Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/33054
Full metadata record
DC FieldValueLanguage
dc.contributor.authorShamekhi Amiri, S-
dc.contributor.authorAl-Zaili, J-
dc.contributor.authorSayma, AI-
dc.date.accessioned2026-03-28T11:20:25Z-
dc.date.available2026-03-28T11:20:25Z-
dc.date.issued2026-02-27-
dc.identifierORCiD: Jafar Al-Zaili https://orcid.org/0000-0003-4072-2107-
dc.identifierORCiD: Abdulnaser I. Sayma https://orcid.org/0000-0003-2315-0004-
dc.identifier.citationShamekhi Amiri, S., Al-Zaili, J. and Sayma, A.I. (2026) 'Development and Validation of a Transient Electro-Thermo- Mechanical Model for Parabolic Dish Micro Gas Turbines', Energies, 19 (5), 1188, pp. 1–28. doi: 10.3390/en19051188.en-US
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/33054-
dc.descriptionData Availability Statement: The original contributions presented in this study are included in the article. Further inquiries can be directed to the corresponding author.en-US
dc.description.abstractSmall-scale concentrated solar power (CSP) systems coupled with micro gas turbines (MGTs) offer a promising solution for decentralised and sustainable power generation. However, CSP–MGT systems are subject to pronounced transient behaviour during start-up and operation due to fluctuating solar irradiance, making accurate transient modelling essential. This work introduces a fully coupled transient electro-thermo-mechanical model of a CSP-driven micro gas turbine, explicitly linking thermal transients and heat soakage effects to electrical performance during start-up. Unlike existing models, the proposed approach captures the interaction between turbomachinery thermal inertia, shaft dynamics, and detailed electrical machine and power converter losses under real-world transient operating conditions. The model integrates thermodynamic, mechanical, electrical, and control subsystems within a unified framework using a lumped-volume formulation suitable for real-time-capable simulations. To improve prediction accuracy at low rotational speeds, a dedicated interpolation strategy for turbomachinery performance maps is implemented. The model is validated at both component and system levels using experimental data from a 6 kWe CSP–MGT test facility. The results show good agreement with measurements, with maximum deviations of approximately 8% in receiver outlet temperature and less than 6% in air mass flow rate. The findings demonstrate that accounting for heat soakage is critical for a realistic prediction of thermal and electrical transients, as neglecting thermal inertia leads to an underestimation of the start-up electrical energy consumption by up to 140%, highlighting the dominant role of thermal mass effects in small-scale micro gas turbines compared to larger systems. The proposed model provides a robust tool for analysing start-up behaviour and supports improved control and operational strategy development for CSP–MGT systems under variable solar conditions.en-US
dc.description.sponsorshipThis research received no external funding.en-US
dc.format.extent1–28-
dc.format.mediumElectronic-
dc.languageen-USen-US
dc.language.isoenen-US
dc.publisherMDPIen-US
dc.rightsCreative Commons Attribution 4.0 International-
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/-
dc.subjectmicro gas turbineen-US
dc.subjectconcentrated solar power systemen-US
dc.subjecttransient modellingen-US
dc.subjectelectro-thermo-mechanical modelen-US
dc.subjectstart-up phaseen-US
dc.subjectheat soakageen-US
dc.titleDevelopment and Validation of a Transient Electro-Thermo- Mechanical Model for Parabolic Dish Micro Gas Turbinesen-US
dc.typeArticleen-US
dc.date.dateAccepted2026-02-08-
dc.identifier.doihttps://doi.org/10.3390/en19051188-
dc.relation.isPartOfEnergies-
pubs.issue5-
pubs.publication-statusPublished online-
pubs.volume19-
dc.identifier.eissn1996-1073-
dc.rights.licensehttps://creativecommons.org/licenses/by/4.0/legalcode.en-
dcterms.dateAccepted2026-02-08-
dc.rights.holderThe authors-
dc.contributor.orcidAl-Zaili, Jafar [0000-0003-4072-2107]-
dc.contributor.orcidSayma, Abdulnaser I. [0000-0003-2315-0004]-
dc.identifier.number1188-
Appears in Collections:Department of Mechanical and Aerospace Engineering Research Papers

Files in This Item:
File Description SizeFormat 
FullText.pdfCopyright © 2026 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/).3.12 MBAdobe PDFView/Open


This item is licensed under a Creative Commons License Creative Commons