Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan
This study presents a feasibility study for an induction motor rim drive to power aircraft boundary-layer-ingestion (BLI) fans. The design is developed from a BLI-fan specification for traditional aircraft architecture: the rotor is fastened to the rim of the blade shroud, not to obstruct the fan du...
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Online Access: | https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8044 |
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doaj-18fdf4725b56468db6f2dbc382c0a47a2021-04-02T17:39:58ZengWileyThe Journal of Engineering2051-33052019-04-0110.1049/joe.2018.8044JOE.2018.8044Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fanAlexander C. Smith0Matteo F. Iacchetti1Paul M. Tuohy2School of Electrical and Electronic Engineering, The University of ManchesterSchool of Electrical and Electronic Engineering, The University of ManchesterSchool of Electrical and Electronic Engineering, The University of ManchesterThis study presents a feasibility study for an induction motor rim drive to power aircraft boundary-layer-ingestion (BLI) fans. The design is developed from a BLI-fan specification for traditional aircraft architecture: the rotor is fastened to the rim of the blade shroud, not to obstruct the fan duct and interfere with the air flow. The main objective of this study is the identification of achievable power density and efficiency levels with an induction motor rim drive configuration considering the structural requirements for the integrity of the rotor operating with high tip speeds. The proposed 250 kW, 14,000 rpm design example achieves an efficiency in excess of 97% with an active mass around 20 kg.https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8044aerospace propulsionductsdesign engineeringboundary layersfansrotorsbladesaircraftsuperconducting machinesaerodynamicsfeasibility studypower aircraft boundary-layer-ingestion fansBLI-fan specificationtraditional aircraft architecturefan ductachievable power densityinduction motor rim drive configurationaircraft boundary-layer-ingestion fanpower 250.0 kWmass 20.0 kg |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Alexander C. Smith Matteo F. Iacchetti Paul M. Tuohy |
spellingShingle |
Alexander C. Smith Matteo F. Iacchetti Paul M. Tuohy Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan The Journal of Engineering aerospace propulsion ducts design engineering boundary layers fans rotors blades aircraft superconducting machines aerodynamics feasibility study power aircraft boundary-layer-ingestion fans BLI-fan specification traditional aircraft architecture fan duct achievable power density induction motor rim drive configuration aircraft boundary-layer-ingestion fan power 250.0 kW mass 20.0 kg |
author_facet |
Alexander C. Smith Matteo F. Iacchetti Paul M. Tuohy |
author_sort |
Alexander C. Smith |
title |
Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan |
title_short |
Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan |
title_full |
Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan |
title_fullStr |
Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan |
title_full_unstemmed |
Feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan |
title_sort |
feasibility study of an induction motor rim drive for an aircraft boundary-layer-ingestion fan |
publisher |
Wiley |
series |
The Journal of Engineering |
issn |
2051-3305 |
publishDate |
2019-04-01 |
description |
This study presents a feasibility study for an induction motor rim drive to power aircraft boundary-layer-ingestion (BLI) fans. The design is developed from a BLI-fan specification for traditional aircraft architecture: the rotor is fastened to the rim of the blade shroud, not to obstruct the fan duct and interfere with the air flow. The main objective of this study is the identification of achievable power density and efficiency levels with an induction motor rim drive configuration considering the structural requirements for the integrity of the rotor operating with high tip speeds. The proposed 250 kW, 14,000 rpm design example achieves an efficiency in excess of 97% with an active mass around 20 kg. |
topic |
aerospace propulsion ducts design engineering boundary layers fans rotors blades aircraft superconducting machines aerodynamics feasibility study power aircraft boundary-layer-ingestion fans BLI-fan specification traditional aircraft architecture fan duct achievable power density induction motor rim drive configuration aircraft boundary-layer-ingestion fan power 250.0 kW mass 20.0 kg |
url |
https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8044 |
work_keys_str_mv |
AT alexandercsmith feasibilitystudyofaninductionmotorrimdriveforanaircraftboundarylayeringestionfan AT matteofiacchetti feasibilitystudyofaninductionmotorrimdriveforanaircraftboundarylayeringestionfan AT paulmtuohy feasibilitystudyofaninductionmotorrimdriveforanaircraftboundarylayeringestionfan |
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1721553551340077056 |