Improvements to commercial and general aviation via adaptive aerostructures

Collection of Technical Papers - 7th AIAA Aviation Technology, Integration, and Operations Conference

Volumn 2, Issue , 2007, Pages 1786-1794

  Barrett, Ron ^a  

^a University of Kansas   (United States)

Author keywords

Flight control; MAV; PBP; Piezoelectric; UAV

Indexed keywords

FLIGHT CONTROL SYSTEMS; JET AIRCRAFT; MISSILES; PIEZOELECTRIC MATERIALS; UNMANNED AERIAL VEHICLES (UAV); VIBRATIONAL SPECTRA;

ADAPTIVE AEROSTRUCTURES; ADAPTIVE MATERIALS; CHANGE MODULUS; JET NOISE SUPPRESSION; MUNITIONS;

CIVIL AVIATION;

EID: 37249007761     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-7873     Document Type: Conference Paper

References (21)

1. Barrett, R., "Actuation Strain Decoupling Through Enhanced Directional Attachment in Plates and Aerodynamic Surfaces," proceedings of the First European Conference on Smart Structures and Materials, Glasgow, Scotland, 12-14 May 1992, edited by B. Culshaw, P. T. Gardiner, and A. McDonach, Institute of Physics Publishing, Bristol, UK 1992, pp. 383-386.
2. Barrett, R., "Modeling Techniques and Design Principles of a Low Aspect Ratio Active Aeroservoelastic Wing," proceedings of the SPIE 1993 Symposium on Smart Structures and Materials, Albuquerque, NM, 1-4 February 1993, published by the SPIE, Bellingham, WA, Vol. 1917, pp. 107-118.
3. Barrett, R., Brozoski, F., and Gross, R. S., "Design and Testing of Subsonic AllMoving Smart Flight Control Surfaces," proceedings of the 36th Structures, Structural Dynamics and Materials Conference, New Orleans, LA, April 10-12, 1995, published by the AIAA, Washington, D.C., pp. 2289-2296
4. Barrett, R., "Active Aeroelastic Tailoring of an Adaptive Flexspar Stabilator," Journal of Smart Materials and Structures, Vol. 5, No. 6 December 1996, Techno House, Bristol, UK, 1996, pp. 723-730. See also proceeding 4.B.2.b.6 and invited paper 4.B.2.c.3.
5. Barrett, R. and Brozoski, F., "Missile Flight Control using Active Flexspar Actuators, " Journal of Smart Materials and Structures, Institute of Physics Publishing, Ltd., Techno House, Bristol, UK, Vol. 5, No. 2, March 1996, pp. 121-128._Also proceedings publication. See also proceeding 4.B.2.b.7. Institute of Physics Publishing featured article for Fall 1996, http://www.ioppublishing.com/Journals/sm.
6. Barrett, R., Frye, P., and Schliesman, M., "Design, Development and Testing of a Solid State Adaptive Rotorcraft," proceedings of the 4th Annual Society of PhotoOptical Instrumentation Engineers Symposium on Smart Structures and Materials, San Diego, CA 3-6 March 1997 SPIE paper no. 3041-19, pp. 231-242.
7. Barrett, R. and Lee, G., "Design Criteria, Aircraft Design, Fabrication and Testing of Sub-Canopy and Urban Micro-Aerial Vehicles," proceedings of the AIAA/AHS International Powered Lift Conference, Alexandria, Virginia, 1 November 2000.
8. Barrett, R., "Convertible Vertical Take-Off and Landing Miniature Aerial Vehicle," US Patent 6,502,787, issued 7 January 2003.
9. th European Demonstrators Conference, 10-15 December 2001, Edinburgh, Scotland.
10. Barrett, R. and Lee, G., "Design Criteria, Aircraft Design, Fabrication and Testing of Sub-Canopy and Urban Micro-Aerial Vehicles," proceedings of the AIAA/AHS International Powered Lift Conference, Alexandria, Virginia, 1 November 2000.
11. Barrett, R., and Stutts, J., "Development of a Piezoceramic Flight Control Surface Actuator for Highly Compressed Munitions," proceedings of the 39th Structures, Structural Dynamics and Materials Conference 20-23 April 1998, Long Beach, CA, published by the American Institute of Aeronautics and Astronautics, Washington, D.C. 1998, paper no. AIAA-98-2034.
12. th AIAA/ASME/AHS Adaptive Structures Conference 19-22 April 2004/Palm Springs, California, AIAA paper no. 2004-1886.
13. Lesieutre, G.A., and C.L. Davis, "Can a Coupling Coefficient of a Piezoelectric Actuator be Higher Than Those of Its Active Material?," Journal of Intelligent Materials Systems and Structures, Vol. 8, 1997, pp. 859-867.
14. Lesieutre, G. A. and Davis, C. L., "Transfer Having a Coupling Coefficient Higher than its Active Material," US Pat. 6,236,143 issued 22 May 2001.
15. Barrett, R. and Tiso, P. "PBP Adaptive Actuator Device and Embodiments," International Patent Application number PCT/NL2 005/000054, via TU Delft, 18 February 2005.
16. Barrett, R., Vos, R., Tiso, P. and De Breuker, R., "Post-Buckled Precompressed (PBP) Actuators: Enhancing VTOL Autonomous High Speed MAVs," Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference , Austin, Texas, Apr. 18-21, 2005, AIAA paper no. AIAA-2005-2113.
17. Vos, R., De Breuker, R., Barrett, R. and Tiso, P., " Morphing Wing Flight Control Via Post-Buckled Precompressed Piezoelectric Actuators," accepted for publication in the AIAA Journal of Aircraft," 13 June 2006.
18. Barrett, R., McMurtry, R., Vos, R.., Tiso, P. and De Breuker, R., "Post-Buckled Precompressed Piezoelectric Flight Control Actuator Design, Development and Demonstration," Journal of Smart Materials and Structures, Volume 15, No. 5, October 2006 1323-1331.
19. De Breuker, R., Vos, R., Barrett, R. and Tiso, P., "Nonlinear Semi-Analytical Modeling of Post-Buckled Precompressed (PBP) Piezoelectric Actuators for UAV Flight Control," Proceedings of the 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th, Newport, Rhode Island, May 1-4, 2006 AIAA-2006-1795.
20. Jones, R. M., "Micromechanical Behavior of a Lamina," Mechanics of Composite Materials, Hemisphere Publishing Corporation, New York, 1975.
21. Barrett, R. M., Gross, R. S. and Brozoski, F. T., "Design and Testing of a Subsonic All-Moving Adaptive Flight Control Surface," AIAA Journal, Volume 35, Number 7, July 1997.