<?xml version="1.0" encoding="UTF-8"?><ns2:project xmlns:ns1="http://gtr.rcuk.ac.uk/gtr/api" xmlns:ns2="http://gtr.rcuk.ac.uk/gtr/api/project" xmlns:ns3="http://gtr.rcuk.ac.uk/gtr/api/fund" xmlns:ns4="http://gtr.rcuk.ac.uk/gtr/api/person" xmlns:ns5="http://gtr.rcuk.ac.uk/gtr/api/project/outcome" xmlns:ns6="http://gtr.rcuk.ac.uk/gtr/api/organisation" ns1:created="2026-06-03T15:52:43Z" ns1:href="http://gtr.ukri.org/gtr/api/projects/C78EA8D2-E9DD-4EFD-9529-3C41D6D2C4D6" ns1:id="C78EA8D2-E9DD-4EFD-9529-3C41D6D2C4D6"><ns1:links><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/7BD7D0DA-C696-489D-8751-A4B3272A4765" ns1:rel="LEAD_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/AF5A1541-D454-4E94-8117-8C5254C79ED2" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/D9E2F69B-E694-49DC-B660-E0AA6C7A28E8" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/15B9E8A6-BB18-48B9-A6A6-C6A17D568414" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/7BD7D0DA-C696-489D-8751-A4B3272A4765" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/B3D759FF-F1BF-4184-A582-944EA26ADDB7" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:end="2013-10-31T00:00:00Z" ns1:href="http://gtr.ukri.org/gtr/api/funds/4F1E59E8-7771-4FCA-A5A5-06628C98EAD8" ns1:rel="FUND" ns1:start="2009-11-01T00:00:00Z"/></ns1:links><ns2:identifiers><ns2:identifier ns2:type="RCUK">110030</ns2:identifier></ns2:identifiers><ns2:title>SILOET Project 1 - Fan System</ns2:title><ns2:status>Closed</ns2:status><ns2:grantCategory>BEIS-Funded Programmes</ns2:grantCategory><ns2:leadFunder>Innovate UK</ns2:leadFunder><ns2:abstractText>The Strategic Investment in Low Carbon Engine Technologies (SILOET) Project 1 was conceived by Rolls-Royce and its partners to deliver light weight, robust and reliable and fuel efficient Fan technologies. The Project aims to develop and validate these in a Light Weight Fan System. As engine cycles move to lower specific thrust to reduce fuel burn and CO2, fans tend to become larger for a given thrust and, therefore, the fan system’s weight must be reduced or else the fuel burn advantage is lost. This project, therefore, has 3 main parts – fan aero-acoustics and flutter; blade reinforcement and composite casing.</ns2:abstractText></ns2:project>