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Energy Harvesting from Landing and Taxiing of Commercial Aircraft
Journal Article
01-15-01-0004
ISSN: 1946-3855, e-ISSN: 1946-3901
Sector:
Topic:
Citation:
Brown, E. and Zaidi, Y., "Energy Harvesting from Landing and Taxiing of Commercial Aircraft," SAE Int. J. Aerosp. 15(1):57-74, 2022, https://doi.org/10.4271/01-15-01-0004.
Language:
English
Abstract:
We demonstrate a virtual proof-of-concept design and experiment for energy
harvesting enabling economic and environment-friendly aircraft by recycling
forces for power conversion. The harvesting uses piezoelectric materials for
extracting energy from the impact at the touchdown during the landing of an
aircraft and direct current (DC) generators powered by the rotational motion of
the aircraft wheels during taxiing. The design begins with a multidomain model
comprising multibody dynamics, mathematical descriptions, abstract behavioral
blocks, and programmed code. Piezoelectric harvesting explores six types of
materials consisting of ring and disk pad geometries. Both geometries are
typical configurations in suspension systems. Recent advances have shown the
potential of getting higher voltage out of new materials properties. Our
objective is to determine the useful impact force during a touchdown on the pads
and a pad type that maximizes the power transfer. The evaluation shows that the
American Piezo Ceramics (APC) 860/porous material in the ring shape gives the
maximum power. For constant power generation during taxiing, we analyze four
configurations of the DC generator. The DC generation offers a rich system-level
design trade-off in evaluating a steady output voltage as the generator spins
cyclically and changes flux in the coil during the contact between the wheel and
the runway. The methodology for harvesting energy through touchdown and taxiing
is agile to experiment with loads and their release heights for evaluating other
piezoelectric materials for their potential for generating power as well as for
the parametric tradespace analysis in generator performance.