Browse > Article
http://dx.doi.org/10.12989/sss.2011.7.1.001

Design and control of a proof-of-concept active jet engine intake using shape memory alloy actuators  

Song, Gangbing (Department of Mechanical Engineering, University of Houston)
Ma, Ning (Department of Mechanical Engineering, University of Houston)
Li, Luyu (Department of Mechanical Engineering, University of Houston)
Penney, Nick (Ohio Aerospace Institute (OAI))
Barr, Todd (Jackson & Tull Aerospace Division)
Lee, Ho-Jun (NASA Johnson Space Center)
Arnold, Steve (NASA Glenn Research Center)
Publication Information
Smart Structures and Systems / v.7, no.1, 2011 , pp. 1-13 More about this Journal
Abstract
It has been shown in the literature that active adjustment of the intake area of a jet engine has potential to improve its fuel efficiency. This paper presents the design and control of a novel proof-of-concept active jet engine intake using Nickel-Titanium (Ni-Ti or Nitinol) shape memory alloy (SMA) wire actuators. The Nitinol SMA material is used in this research due to its advantages of high power-to-weight ratio and electrical resistive actuation. The Nitinol SMA material can be fabricated into a variety of shapes, such as strips, foils, rods and wires. In this paper, SMA wires are used due to its ability to generate a large strain: up to 6% for repeated operations. The proposed proof-of-concept engine intake employs overlapping leaves in a concentric configuration. Each leaf is mounted on a supporting bar than can rotate. The supporting bars are actuated by an SMA wire actuator in a ring configuration. Electrical resistive heating is used to actuate the SMA wire actuator and rotate the supporting bars. To enable feedback control, a laser range sensor is used to detect the movement of a leaf and therefore the radius of the intake area. Due to the hysteresis, an inherent nonlinear phenomenon associated with SMAs, a nonlinear robust controller is used to control the SMA actuators. The control design uses the sliding-mode approach and can compensate the nonlinearities associated with the SMA actuator. A proof-of-concept model is fabricated and its feedback control experiments show that the intake area can be precisely controlled using the SMA wire actuator and has the ability to reduce the area up to 25%. The experiments demonstrate the feasibility of engine intake area control using an SMA wire actuator under the proposed design.
Keywords
shape memory alloy wire; Nitinol; jet engine intake; sliding mode control;
Citations & Related Records

Times Cited By Web Of Science : 1  (Related Records In Web of Science)
Times Cited By SCOPUS : 2
연도 인용수 순위
1 Barooah, P. and Rey, N. (2002), "Closed loop control of a shape memory alloy actuation system for variable area fan nozzle", Proceedings of the SPIE International Symposium on Smart Structures and Materials, 4693, 384- 395.
2 Barbarino, S., Pecora, R., Lecce, L., Concilio, A., Ameduri, S. and Calvi, E. (2009), "A novel SMA-based concept for airfoil structural morphing", J. Mater. Eng. Perform., 18(5-6), 696-705.   DOI   ScienceOn
3 Calkins, F.T., Mabe, J.H. and Butler, G.W. (2006), "Boeing's variable geometry chevron: Morphing aerospace structures for jet noise reduction", Proceedings of the SPIE - The International Society for Optical Engineering, 6171.
4 Choi, S.B., Han, Y.M. and Cheong, C.C. (2001), "Force tracking control of a flexible gripper featuring shape memory alloy actuators", Mechatronics, 11(6), 677-690.   DOI   ScienceOn
5 Dayananda, G.N., Varughese, B. and Subba Rao, M. (2007), "Shape memory alloy based smart landing gear for an airship", J. Aircraft, 44(5), 1469-1477.   DOI   ScienceOn
6 Epps, J. and Chopra, I. (2001), "In-flight tracking of helicopter rotor blades using shape memory alloy actuators", Smart Mater. Struct., 10(2001), 104-111.   DOI
7 Grant, D. and Hayward, V. (1997), "Variable structure control of shape memory alloy actuator", IEEE Contr. Syst. Mag., 17(3), 80-88.   DOI
8 Majima, S., Kodama, K. and Hasegawa, T. (2001), "Modeling of shape memory alloy actuator and tracking control system with the model", IEEE T. Contr. Syst. T., 9(1), 54-59.   DOI   ScienceOn
9 Peng, F., Jiang, X., Hu, Y. and Ng, A. (2009), "Application of SMA in membrane structure shape control", IEEE T. Aero. Elec. Sys., 45(1), 85-93.   DOI
10 Pitt, D.M., Dune, J.P., White, E.V. and Garcia, E. (2001), "Wind tunnel demonstration of the SMAPON smart inlet", Proceedings of the SPIE International Symposium on Smart Structures and Materials, 4332, 345-356.
11 Rey, N.M., Tillman, G., Miller, R.M., Wynosky, T., Larkin, M.J., Flamm, J.D. and Bangert, L.S. (2001), "Shape memory alloy actuation for a variable area fan nozzle", Proceedings of the SPIE International Symposium on Smart Structures and Materials, 4332, 371-382.
12 Song, G. and Mukherjee, R. (1998), "A comparative study of conventional non-smooth time-invariant and smooth time-varying robust compensators", IEEE T. Contr. Syst. T., 6(4), 571-576.   DOI   ScienceOn
13 Song, G. and Quinn, D. (2000), "Robust tracking control a shape memory alloy wire actuator", Proceedings of the Symposium on Control of Vibration and Noise at ASME International Mechanical Engineering Congress and Exposition.
14 Strelec, J.K., Lagoudas, D.C., Khan, M.A. and Yen, J. (2003), "Design and implementation of a shape memory alloy actuated reconfigurable airfoil", J. Intel. Mater. Syst. Str., 14(4-5), 257-273.   DOI
15 Wolf, W. and Gunter, P. (2001), "Shape adaptive structures for smart airfoils", Proceedings of the IEEE International Conference on Multisensor Fusion and Integration for Intelligent Systems, Baden-Baden, Germany, August.