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You are here: Home » Insight hub » Case Studies » Lucideon's Surface Analysis Provides Key Data for Rolls-Royce

Lucideon's Surface Analysis Provides Key Data for Rolls-Royce

The Challenge

Ni-base superalloys, grown from single crystals, have been developed to meet stringent demands in the hot sections of modern gas turbine engines. These turbine blades require a thermal barrier coating (TBC) to provide adequate insulation. The TBC comprises an yttria-stabilised zirconia (YSZ) top coat and a Pt-diffused bond coat which aids adhesion of the YSZ to the superalloy substrate. Sulphur, which is present at low ppm levels in the Ni-base alloy, is known to segregate during thermal cycling and may accelerate cavity formation with the potential to compromise long-term engine performance.

Lucideon was approached by Rolls-Royce to assess quantitative changes in sulphur concentration across the microstructure of a turbine blade material which had been subjected to a series of treatments including high temperature ageing and oxidation cycles.

What We Delivered

Lucideon utilized its expertise in secondary ion mass spectrometry (SIMS) to develop a custom method to examine the in-depth distribution of sulphur and other key elements including Pt, Cr and Al across the near-surface microstructure using cross-sectional imaging of the treated turbine blade materials. Retrospective linescans from the image data allowed quantitative comparison of the effects of treatments on sulphur segregation through the top coat / bond coat / substrate structure1.

Value to the Client

The SIMS method successfully monitored the in-depth distribution of key alloying elements and trace elements i.e. sulphur, within Ni-base superalloys. It clearly identified areas of sulphur partitioning within the structure and the effects of thermal cycling on this process. This study helped Rolls-Royce to increase its current understanding of sulphur’s role in the failure mechanisms of TBC’s along with the potential to investigate ways to reduce failures in the TBC structure.

References :

  1. N. D’Souza, F. Liu, S. Irwin, A. Brown, I.M. Edmonds & D.S. Rickerby; Oxid. Met. (2016) 85:369-389
Aircraft Engine

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