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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Main Authors: Alexander C. Smith, Matteo F. Iacchetti, Paul M. Tuohy
Format: Article
Language:English
Published: Wiley 2019-04-01
Series:The Journal of Engineering
Subjects:
Online Access:https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8044
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spelling 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
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AT paulmtuohy feasibilitystudyofaninductionmotorrimdriveforanaircraftboundarylayeringestionfan
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