Completed Clean Energy Engineering

SAMULET Project 1 - High Efficiency Turbomachinery

In plain English

AI plain-English summary

A single gas turbine engine on a long-haul flight could emit 836 fewer tonnes of carbon dioxide per year if the efficiency gains from this project are realised. Air travel demand is set to double within 15 years, yet Europe’s aviation research body has set strict emissions targets that current engine technology cannot meet. To square growth with climate goals, gas turbines must burn less fuel and run hotter. This project tackles that challenge from four directions at once: better cooling systems, improved aerodynamics, reduced vibration-induced fatigue, and new materials that can withstand higher temperatures. Because these work packages are interlinked, a material that allows a hotter running temperature, for example, opens up new design options for the cooling team. If successful, the research could directly cut the carbon footprint of every new aircraft that uses the technology. It also reduces lifecycle costs for airlines, which in turn affects ticket prices and fleet renewal decisions. The project is part of a larger programme that deliberately combines disciplines—materials scientists, aerodynamicists, and cooling engineers working together—rather than pursuing narrow, isolated improvements. This cross-disciplinary approach is expected to deliver greater overall efficiency than previous efforts.

View original technical description
The project aims to reduce the environmental impact of gas turbines by improving their efficiency. It also aims to reduce their lifecycle cost. Air transport demand is predicted to double in the next 10 - 15 years and triple in 20 years time. In order to enable sustained growth, whilst limiting the environmental impact of air transport in the future, the Advisory Council for Aeronautical Research in Europe (ACARE) has set challenging targets for emission levels from gas turbines. Improvements in efficiency and increased operating temperature capability are required to address these issues. The reduction in fuel burn anticipated from the project can be converted to a reduction of 836 tonnes of carbon dioxide emitted per aircraft per year. To achieve this large reduction a multifaceted approach is necessary. Hence, the project is split into a number of work packages (WP) covering cooling, aerodynamics, aeromechanical interaction and materials. The latter facilitates a wider design space for the former packages and hence all packages are interlinked. The project forms part of the larger SAMULET programme. The cross-disciplinary approach being taken, in this programme, is expected to deliver greater technical capability when compared to previous more narrowly defined research.

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Researchers

Catherine Rae (Co-Investigator)Howard Hodson (Co-Investigator)Howard Stone (Co-Investigator)Paul G. Tucker (Principal Investigator)

Related Research

Grants with similar aims, by meaning.

SAMULET Programme: High Efficiency Turbomachinery Project 1
The SAMULET Programme: Combustion Systems for Low Environmental Impact: Project 2
SAMULET_Project_2_Combustion Systems for Low Environmental Impact
The SAMULET Programme: Advanced Transmission Systems: Project 3
Improving Turbine Efficiency by Combining the Effects of Rim Seals and End-wall Contours in the Presence of Purge Flow

Original classification

Research Grant

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