Hostname: page-component-586b7cd67f-g8jcs Total loading time: 0 Render date: 2024-11-24T05:39:16.407Z Has data issue: false hasContentIssue false
  • English
  • Français

Morphing structure for a rudder

Part of: Smart Aircraft

Published online by Cambridge University Press:  20 June 2016

M. A. Castillo-Acero ,
C. Cuerno-Rejado  and
M. A. Gómez-Tierno
M. A. Castillo-Acero*
Affiliation:
Aernnova, C. Princesa de Éboli, Madrid, Spain
C. Cuerno-Rejado
Affiliation:
Escuela Técnica Superior Ingenieros Aeronáuticos, UPM, Madrid 28040, Spain
M. A. Gómez-Tierno
Affiliation:
Escuela Técnica Superior Ingenieros Aeronáuticos, UPM, Madrid, Spain
*
[email protected]
Get access Rights & Permissions [Opens in a new window]

Abstract

The modification of aerofoils with structural morphing in order to enhance aerodynamic efficiency is an active field of research. The required forced and induced displacements are, usually, out the current developments on shape memory alloys, piezoelectric actuators or multi-stable structures for commercial transport aircraft applications. This work aims to present studies for obtaining an optimum rudder structure which morphs to a pre-defined curvature that can sustain aerodynamic and internal loads in a critical certification load case for a commercial transport aircraft. It also includes the feasibility of a morphing rudder based on a zero Poisson skeleton, or close to a zero Poisson ratio panel geometrical configuration that has no transverse deformation when perpendicularly loaded and which is produced with an additive layer manufacturing process.

Keywords

morphingstructuresvertical stabilizerrudderzero Poisson skeletonsadditive layer manufacturing
Type
Research Article
Information
The Aeronautical Journal , Volume 120 , Issue 1230 , August 2016 , pp. 1291 - 1314
Copyright
Copyright © Royal Aeronautical Society 2016 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

1. Castillo-Acero, M.A., Cuerno-Rejado, C. and Gómez-Tierno, M.A. Aerodynamic modelling for a morphing rudder, Proceedings of the 2014 RAES Aerodynamics Conference, 22-24 July 2014, RAES Bristol, UK.Google Scholar
2. Barbarino, S., Bilgen, O., Ajaj, R.M., Friswell, M.I. and Inman, D.J. A review of morphing aircraft, J Intelligence Materials, Systems and Structures, August 2011, 22, (9), pp 823–877.CrossRefGoogle Scholar
3. Sofla, A.Y.N., Meguid, S.A., Tan, K.T. and Yeo, W.K. Shape morphing of aircraft wing: status and challenges, Materials and Design, March 2010, 31, (3), pp 1284–1292.CrossRefGoogle Scholar
4. Portela, P., Camanho, P., Weaver, P. and Bond, I. Analysis of morphing, multi stable structures actuated by piezoelectric patches, Computers and Structures, February 2008, 86, (3–5), pp 347–356.CrossRefGoogle Scholar
5. Monner, H.P. Realization of an optimized wing camber by using form variable flap structures, Aerospace Science Technology, 5, (7), pp 445–455.CrossRefGoogle Scholar
6. Pecora, R., Amoroso, F. and Magnifico, M. Design and experimental validation of a morphing wing flap device, Proceedings of the 6th ECCOMAS Conference on Smart Structures and Materials (SMART’13), 24-26 June 2013, Politecnico di Torino, Turin, Italy.Google Scholar
7. Lachenal, X., Daynes, S. and Weaver, P.M. Review of morphing concepts and materials for wind turbine blade applications, Wind Energy, February 2013, 16, pp 283–307.CrossRefGoogle Scholar
8. Daynes, S. and Weaver, P.M. A morphing trailing edge device for a wind turbine, J Intelligence Materials, Systems and Structures, March 2012, 23, (6), pp 691–701.CrossRefGoogle Scholar
9. Daynes, S. and Weaver, P.M. Design and testing of a deformable wind turbine blade control surface, Smart Materials and Structures, 21, (10), pp 105–119.Google Scholar
10. Schweiger, J. and Krammer, J. Active aircraft and its impact on structure flight control systems design, RTO AVT Specialists’ Meeting on Structural Aspects of Flexible Aircraft, 18-20 October 1999, Ottawa, Ontario, Canada.Google Scholar
11. Schweiger, J. Active aeroelastic aircraft concepts, RTA-AVT-86 Technical Course, 25-29 March 2002, METU, Ankara, Turkey.Google Scholar
12. Gomez, J.C. and Garcia, E. Morphing unmanned aerial vehicles, Smart Materials and Structures, 20, (10), p 103001 (16pp).CrossRefGoogle Scholar
13. Vocke, R.D., Kothera, C.S., Woods, B.K.S., Bubert, E.A. and Wereley, N.M. One dimensional morphing structures for advanced aircraft, Phase I SBIR Project from NASA Langley Research Center, contract number NNX09CF06P, 2007.Google Scholar
14. 3D systems Corporation, Professional 3D Printers Productivity Precision, available on line, accessed 2 March 2014, http://www.3dsystems.com.Google Scholar
15. Bubert, E.A. Highly Extensible Skin for a Variable Wing-Span Morphing Aircraft Utilizing Pneumatic Artificial Muscle, MSc Thesis, University of Maryland, USA, 2009.Google Scholar
16. Farrar, D.J. Investigation of skin buckling, ARC R&M No. 2652, 1953.Google Scholar
17. Vos, R. Mechanics and applications of pressure adaptive honeycomb, PhD Thesis, University of Kansas, USA, 2009.CrossRefGoogle Scholar
18. Chen, J., Wang, Q., Shen, W.Z., Pang, X., Li, S. and Guo, X. Structural optimization study of composite wind turbine blade, Materials and Design, April 2013, 46, pp 247–255.CrossRefGoogle Scholar
19. Wang, H.M., Gao, H., Luo, X.Y., Berry, C., Griffith, B.E., Ogden, R.W. and Wang, T.J. Structure-based finite strain modeling of the human left ventricle in diastole, Int J Numerical Methods in Biomedical Engineering, June 2013, 29, pp 83–103.CrossRefGoogle ScholarPubMed
20. Diaconu, C.G., Weaver, P.M. and Mattioni, F. Concepts for morphing airfoil sections using bi-stable laminated composite structures, Thin-Walled Structures, June 2008, 46, (6), pp 689–701.CrossRefGoogle Scholar
21. Kota, S., Hetrick, J. and Osborn, R. Design and application of compliant mechanisms for morphing, Smart Structures and Materials, June 2003, 5054, (734), pp 24–33.Google Scholar
22. Vasista, S., Tong, L. and Wong, K.C. Realization of morphing wings: a multidisciplinary challenge, J Aircraft, January 2012, 49, (1), pp 11–28.CrossRefGoogle Scholar
23. Jee, S. Development of morphing aircraft structures using SMP, AFIT/GSE/ENV/10-M02, Air Force Institute of Technology Graduate School of Engineering and Management, Wright-Patterson Air Force Base, Ohio, US, 2010.Google Scholar
24. Thill, C., Etches, J., Bond, I., Potter, K. and Weaver, P. Morphing skins, Aeronautical J, March 2008, 112, (1129), pp 117–139.CrossRefGoogle Scholar