Completed Materials & Manufacturing Engineering

SILOET 2: Project 5 High Temperature Seals and Oil System

In plain English

AI plain-English summary

Rolls-Royce and three UK universities are redesigning the hot, high-pressure sections inside jet engines to run at even higher temperatures. Today’s gas turbine engines are limited by how well their internal seals and oil systems can handle extreme heat. Pushing temperatures higher would allow the engine to burn fuel more completely, cutting CO₂ emissions and improving fuel efficiency. It would also extend the life of critical components such as compressor discs and blades, reducing maintenance costs and downtime for airlines. If the project succeeds, the new materials and thermal management designs could be used in future civil aircraft engines, making flying cheaper and less polluting. The same technologies could also be adapted for power-generation gas turbines, helping to reduce emissions from electricity production. For passengers, the most visible change would be lower ticket prices and fewer flight delays caused by engine maintenance—but the real impact would be a quieter, less visible one: a measurable reduction in aviation’s carbon footprint.

View original technical description
The High Temperature Compressors and Discs project is a collaborative research and technology project led by Rolls-Royce with University of Nottingham, University of Surrey and Swansea University. The project aims to develop compressor system and material technologies for future civil aerospace gas turbine engines, with potential wider benefits of exploitation in gas turbines for other market sectors. New technologies will enable increased temperatures for gas turbines which will help reduce fuel consumption and resultant CO2 emissions; and improve component life and life predictions. Fundamental and applied research will develop new materials and new designs of compressor sub-systems to improve thermal management.

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Related Research

Grants with similar aims, by meaning.

SILOET 2: Project 8 High Temperature Turbine Technology and Demonstration
SILOET Project 4 - High Temperature Materials
SILOET 2: Project 6 High Temperature Capability - Compressor and Discs
EPSRC Industrial Case Award/Rolls Royce - Application of CMCs for static sealing components to be used in high temperature engine components
SILOET Project 7 - Component Technologies

Original classification

BEIS-Funded Programmes

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