Hot Corrosion of Nickel alloys for aero-engine applications

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Title
Hot Corrosion of Nickel alloys for aero-engine applications

CoPED ID
7a07b976-4665-4812-921a-24fc411000fa

Status
Active


Value
No funds listed.

Start Date
Feb. 28, 2020

End Date
Nov. 30, 2023

Description

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The project will help understand the fundamental effect of refractory elements on nickel superalloy corrosion. Nickel superalloys are used in the turbine blades and discs of aero-engines because of their outstanding mechanical properties up to elevated temperatures. Rolls-Royce plc, as a world leading aero-engine manufacturer, has a strong interest in understanding the failure mechanisms of alloys in service, in order to improve them. Some nickel-based superalloys fail substantially faster than others when exposed to sulphur-containing compounds, however, the mechanisms are not well understood. Refractory elements such as Mo, W, Re and Ru can accelerate the rate of corrosion when the alloy is exposed to corrosive gases and molten salts. A systematic study producing alloys with varying compositions that swap refractories (Mo/W) with elements that form protective oxides (Cr/Al) is required to understand the effect of those elements. Your project will involve the production of new alloys, advanced characterisation techniques such as scanning/transmission electron microscopy, atom probe tomography and synchrotron-based techniques. It will involve mechanical testing under different environments and some thermodynamic modelling to understand the failure mechanisms.

Imperial College London LEAD_ORG
Rolls-Royce plc STUDENT_PP_ORG

Stella Pedrazzini SUPER_PER
Cynthia Rodenkirchen STUDENT_PER

Subjects by relevance
  1. Alloys
  2. Nickel
  3. Metals
  4. Electron microscopy
  5. Materials testing
  6. Physical properties
  7. Corrosion
  8. Tomography
  9. Metallurgy

Extracted key phrases
  1. Nickel alloy
  2. Nickel superalloy corrosion
  3. Hot Corrosion
  4. Engine application
  5. New alloy
  6. Refractory element
  7. Engine manufacturer
  8. Aero
  9. Outstanding mechanical property
  10. Fundamental effect
  11. Failure mechanism
  12. Advanced characterisation technique
  13. Project
  14. Mechanical testing
  15. Turbine blade

Related Pages

UKRI project entry

UK Project Locations