4.4 Article

Abradable Coatings for Small Turboprop Engines: A Case Study of Nickel-Graphite Coating

Journal

JOURNAL OF THERMAL SPRAY TECHNOLOGY
Volume 28, Issue 4, Pages 794-802

Publisher

SPRINGER
DOI: 10.1007/s11666-019-00838-4

Keywords

abradable coating; aerospace; coatings for engine components; erosion resistance; Rietveld analysis

Funding

  1. Ministry of Trade of the Czech Republic [FV-TRIO FV10211]

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For the engines used in small turboprop aircrafts, the introduction of abradable coatings represents a feasible way to reach higher levels of overall engine efficiency, specifically by improving the fuel consumption and increasing the inter-turbine temperature margin. Abradable coatings on seals also contribute to improved hot restarts capability of an engine and lead to substantial extension of service life of the rotating counter bodies. In our contribution, we concentrate on flame-sprayed nickel-graphite abradable coating that can be used in turboprop engines both for seals and clearance control. The focus is the impact of spraying parameters on the physical and function properties of the abradable coating.

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