Title
SAMULET Project 1 - High Efficiency Turbomachinery

CoPED ID
cd65ee17-077a-4c33-967d-b5615e6460e8

Status
Closed

Funders

Value
£571,164

Start Date
June 30, 2009

End Date
June 29, 2011

Description

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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.

Subjects by relevance
  1. Emissions
  2. Environmental effects
  3. Gas turbines
  4. Decrease (active)
  5. Carbon dioxide
  6. Greenhouse gases
  7. Projects
  8. Traffic
  9. Climate changes

Extracted key phrases
  1. High Efficiency Turbomachinery
  2. SAMULET Project
  3. Project
  4. Air transport demand
  5. Environmental impact
  6. Gas turbine
  7. Large samulet programme
  8. Large reduction
  9. Year time
  10. Work package
  11. Great technical capability
  12. Disciplinary approach
  13. Multifaceted approach
  14. Lifecycle cost
  15. Temperature capability

Related Pages

UKRI project entry

UK Project Locations