Joo J.J., 2005, Conceptual skin design for morphing aircraft, Proc. 16th Int. Conf. on Adaptive Structures and Technologies (ICAST), 16, 275-281
  • 12. Thill C., Etches J., Bond I., Potter K., Weaver P., 2008, Morphing skins, Aeronautical Journal, 112, 1129, 117-139
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-ffcfb728-27c5-4f7d-872a-4a2f78156d60
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.