Resumo:
Structural Health Monitoring (SHM) is an essential strategy for ensuring the safety and
longevity of critical infrastructure and advanced composite structures. While embedded
sensors offer a transformative approach to real-time monitoring by enabling in-situ damage
detection, their widespread adoption is hindered by challenges at the sensor-material
interface, unoptimized geometric designs, and a critical lack of system-level validation
in complex load-bearing components. This thesis presents a comprehensive ”Experiment-
Model-Optimize-Validate” framework for the development, optimization, and system-level
integration of additively manufactured piezoresistive strain sensors. Through a systematic
review of the state-of-the-art, the predominance of carbon-based piezoresistive sensors
manufactured via Fused Deposition Modeling (FDM) was established, alongside the critical
need to balance sensor sensitivity with the mechanical integrity of the host structure.
To address this inherent trade-off, a rigorous computational and experimental methodology
was developed. A Design of Experiments (DoE) evaluated the influence of geometric
parameters (trace width, inter-trace distance, thickness, and end-loops) on sensor performance.
Utilizing Gaussian Process Regression (GPR) and a Multi-Objective Particle
Swarm Optimization (MOPSO) algorithm, optimal geometries were identified. Experimental
validation demonstrated that fully embedded configurations achieved exceptional
piezoresistive sensitivity (Gauge Factor ≈ 59), while a geometrically scaled variant successfully
restored the host structure’s stiffness to near-native levels (≈ 2.18 GPa) without
significant loss of sensitivity. To bridge the gap between laboratory-scale coupon testing
and field-ready deployment, the optimized sensing architectures were integrated into
a geometrically complex aerospace pylon structure using multi-material FDM. Sensor
placement was strategically guided by Finite Element Analysis (FEA) to target critical
strain hotspots, and a redundant sensing network was implemented to ensure fault
tolerance. System-level testing, validated by full-field Digital Image Correlation (DIC),
proved that the embedded sensors exhibited high-fidelity temporal synchronization with
mechanical deformation, capturing transient structural events with negligible viscoelastic
lag. Furthermore, the redundant architecture successfully maintained monitoring capabilities
and diagnosed asymmetrical loading anomalies. Ultimately, this research provides a
highly scalable and robust methodology for transitioning 3D-printed embedded sensors
from isolated component optimization to integrated, self-sensing structural systems, advancing
the technological readiness of real-time SHM in aerospace and civil engineering
applications.