Oxidation of nickel superalloys for aero-engine applications

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Title
Oxidation of nickel superalloys for aero-engine applications

CoPED ID
461d0b9c-15b0-4faf-be99-803d26216567

Status
Active

Funders

Value
No funds listed.

Start Date
Sept. 30, 2019

End Date
June 29, 2023

Description

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Nickel superalloys are used in aero-engines due to their outstanding mechanical strength up to high temperatures. Thermally grown oxides can weaken the alloys, however, when carefully designed, these oxides are the alloy's first line of defence against corrosion. Oxides can protect alloys by passivating the surface and preventing further reactions. For this, oxides need to be continuous, non-porous and adhere well to the substrate. This leaves plenty of scope for the optimization of alloy composition to improve the oxide scale. The aim of your PhD project is to optimize the composition to create a strong oxide through targeted alloying additions. In particular, the effect of trace amounts of Si have been shown to promote the formation of a continuous, protective layer of alumina on the surface. This layer of alumina is more protective than the chromia or nickel-based spinels that normally form. However, there is an optimal amount of silicon beyond which the effect will be deleterious both for oxidation and for the precipitation of embrittling phases within the alloy, causing microstructural instability. Silicon in the oxide scale has been shown to interact directly with tantalum, though no systematic study on the topic has ever been performed and the mechanisms are not well understood

Imperial College London LEAD_ORG
Rolls-Royce plc STUDENT_PP_ORG

Stella Pedrazzini SUPER_PER
Declan Clarke STUDENT_PER

Subjects by relevance
  1. Nickel
  2. Alloys
  3. Oxides
  4. Corrosion
  5. Oxidation (passive)
  6. Aluminum oxide
  7. Interaction
  8. Lines of defence

Extracted key phrases
  1. Nickel superalloy
  2. Oxide scale
  3. Oxidation
  4. Strong oxide
  5. Engine application
  6. Alloy composition
  7. Outstanding mechanical strength
  8. Aero
  9. Protective layer
  10. Trace amount
  11. High temperature
  12. Effect
  13. Continuous
  14. Surface
  15. Alumina

Related Pages

UKRI project entry

UK Project Locations