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Variable camber morphing wing mechanism using deployable scissor structure: Design, analysis and manufacturing

  • Choi, Yeeryung (Department of Aerospace Engineering, Seoul National University) ;
  • Yun, Gun Jin (Institute of Advanced Aerospace Technology, Seoul National University)
  • Received : 2021.08.25
  • Accepted : 2022.02.05
  • Published : 2022.03.25
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Abstract

In this paper, a novel morphing mechanism using a deployable scissor structure was proposed for a variable camber morphing wing. The mechanism was designed through the optimization process so that the rib can form the target airfoils with different cambers. Lastly, the morphing wing was manufactured and its performance was successfully evaluated. The mechanism of the morphing wing rib was realized by a set of deployable scissor structure that can form diverse curvatures. This characteristic of the structure allows the mechanism to vary the camber that refers to the airfoil's curvature. The mechanism is not restrictive in defining the target shapes, allowing various airfoils and overall morphing wing shape to be implemented.

Keywords

Acknowledgement

This research is based upon work supported by the Air Force Office of Scientific Research under award number FA2386-17-1-4081 and the Institute of Engineering Research at Seoul National University. The authors are grateful for their supports.

References

  1. Abdulrahim, M. (2005), "Flight performance characteristics of a biologically-inspired morphing aircraft", 43rd AIAA Aerospace Sciences Meeting and Exhibit, 345, January.
  2. Abdulrahim, M. and Lind, R. (2004), "Flight testing and response characteristics of a variable gull-wing morphing aircraft", AIAA Guidance, Navigation, and Control Conference and Exhibit, 5113. August.
  3. Ajaj, R.M., Flores, E.S., Friswell, M.I., Allegri, G., Woods, B.K.S., Isikveren, A.T. and Dettmer, W.G. (2013), "The Zigzag wingbox for a span morphing wing", Aerosp. Sci. Technol., 28(1), 364-375. https://doi.org/10.1016/j.ast.2012.12.002.
  4. Ajaj, R.M., Friswell, M.I., Bourchak, M. and Harasani, W. (2016), "Span morphing using the GNATSpar wing", Aerosp. Sci. Technol., 53, 38-46. https://doi.org/10.1016/j.ast.2016.03.009.
  5. Andersen, G., Cowan, D. and Piatak, D. (2007), "Aeroelastic modeling, analysis and testing of a morphing wing structure", 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 1734, April.
  6. Barbarino, S., Bilgen, O., Ajaj, R.M., Friswell, M.I. and Inman, D.J. (2011), "A review of Morphing aircraft", J. Intel. Mater. Syst. Struct., 22(9), 823-877. https://doi.org/10.1177/1045389X11414084.
  7. Bourdin, P., Gatto, A. and Friswell, M.I. (2008), "Aircraft control via variable cant-angle winglets", J. Aircraft, 45(2), 414-423. https://doi.org/10.2514/1.27720.
  8. Cuji, E. and Garcia, E. (2008), "Aircraft dynamics for symmetric and asymmetric V-shape Morphing wings", Smart Materials, Adaptive Structures and Intelligent Systems, Vol. 43321, 579-588, January.
  9. Dale, A., Cooper, J.E. and Mosquera, A. (2013), "Adaptive Camber-Morphing wing using 0-? Honeycomb", 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 1510.
  10. Detrick, M. and Washington, G. (2007), "Modeling and design of a morphing wing for micro unmanned aerial vehicles via active twist", 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 1788, April.
  11. Dimino, I., Ciminello, M., Gratias, A., Schueller, M. and Pecora, R. (2017), "Control system design for a morphing wing trailing edge", Smart Structures and Materials, 175-193, Springer, Cham.
  12. Elzey, D.M., Sofla, A.Y.N. and Wadley, H.N. (2003), "A bio-inspired high-authority actuator for shape morphing structures", Smart Sstructures and Materials 2003: Active Materials: Behavior and Mechanics, Vol. 5053, 92-100, August.
  13. de Marmier, P. and Wereley, N. (2003), "Control of sweep using pneumatic actuators to morph wings of small scale UAVs", 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 1802.
  14. De Temmerman, N. (2007), "Design and analysis of deployable bar structures for mobile architectural applications", Ph.D. Dissertation, Vrije Universiteit Brussel, Brussels, Belgium.
  15. Finistauri, A.D. and Xi, F.J. (2009), "Type synthesis and kinematics of a modular variable geometry truss mechanism for aircraft wing morphing", 2009 ASME/IFToMM International Conference on Reconfigurable Mechanisms and Robots, 478-485.
  16. Fenci, G.E. and Currie, N.G. (2017), "Deployable structures classification: A review", Int. J. Space Struct., 32(2), 112-130. https://doi.org/10.1177/0266351117711290.
  17. Joo, J.J., Marks, C.R., Zientarski, L. and Culler, A.J. (2015), "Variable camber compliant wing-design 23rd AIAA", AHS Adaptive Structures Conference.
  18. Kimaru, J. and Bouferrouk, A. (2017), "Design, manufacture and test of a camber morphing wing using MFC actuated mart rib", 2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 791-796, July.
