In the United States, many civil, aerospace, and military aircraft are nearing the end of their service life. Many of these service life predictions were determined by models that were created at the time of the design of the structure, possibly decades ago. As a precaution, these structures are inspected on a regular basis with techniques that tend to be expensive and laborious, such as tear-down inspections of aircraft. To complicate matters, new complex materials have been incorporated in recent structures to take advantage of their desirable properties, but these materials sustain damage in a manner that is different from that of past monolithic materials. One example is fiber-reinforced polymer (FRP) composites, which are heterogeneous, direction-dependent, and tend to manifest damage internal to their laminate structure, thus making the detection of this damage nearly impossible. For these reasons, numerous groups have focused on developing sensors that can be applied to or embedded within these structures to detect this damage. Some of the most promising of these approaches include using piezoelectric materials as passive or active ultrasonic sensors and actuators, fiber optic-based sensors to measure strain and detect cracking, and carbon nanotube-based sensors that can detect strain and cracking. These are mostly point-based sensors that are accurate at the location of application but require interpolative methods to ascertain the structural health elsewhere on the structure. To conduct direct damage detection across a structure, we have coupled the ability to deposit a carbon nanotube thin film across large substrates with a spatially distributed electrical conductivity measurement methodology called electrical impedance tomography. As indicated by previous research on carbon nanotube thin films, the electrical conductivity of these films changes when subjected to strain or become damaged. Our structural health monitoring strategy involves monitoring for changes in electrical conductivity across an applied CNT thin film, which would indicate damage. In this work, we demonstrate the ability of the Electrical Impedance Tomography (EIT) methodology to detect, locate, size, and determine severity of damage from impact events subjected to glass fiber-reinforced polymer composites. This will demonstrate the value and effectiveness of this next-generation structural health monitoring approach.
Skip Nav Destination
ASME 2013 Conference on Smart Materials, Adaptive Structures and Intelligent Systems
September 16–18, 2013
Snowbird, Utah, USA
Conference Sponsors:
- Aerospace Division
ISBN:
978-0-7918-5604-8
PROCEEDINGS PAPER
Evaluation of the Damage Detection Characteristics of Electrical Impedance Tomography
Bryan R. Loyola,
Bryan R. Loyola
Sandia National Laboratories, Livermore, CA
Search for other works by this author on:
Luciana Arronche,
Luciana Arronche
University of California, Davis, Davis, CA
Search for other works by this author on:
Marianne LaFord,
Marianne LaFord
Sandia National Laboratories, Livermore, CA
Search for other works by this author on:
Valeria La Saponara,
Valeria La Saponara
University of California, Davis, Davis, CA
Search for other works by this author on:
Kenneth J. Loh
Kenneth J. Loh
University of California, Davis, Davis, CA
Search for other works by this author on:
Bryan R. Loyola
Sandia National Laboratories, Livermore, CA
Luciana Arronche
University of California, Davis, Davis, CA
Marianne LaFord
Sandia National Laboratories, Livermore, CA
Valeria La Saponara
University of California, Davis, Davis, CA
Kenneth J. Loh
University of California, Davis, Davis, CA
Paper No:
SMASIS2013-3317, V002T05A017; 8 pages
Published Online:
February 20, 2014
Citation
Loyola, BR, Arronche, L, LaFord, M, La Saponara, V, & Loh, KJ. "Evaluation of the Damage Detection Characteristics of Electrical Impedance Tomography." Proceedings of the ASME 2013 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. Volume 2: Mechanics and Behavior of Active Materials; Structural Health Monitoring; Bioinspired Smart Materials and Systems; Energy Harvesting. Snowbird, Utah, USA. September 16–18, 2013. V002T05A017. ASME. https://doi.org/10.1115/SMASIS2013-3317
Download citation file:
17
Views
Related Proceedings Papers
Related Articles
Structural Health Monitoring of Glass/Epoxy Composite Plates Using PZT and PMN-PT Transducers
J. Eng. Mater. Technol (January,2011)
Influence of Thermal Gradients and Arctic Temperatures on the Mechanical Properties and Fracture Behavior of Woven Carbon and Woven Kevlar ® Composites
ASME Open J. Engineering (January,2024)
Flexural Fatigue of Unbalanced Glass-Carbon Hybrid Composites
J. Sol. Energy Eng (November,2014)
Related Chapters
Layer Arrangement Impact on the Electromechanical Performance of a Five-Layer Multifunctional Smart Sandwich Plate
Advanced Multifunctional Lightweight Aerostructures: Design, Development, and Implementation
Introduction
Computer Vision for Structural Dynamics and Health Monitoring
Digital Transformation by the Implementation of the True Digital Twin Concept and Big Data Technology for Structural Integrity Management
Ageing and Life Extension of Offshore Facilities