Oil-cooled thermoelectric energy harvesting for aero-engine sensing system
Oil-cooled thermoelectric energy harvesting for aero-engine sensing system
To enhance the performance and reliability of aircraft propulsion systems, an integrated bearing condition monitoring system is proposed. This intelligent bearing must have advanced health management capabilities to provide early warning of problems. In most commercial high-temperature applications, the sensing system is located externally due to lack of appropriate electronic devices that can function at high temperature. This paper presents the design and implementation of a self-powered sensing system for use in a high-temperature aircraft environment. The performance of the thermoelectric generator and energy availability to process acceleration data is shown from our laboratory tests based on realistic operating conditions.
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Zaghari, Bahareh
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Bashir, Imran
e7bed382-cefa-4a4b-a2e2-253ef98a963a
Weddell, Alexander
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White, Neil
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Harvey, Terry J.
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Wang, Ling
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10 December 2018
Zaghari, Bahareh
a0537db6-0dce-49a2-8103-0f4599ab5f6a
Bashir, Imran
e7bed382-cefa-4a4b-a2e2-253ef98a963a
Weddell, Alexander
3d8c4d63-19b1-4072-a779-84d487fd6f03
White, Neil
c7be4c26-e419-4e5c-9420-09fc02e2ac9c
Harvey, Terry J.
3b94322b-18da-4de8-b1af-56d202677e04
Wang, Ling
c50767b1-7474-4094-9b06-4fe64e9fe362
Zaghari, Bahareh, Bashir, Imran, Weddell, Alexander, White, Neil, Harvey, Terry J. and Wang, Ling
(2018)
Oil-cooled thermoelectric energy harvesting for aero-engine sensing system.
Proceedings, 2 (13), , [965].
(doi:10.3390/proceedings2130965).
Abstract
To enhance the performance and reliability of aircraft propulsion systems, an integrated bearing condition monitoring system is proposed. This intelligent bearing must have advanced health management capabilities to provide early warning of problems. In most commercial high-temperature applications, the sensing system is located externally due to lack of appropriate electronic devices that can function at high temperature. This paper presents the design and implementation of a self-powered sensing system for use in a high-temperature aircraft environment. The performance of the thermoelectric generator and energy availability to process acceleration data is shown from our laboratory tests based on realistic operating conditions.
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Oil-cooled thermoelectric energy harvesting for aero-engine sensing system
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Oil-cooled thermoelectric energy harvesting Euro Sensors 2018
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Accepted/In Press date: 1 June 2018
e-pub ahead of print date: 10 September 2018
Published date: 10 December 2018
Additional Information:
This publication is from I2BS project funded by “Clean Sky 2 Joint Undertaking”, “European Union (EU)” and “Horizon 2020”. The name of the action is ‘IA’, the acronym is I2BS and grant number is 717174. Proceedings of Eurosensors 2018. Presented at the Eurosensors 2018 Conference, Graz, Austria, 9–12 September 2018.
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Eurosensors 2018, , Graz, Austria, 2018-09-09 - 2018-09-12
Identifiers
Local EPrints ID: 423201
URI: http://eprints.soton.ac.uk/id/eprint/423201
ISSN: 2504-3900
PURE UUID: 5363d1f2-9f42-4c06-8a3e-aabbedcca035
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Date deposited: 19 Sep 2018 16:30
Last modified: 21 Sep 2024 01:54
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