Towards net zero - aerospace

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Title
Towards net zero - aerospace
CoPED ID
3d63f9c7-04f6-4aea-9be4-31c169707c55
Status
Active
Funder
EPSRC
Value
No funds listed.
Start Date
Sept. 30, 2021
End Date
Sept. 29, 2025
Description

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The project relates to the study of ammonia/hydrogen blends for their potential use in civil aviation applications. The study will include:

- Investigation of thermoacoustics and various injection techniques to enable high flame stability combined with low emissions
- Determination of optimal cracking split of NH3/H2/N2 for use in turbofan engine
- Development/demonstration of full scale engine injector and combustor sector suited to that fuel blend.

Jordan Davies STUDENT_PER

Subjects by relevance
  1. Emissions
  2. Fuel injection engines
  3. Diesel engines
  4. Combustion (active)

Extracted key phrases
  1. Civil aviation application
  2. Scale engine injector
  3. Potential use
  4. Study
  5. High flame stability
  6. Optimal cracking split
  7. Turbofan engine
  8. Project
  9. Net
  10. Aerospace
  11. Fuel blend

Related Pages

UKRI project entry

UK Project Locations