Vibrational energy harvesting devices are a possible solution to provide adequate power for structural health monitoring by taking ambient vibrations and converting them into usable electric power. This work aims to quantify critical single crystal energy harvester design parameters by investigating lead magnesium niobate-lead titanate (PMN-PT) single crystal devices in long-duration, high-temperature, and high acceleration environments typical of rotorcraft applications, expanding the environmental parameters from current literature, and comparing them to conventional lead zirconite titanate (PZT) ceramics. The harvesters proved to be a reliable source of power generation and are practical for harvesting usage. The work also provides new data by expanding upon current test data sets by including device damping and scalability studies and by developing and testing a compact energy harvester more representative of true flight hardware. A laboratory test article produced 25 V RMS at 1.0 g base acceleration at room temperature and was stable for 120 h of continuous use. Its performance exhibited strong temperature dependence, which was lessened by using different material compositions. The output power of a prototype, 40-g compact harvester surpassed that of PZT devices and was sufficient for low-power sensors. At 1.0 g and room temperature, the single crystal harvester produced approximately three times the power of a PZT device. A scalability study was conducted to compare size and mass of a prototype compact device for use at a range of frequencies of interest, which showed the harvester is easily scaled with minimal design changes.
Nomenclature
Cpiezoelectric material capacitance, F d piezoelectric charge coefficient, C/N or m/V k piezoelectric coupling factor, dimensionless t piezoelectric material thickness, m tan δ piezoelectric loss factor, % Y Young's modulus, Pa δ normal strain in the x direction, m/m ε piezoelectric permittivity, dimensionless ζ mechanical system damping ratio, dimensionless ω harvester resonance frequency, rad/s wiring and all associated components are often of concern. Because of this, wireless sensor solutions along with new power options for SHM problems are desired. The major component under consideration in this study is the power supply. Currently, onboard systems have to rely mainly on batteries or similar sources for power. Unfortunately, batteries have a finite lifetime and may be placed in areas that are extremely difficult to reach, or that require some disassembly to replace or recharge (Refs. 1-3). Harvesting ambient energy from surroundings is an area of interest in the SHM world that aims to solve this problem. Energy can come in many forms, including electromagnetic, acoustic, thermal, and vibrational (Ref. 4). Different harvesting techniques require different host structure environments. The output of thermal harvesters depends on device size and available thermal gradients. Vibrational harvester output depends on the frequency and amplitude of the base excitation. The f...