Compressor degradation management strategies for gas turbine aero-engine controller design

Show simple item record

dc.contributor.author Sun, Xiaohuan
dc.contributor.author Jafari, Soheil
dc.contributor.author Fashandi, Seyed Alireza Miran
dc.contributor.author Nikolaidis, Theoklis
dc.date.accessioned 2021-09-14T10:31:55Z
dc.date.available 2021-09-14T10:31:55Z
dc.date.issued 2021-09-10
dc.identifier.citation Sun X, Jafari S, Fashandi SAM, Nikolaidis T. (2021) Compressor degradation management strategies for gas turbine aero-engine controller design. Energies, Volume 14, Issue 18, September 2021, Article number 5711 en_UK
dc.identifier.issn 1996-1073
dc.identifier.uri https://doi.org/10.3390/en14185711
dc.identifier.uri https://dspace.lib.cranfield.ac.uk/handle/1826/17075
dc.description.abstract The Advisory Council for Aeronautics Research in Europe (ACARE) Flight Path 2050 focuses on ambitious and severe targets for the next generation of air travel systems (e.g., 75% reduction in CO2 emissions per passenger kilometre, a 90% reduction in NOx emissions, and a 65% reduction in the noise emissions of flying aircraft relative to the capabilities of typical new aircraft in 2000). Degradation is an inevitable phenomenon as aero-engines age with significant impacts on the engine performance, emissions level, and fuel consumption. The engine control system is a key element capable of coping with degradation consequences subject to the implementation of an advanced management strategy. This paper demonstrates a methodological approach for aero-engine controller adjustment to deal with degradation implications, such as emission levels and increased fuel consumption. For this purpose, a component level model for an aero-engine was first built and transformed to a block-structured Wiener model using a system identification approach. An industrial Min-Max control strategy was then developed to satisfy the steady state and transient limit protection requirements simultaneously while satisfying the physical limitation control modes, such as over-speed, surge, and over-temperature. Next, the effects of degradation on the engine performance and associated changes to the controller were analysed thoroughly to propose practical degradation management strategies based on a comprehensive scientometric analysis of the topic. The simulation results show that the proposed strategy was effective in restoring the degraded engine performance to the level of the clean engine while protecting the engine from physical limitations. The proposed adjustments in the control strategy reduced the fuel consumption and, as a result, the emission level and carbon footprint of the engine. en_UK
dc.language.iso en en_UK
dc.publisher MDPI en_UK
dc.rights Attribution 4.0 International *
dc.rights.uri http://creativecommons.org/licenses/by/4.0/ *
dc.subject environmental considerations en_UK
dc.subject flight path 2050 en_UK
dc.subject emissions level reduction en_UK
dc.subject aero-engines control en_UK
dc.subject degradation management strategy en_UK
dc.title Compressor degradation management strategies for gas turbine aero-engine controller design en_UK
dc.type Article en_UK


Files in this item

The following license files are associated with this item:

This item appears in the following Collection(s)

Show simple item record

Attribution 4.0 International Except where otherwise noted, this item's license is described as Attribution 4.0 International

Search CERES


Browse

My Account

Statistics