A novel methodology for macroscale, thermal characterization of carbon fiber-reinforced polymer for integrated aircraft electrical power systems
Jones, Catherine E. and Hamilton, Andrew W. and Norman, Patrick J. and Cleary, Alison and Galloway, Stuart J. and Atkinson, Robert and Burt, Graeme M. and Michie, Craig and Andonovic, Ivan and Tachtatzis, Christos (2019) A novel methodology for macroscale, thermal characterization of carbon fiber-reinforced polymer for integrated aircraft electrical power systems. IEEE Transactions on Transportation Electrification, 5 (2). pp. 479-489. ISSN 2332-7782 (https://doi.org/10.1109/TTE.2019.2914890)
Preview |
Text.
Filename: Jones_etal_TTE2019_A_novel_methodology_for_macro_scale_thermal_characterisation_of_carbon_fibre.pdf
Accepted Author Manuscript Download (1MB)| Preview |
Abstract
Carbon fiber-reinforced polymer (CFRP) is increasingly used for aero-structure applications due to their high strength-to-weight ratio. The integration of the on-board electrical power system (EPS) with CFRP is challenging due to the requirement to thermally and electrically isolate these systems to meet existing safety standards. By capturing the thermal characteristics of CFRP at a macro (component) scale for CFRP components, it is possible to understand, and design for, the increased integration of the EPS into CFRP aero-components. A significant challenge is to develop a macroscale characterization of CFRP, which is not only of an appropriate fidelity for compatibility with systems-level models of an EPS but also can be used to represent different geometries of CFRP components. This paper presents a novel methodology for capturing a transient, macroscale thermal characterization of CFRP with regard to component layup and geometry (thickness). The methodology uses experimentally derived thermal responses of specific resin and ply orientation CFRP samples to create a generalized relationship for the prediction of thermal transfer in other sample thicknesses of the same material type. This methodology can be used to characterize thermal gradients across CFRP components in aircraft EPS integration applications, ultimately informing the optimized integration of the EPS with CFRP.
ORCID iDs
Jones, Catherine E. ORCID: https://orcid.org/0000-0001-7524-5756, Hamilton, Andrew W. ORCID: https://orcid.org/0000-0002-8436-8325, Norman, Patrick J. ORCID: https://orcid.org/0000-0001-5577-1281, Cleary, Alison ORCID: https://orcid.org/0000-0002-3717-9812, Galloway, Stuart J. ORCID: https://orcid.org/0000-0003-1978-993X, Atkinson, Robert ORCID: https://orcid.org/0000-0002-6206-2229, Burt, Graeme M. ORCID: https://orcid.org/0000-0002-0315-5919, Michie, Craig ORCID: https://orcid.org/0000-0001-5132-4572, Andonovic, Ivan ORCID: https://orcid.org/0000-0001-9093-5245 and Tachtatzis, Christos ORCID: https://orcid.org/0000-0001-9150-6805;-
-
Item type: Article ID code: 67752 Dates: DateEvent30 June 2019Published6 May 2019Published Online19 April 2019AcceptedNotes: © 2019 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. Subjects: Technology > Electrical engineering. Electronics Nuclear engineering Department: Faculty of Engineering > Electronic and Electrical Engineering
Strategic Research Themes > Measurement Science and Enabling TechnologiesDepositing user: Pure Administrator Date deposited: 09 May 2019 13:24 Last modified: 11 Nov 2024 12:17 URI: https://strathprints.strath.ac.uk/id/eprint/67752