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Greener Aviation with Advanced Propulsion Systems (GAAPS)

Reference Number
EP/W010119/1
Title
Greener Aviation with Advanced Propulsion Systems (GAAPS)
Status
Completed
Energy Categories
Energy Efficiency(Transport)
Not Energy Related
Research Types
Basic and strategic applied research
Applied Research and Development
Science and Technology Fields
ENGINEERING AND TECHNOLOGY (Mechanical, Aeronautical and Manufacturing Engineering)
UKERC Cross Cutting Characterisation
Not Cross-cutting
Principal Investigator
Dr A Filippone
Mechanical, Aerospace and Civil Engineering
University of Manchester
Award Type
Standard
Funding Source
EPSRC
Start Date
01 October 2022
End Date
31 March 2026
Duration
42 months
Total Grant Value
£1,750,240
Industrial Sectors
Design
Region
North West
Programme
Manufacturing and the Circular Economy
Investigators
Principal Investigator
Dr A Filippone, Mechanical, Aerospace and Civil Engineering, University of Manchester
Other Investigator
Professor G Barakos, Aerospace Engineering, University of Glasgow
Dr N Bojdo, Mechanical, Aerospace and Civil Engineering, University of Manchester
Dr W Crowther, Mechanical, Aerospace and Civil Engineering, University of Manchester
Dr R Green, Aerospace Engineering, University of Glasgow
Mr K Kabbabe, Mechanical, Aerospace and Civil Engineering, University of Manchester
Dr R Steijl, College of Science and Engineering, University of Glasgow
Industrial Collaborator
Project Contact, Rolls-Royce PLC
Project Contact, DSTL - Defence Science and Technology Laboratory
Web Site
Objectives
Abstract
A number of novel aircraft configurations is likely to be developed in the next decade. These new aircraft will rely almost exclusively on advanced propellers, because they address flight conditions that are not viable with conventional gas turbine engines. First, there are issues of scaling, as the new vehicles target sub-scale (unmanned) to full scale (manned transport). Second, there are opportunities with hybrid or fully electric propulsions, which scale well at the low power outputs, but require variable-speed propellers. Propellers currently used in aviation operate at constant rpm and are fully reversible. The new propellers addressed in this research operate over a wide range of rpm and are mostly non-reversible (fixed-pitch). Thus, the strategic aims of the proposal is to build understanding of these new propeller systems, to create a database of experimental data that do not depend on a specific flight platform and can be used for further development in the industry. The proposal targets a mix of design, simulation models, advanced manufacturing, wind tunnel testing, open-air flight testing, and builds on several years of experience with rotary-wing systems
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Added to Database
14/07/22