SILOET II Project 14 Aero-mechanically Optimised Composite Fan System

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Title
SILOET II Project 14 Aero-mechanically Optimised Composite Fan System

CoPED ID
f8b7e930-667f-4f31-add8-8edb3ea3aad4

Status
Closed


Value
£16,799,808

Start Date
Jan. 1, 2014

End Date
March 30, 2017

Description

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Aircraft in service are forecasted to double next 20 years with approximately 30,000 new aircraft. To minimise their environment impact a sustained improvement in the efficiency of gas turbine engines is required. For aerospace, the Advisory Council on Aeronautics Research and Innovation in Europe (ACARE), has defined long term challenging competitiveness and environmental goals for the aviation industry. This, together with the airline operators’ requirement for extended time periods between overhauls, requires the introduction of step change technologies. 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 programme is aimed at introducing a carbon fibre composite fan system on to next generation Rolls-Royce engines. As a lightweight material with high resistance to fatigue, carbon fibre reinforced organic matrix composites provide significant potential for reducing the weight of major components in the gas turbine engine and increasing their operating life when used in applications prone to vibration. A reduced weight saves energy and fuel and consequently reduces emissions. This programme includes design and tooling for the next generation composite fan system aimed at meeting future large engine market. It also includes mechanical and environmental testing to validate such designs.

Rolls-Royce plc LEAD_ORG
Rolls-Royce plc PARTICIPANT_ORG

Subjects by relevance
  1. Gas turbines
  2. Fuels
  3. Emissions
  4. Gas engine
  5. Motors and engines
  6. Carbon fibres

Extracted key phrases
  1. Composite Fan System
  2. SILOET II Project
  3. Carbon fibre composite fan system
  4. Generation composite fan system
  5. Gas turbine engine
  6. Future large engine market
  7. Aero
  8. Royce engine
  9. Engine cycle
  10. Aircraft
  11. Fuel burn advantage
  12. Service
  13. Organic matrix composite
  14. Generation Rolls
  15. Reduced weight

Related Pages

UKRI project entry

UK Project Locations