Shape memory alloy based morphing aerostructures

Journal of Mechanical Design

Volumn 132, Issue 11, 2010, Pages

  Calkins, Frederick T ^a   Mabe, James H ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; AIRCRAFT ENGINES; APPLICATION PROGRAMS; ENGINES; FIGHTER AIRCRAFT; SOFTWARE TESTING; TURBOMACHINE BLADES;

ADAPTIVE STRUCTURE; AEROSTRUCTURES; AIRCRAFT COMPONENTS; AIRCRAFT PERFORMANCE; ALLOY TECHNOLOGY; CURRENT RATE; FLIGHT CONDITIONS; MORPHING; ROTOR BLADES; VARIABLE GEOMETRY;

SHAPE MEMORY EFFECT;

EID: 78649623929     PISSN: 10500472     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.4001119     Document Type: Article

References (22)

1. Cesnik, C, Last, H., and Martin, C, 2004, "A Framework for Morphing Capability Assessment," AIAA Paper No. AIAA-2004-1654.
2. Thill, C, Etches, J., Bond, I., Potter, K., and Weaver, P., 2008, "Morphing Skins," Aeronaut. J., 112, pp. 117-139.
3. Szodruch, J., and Hilbig, R., 1988, "Variable Wing Camber for Transport Aircraft," Prog. Aerosp. Sci., 25, pp. 297-328.
4. NASA, 1989, "Advanced Fighter Technology Integration F-111 Mission Adaptive Wing," NASA Conference, Dryden Flight Research Facility, Edwards, CA, Apr., Paper No. 3055.
5. Kauffman, G., and Mayo, I., 1997, "The Story of Nitinol: The Serendipitous Discovery of the Memory Metal and Its Applications," Chem. Educ, 2(2), pp. 1-21.
6. Lagoudas, D., 2008, Shape Memory Alloys: Modeling and Engineering Applications, Springer, New York, NY.
7. Pitt, D. M., Dunne, J. P., and White, E. V, 2001, "SAMPSON Smart Inlet SMA Powered Adaptive Lip Design and Static Test,"AIAA Paper No. AIAA-2001-1359.
8. Pitt, D. M., Dunne, J. P., and White, E. V, 2002, "SAMPSON Smart Inlet Design Overview and Wind Tunnel Test: I. Design Overview," Proc. SPIE, 4698, pp. 13-23.
9. Pitt, D. M., Dunne, J. P., and White, E. V, 2002, "SAMPSON Smart Inlet Design Overview and Wind Tunnel Test: II. Wind Tunnel Test," Proc. SPIE, 4698, pp. 24-36.
10. Jacot, A. D., 1999, "Shape Memory Alloy Consortium (SMAC)," Proc. SPIE, 3674, pp. 158-165.
11. Calkins, F, Butler, G., and Mabe, J., 2006, "Variable Geometry Chevrons for Jet Noise Reduction," AIAA Paper No. AIAA-2006-2546.
12. Mabe, J. H., Calkins, F T., and Butler, G. W., 2006, "Boeing's Variable Geometry Chevron: Morphing Aerostructure for Jet Noise Reduction," AIAA Paper No. AIAA-2006-2142.
13. Ruggeri, R. T., Bussom, R. C, and Arbogast, D. J., 2008, "Development of a 1/4-Scale NiTinol Actuator for Reconfigurable Structures," Proc. SPIE, 6930, p. 69300L.
14. Bushnell, G. S., Arbogast, D. J., and Ruggeri, R. T., 2008, "Shape Control of a Morphing Structure (Rotor Blade) Using a Shape Memory Alloy Actuator System," Proc. SPIE, 6928, p. 69282A.
15. Mabe, J., Ruggeri, R., and Calkins, F, 2006, "Characterization of Nickel-Rich Nitinol Alloys for Actuator Development," International Conference on Shape Memory and Superelastic Technologies, Pacific Grove, CA, May.
16. Otsuka, K., and Ren, X., 2005, "Physical Metallurgy of Ti-Ni Based Shape Memory Alloys," Prog. Mater. Sci., 50, pp. 511-678.
17. Wojcik, C, 2003, SMST-2003: Proceedings of the International Conference on Shape Memory and Superelastic Technologies, A. Pelton, and T. Duerig, eds., American Society for Metals, Metals Park, OH, pp. 43-52.
18. Wojcik, C, 2004, SMST-2004: Proceedings of the International Conference on Shape Memory and Superelastic Technologies, Baden-Baden, GE.
19. Julien, G., Nitinol Technologies Inc., 2002, "Manufacturing of Nitinol Parts and Forms," U.S. Patent No. 6,422,010.
20. Bridges, J., Wernet, M., and Brown, C, 2003, "Control of Jet Noise Through Mixing Enhancement," NASA Report No. NASA/TM 2003-212335.
21. Mabe, J., Gravatt, L., Bushnell, G., Gutmark, E., DiMicco, R., and Harris, C, 2008, "Shape Memory Alloy Actuators for Deployable Rotor Blade Aerodynamic Devices," AIAA Paper No. AIAA 2008-1451.
22. Mabe, J. H., Calkins, F T., and Alkislar, M. B., 2008, "Variable Area Jet Nozzle Using Shape Memory Alloy Actuators in an Antagonistic Design," Proc. SPIE, 6930, p. 69300T.