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Lightweight Innovative Generator for Future Air Transportation

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€599 870
EU Contribution
€599 870
Project website
Project Acronym
LIFT
STRIA Roadmaps
Transport electrification (ELT)
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Other specified
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP07-2017-02
Link to CORDIS
Background & Policy context

LIFT will deliver a beyond state-of-the-art solution for lightweight non-active components for a megawatt range electrical machine proposed for Clean Sky 2 Large Passenger Aircraft IADP work package 1.6.1 as defined in the Topic Description JTI-CS2-2017-CfP07-01-4.

As stated in the Topic Description, the non-active parts of electrical machines contribute to 30-40% of the weight of the machine. LIFT proposes a number of solutions to reduce the mass and the weight of these non-active parts ranging from using composites or metal foams to corrugated structures that are all within the expertise of the University of Nottingham. In total, our preliminary workings illustrate that it is possible to deliver a mass and weight saving of at least 50% using a combination of technologies without significantly diminishing performance.

Objectives

As a result of the research and innovation activities within the project, UNOTT foresees the generation of new knowledge in the following areas:

  • An innovative MW-class generator with a record power density in excess of 25kW/kg will be developed
  • Innovative thermal management systems will be developed exploiting the voids within lightweight materials
  • A new family of lower-noise e-machines will be incepted, taking advantage of the voids within lightweight materials
  • Development of novel mechanical models and advanced manufacturing methods for cylindrical lattice materials as required for e-machine designs, backed up by experimental testing
  • The power density boundaries and limitations charts for future aerospace PM machines will be established for different speeds

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.1.
Other Programme
JTI-CS2-2017-CfP07-LPA-01-41 Advanced manufacturing for MW range power dense electrical machines for aerospace applications

Partners

Lead Organisation
Organisation
The University Of Nottingham
Address
University Park, Nottingham, NG7 2RD, United Kingdom
EU Contribution
€599 870
Partner Organisations
Organisation
N/a
Address
United Kingdom
EU Contribution
€0

Technologies

Technology Theme
Composite materials
Technology
Composite materials for structural purposes in the aircraft
Development phase
Research/Invention

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