Completed Materials & Manufacturing Engineering

SAMULET Programme: High Efficiency Turbomachinery Project 1

In plain English

AI plain-English summary

A jet engine's hottest turbine blades will soon face higher temperatures and more corrosive exhaust, thanks to new coatings, cooling methods, and casting techniques being developed in this project. The problem is straightforward: aircraft engines burn fuel to produce thrust, and the hotter they run, the more efficient they become. But extreme heat degrades metal components, causing oxidation, fatigue, and corrosion that shorten engine life and increase maintenance costs. Current turbine materials and coatings are approaching their limits. This project targets that ceiling by improving the fundamental understanding of how oxidation and fatigue interact with coatings, then using that knowledge to design better alloys, protective layers, and cooling geometries. If successful, the technologies will reduce fuel burn and CO₂ emissions per flight—a direct environmental and economic benefit. They will also improve component life prediction, meaning airlines can schedule maintenance more precisely rather than replacing parts early as a safety margin. The work draws on Rolls-Royce’s University Technology Centres and includes high-speed rig testing of new aerodynamic designs, as well as new casting methods for single-crystal alloys that can withstand higher operating temperatures. The result is quieter, more efficient engines that stay in service longer.

View original technical description
This project will develop both turbine technologies for turbo-machinery that reduce fuel burn and hence CO2 emissions and technologies that improve component life and life prediction. This is by a programme of work developing fundamental and applied research that produces technologies that will be incorporated into future demonstrators. The project utilises the capabilities of the Rolls-Royce University Technology Centres (UTCs) coupled with Rolls-Royce’s expertise to develop technologies that address a range of high-temperature turbine challenges. These include improved coatings with better oxidation and environmental capability; improving lifing algorithms by improving the understanding of the effects of oxidation, fatigue, corrosion and coatings on component life; new and improved turbine cooling and aerodynamic technologies; demonstrating some of the aerodynamic technologies in a high speed rig; developing new casting technologies to improve the high temperature capability of single crystal alloys; improving aeromechanical design to reduce the impact of high cycle fatigue.

View the original record at the funder ↗

Related Research

Grants with similar aims, by meaning.

SAMULET Project 1 - High Efficiency Turbomachinery
The SAMULET Programme: Advanced Transmission Systems: Project 3
SILOET 2: Project 8 High Temperature Turbine Technology and Demonstration
Improving Turbine Efficiency by Combining the Effects of Rim Seals and End-wall Contours in the Presence of Purge Flow
Turbomachinery for Future Energy Systems

Original classification

BEIS-Funded Programmes

Plain English summaries and category classifications on this site are generated by AI and may not perfectly reflect the original research.