4.5 Article

Electromagnetic Energy Harvester for Vibration Control of Space Rack: Modeling, Optimization, and Analysis

Journal

JOURNAL OF AEROSPACE ENGINEERING
Volume 32, Issue 1, Pages -

Publisher

ASCE-AMER SOC CIVIL ENGINEERS
DOI: 10.1061/(ASCE)AS.1943-5525.0000955

Keywords

Vibration control; Energy harvesting; Space structure; Genetic algorithm

Funding

  1. National Natural Science Foundation of China [11602223]
  2. Open Research Fund of the Key Laboratory of Space Utilization, Chinese Academy of Sciences [LSU-2016-01-01]
  3. State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi'an Jiaotong University [SV2016-KF-14]
  4. Young Researchers Foundation of Zhejiang Provincial Top Key Academic Discipline of Mechanical Engineering of Zhejiang Sci-Tech University [ZSTU-ME02B04]
  5. Fundamental Research Funds for the Central Universities of China [G2018KY0306]

Ask authors/readers for more resources

A space rack suffers from shock and broadband random loads during shipment and launch, which may lead to irreversible damage until the spacecraft reaches final orbit. This paper presents a novel dual-functional electromagnetic energy harvester (DF-EEH) that is regarded as an electrically tuned mass damper (TMD) to simultaneously suppress vibration and harvest energy. The equal modal damping method is proposed to optimize parameters of the DF-EEH. Furthermore, a resonant circuit is utilized to improve the energy harvesting performance and vibration suppression efficiency of the space rack. Genetic algorithm (GA) is used to optimize tuning frequencies and damping ratios of the DF-EEH with the resonant circuit. For the DF-EEH with both the resistor and resonant circuit, the response of the space rack is reduced to 9.29, and the harvested energy is 0.41W/N. Therefore, this research can provide a novel vibration control and sustainable-energy supplement concept for the low-power-consumption electronic devices of space structures. (C) 2018 American Society of Civil Engineers.

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