  19. Langbecker, T. (1999), "Kinematic analysis of deployable scissor structures", Int. J. Space Struct., 14(1), 1-15. https://doi.org/10.1260/0266351991494650.
  20. Majji, M., Rediniotis, O. and Junkins, J. (2007), "Design of a morphing wing: modeling and experiments", AIAA Atmospheric Flight Mechanics Conference and Exhibit, 6310, August.
  21. Marks, C.R., Zientarski, L., Culler, A.J., Hagen, B., Smyers, B.M. and Joo, J.J. (2015), "Variable camber compliant wing-wind tunnel testing", 23rd AIAA/AHS Adaptive Structures Conference, 1051.
  22. Marques, M., Gamboa, P. and Andrade, E. (2009), "Design and testing of a variable camber flap for improved efficiency", The Applied Vehicle Technology Panel Symposium (AVT-168), April.
  23. Mestrinho, J., Gamboa, P. and Santos, P. (2011), "Design optimization of a variable-span morphing wing for a small UAV", 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 19th AIAA/ASME/AHS Adaptive Structures Conference 13t, 2025.
  24. Monner, H., Kintscher, M., Lorkowski, T. and Storm, S. (2009), "Design of a smart droop nose as leading edge high lift system for transportation aircrafts", 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 17th AIAA/ASME/AHS Adaptive Structures Conference 11th AIAA No, 2128, May.
  25. Pagani, A., Zappino, E., de Miguel, A.G., Martilla, V. and Carrera, E. (2019), "Full field strain measurements of composite wing by digital image correlation", Adv. Aircraft Spacecraft Sci., 6(1), 69-86. https://doi.org/10.12989/aas.2019.6.1.069.
  26. Prabhakar, N., Prazenica, R.J. and Gudmundsson, S. (2015), "Dynamic analysis of a variable-span, variablesweep morphing UAV", 2015 IEEE Aerospace Conference, 1-12, March.
  27. Raither, W., Heymanns, M., Bergamini, A. and Ermanni, P. (2013), "Morphing wing structure with controllable twist based on adaptive bending-twist coupling", Smart Mater. Struct., 22(6), 065017. https://doi.org/10.1088/0964-1726/22/6/065017.
  28. Rivero, A.E., Weaver, P.M., Cooper, J.E. and Woods, B.K. (2017), "Progress on the design, analysis and experimental testing of a composite fish bone active camber Morphing wing", ICAST 2017: 28th International Conference on Adaptive Structures and Technologies, 1-11, October.
  29. Rivero, A.E., Weaver, P.M., Cooper, J.E. and Woods, B.K. (2018), "Parametric structural modelling of fish bone active camber morphing aerofoils", J. Intel. Mater Syst. Struct., 29(9), 2008-2026. https://doi.org/10.1177/1045389X18758182.
  30. Roovers, K. and De Temmerman, N. (2017), "Deployable scissor grids consisting of translational units", Int. J. Solid. Struct., 121, 45-61. https://doi.org/10.1016/j.ijsolstr.2017.05.015.
  31. Seow, A.K., Liu, Y. and Yeo, W.K. (2008), "Shape memory alloy as actuator to deflect a wing flap", 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 16th AIAA/ASME/AHS Adaptive Structures Conference, 10th AIAA Non-Deterministic Approaches Conference, 9th AIAA Gossamer Spacecraft Forum, 4th AIAA Multidisciplinary Design Optimization Specialists Conference, 1704.
  32. Sofla, A.Y.N., Meguid, S.A., Tan, K.T. and Yeo, W.K. (2010), "Shape morphing of aircraft wing: Status and challenges", Mater. Des., 31(3), 1284-1292. https://doi.org/10.1016/j.matdes.2009.09.011.
  33. Tarabi, A., Ghasemloo, S. and Mani, M. (2016), "Experimental investigation of a variable-span morphing wing model for an unmanned aerial vehicle", J. Brazil. Soc. Mech. Sci. Eng., 38(7), 1833-1841. https://doi.org/10.1007/s40430-015-0405-6.
  34. Vocke III, R.D., Kothera, C.S., Woods, B.K. and Wereley, N.M. (2011), "Development and testing of a span-extending morphing wing", J. Intel. Mater. Syst. Struct., 22(9), 879-890. https://doi.org/10.1177/1045389X11411121.
  35. Vos, R., Gurdal, Z. and Abdalla, M. (2010), "Mechanism for warp-controlled twist of a morphing wing", J. Aircraft, 47(2), 450-457. https://doi.org/10.2514/1.39328.
  36. Wlezien, R.W., Horner, G.C., McGowan, A.M.R., Padula, S.L., Scott, M.A., Silcox, R.J. and Harrison, J.S. (1998), "Aircraft morphing program", Smart Structures and Materials 1998: Industrial and Commercial Applications of Smart Structures Technologies, Vol. 3326, 176-187.
  37. Yokozeki, T., Sugiura, A. and Hirano, Y. (2014), "Development and wind tunnel test of variable camber morphing wing", 22nd AIAA/ASME/AHS Adaptive Structures Conference, 1261.
  38. Yokozeki, T., Sugiura, A. and Hirano, Y. (2014a), "Development of variable camber morphing airfoil using corrugated structure", J. Aircraft, 51(3), 1023-1029. https://doi.org/10.2514/1.C032573.
  39. Zhang, J., Shaw, A.D., Wang, C., Gu, H., Amoozgar, M., Friswell, M.I. and Woods, B.K. (2021), "Aeroelastic model and analysis of an active camber morphing wing", Aerosp. Sci. Technol., 111, 106534. https://doi.org/10.1016/j.ast.2021.106534.
  40. Zhao, J.S., Chu, F. and Feng, Z.J. (2009), "The mechanism theory and application of deployable structures based on SLE", Mech. Mach. Theory, 44(2), 324-335. https://doi.org/10.1016/j.mechmachtheory.2008.03.014.