Investigating potential substrates to maximize out-of-plane deflection of piezoelectric macro-fiber composite actuators

The work summarized here explores the application of various substrate materials to macro-fiber composites for the purpose of generating curvature. This research experimentally determines the free strain of the macro-fiber composite through its full range of actuation and then examines the resulting deflections when bonded to various substrates. In addition, loads are applied to the resulting unimorph while in a cantilever configuration and the deflections recorded. These results are used to validate finite element models, which are used to explore further design possibilities, including a bimorph configuration. The goal of this work is to determine the substrates that maximize curvature in both unloaded and loaded configurations. The results show that using thin and high modulus substrates results in the largest deflection under loading.

[1]  R. Gibson Principles of Composite Material Mechanics , 1994 .

[2]  Eglin Afb,et al.  Piezoelectric Morphing versus Servo-Actuated MAV Control Surfaces, Part II: Flight Testing , 2013 .

[3]  Paul H. Mirick,et al.  Low-cost piezocomposite actuator for structural control applications , 2000, Smart Structures.

[4]  Daniel J. Inman,et al.  A novel unmanned aircraft with solid-state control surfaces: Analysis and flight demonstration , 2011 .

[5]  Hoon Cheol Park,et al.  Validation of a Laminated Beam Model of LIPCA Piezoelectric Actuators , 2005 .

[6]  Wilkie W. Keats,et al.  Aeroelastic Analysis of Helicopter Rotor Blades Incorporating Anisotropic Piezoelectric Twist Actuation , 1996 .

[7]  Yong Chen,et al.  Design and verification of a smart wing for an extreme-agility micro-air-vehicle , 2011 .

[8]  Anna-Maria Rivas McGowan,et al.  Overview of the DARPA/AFRL/NASA Smart Wing program , 1999, Smart Structures.

[9]  J. N. Kudva,et al.  Overview of the DARPA Smart Wing Project , 2004 .

[10]  Ron Barrett,et al.  Post-buckled precompressed piezoelectric flight control actuator design, development and demonstration , 2006 .

[11]  Daniel J. Inman,et al.  Macro-fiber composite actuators for a swept wing unmanned aircraft , 2009, The Aeronautical Journal (1968).

[12]  Ron Barrett,et al.  Post-buckled precompressed elements: a new class of control actuators for morphing wing UAVs , 2007 .

[13]  Viresh Wickramasinghe,et al.  Material characterization of active fiber composites for integral twist-actuated rotor blade application , 2004 .

[14]  R. Williams Nonlinear Mechanical and Actuation Characterization of Piezoceramic Fiber Composites , 1999 .

[15]  H. Park,et al.  Design and manufacture of a lightweight piezo-composite curved actuator , 2002 .

[16]  Ron Barrett,et al.  Post-buckled precompressed subsonic micro-flight control actuators and surfaces , 2008 .

[17]  W. Keats Wilkie,et al.  Method of Fabricating NASA-Standard Macro-Fiber Composite Piezoelectric Actuators , 2003 .

[18]  S. Hall,et al.  Closed-loop vibration control experiments on a rotor with blade mounted actuation , 2000 .

[19]  Rolf Paradies,et al.  Active wing design with integrated flight control using piezoelectric macro fiber composites , 2009 .

[20]  Ron Barrett,et al.  Missile flight control using active flexspar actuators , 1995, Smart Structures.

[21]  Victor Giurgiutiu,et al.  Review of Smart-Materials Actuation Solutions for Aeroelastic and Vibration Control , 2000 .

[22]  Osgar John Ohanian,et al.  Piezoelectric Morphing versus Servo-Actuated MAV Control Surfaces , 2012 .

[23]  Daniel J. Inman,et al.  Macro-Fiber Composite actuated simply supported thin airfoils , 2010 .