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Abstract <p>The influence of a deposition technology on the structure and properties of a ceramic coating on a turbine blade is studied. The proposed technical solution of satellite rotation of a blade relative to a vapor flow is found to increase the uniformity of the coating thickness and to form a thermal barrier layer on the turbine blade platform. The microstructure of the thermal barrier coating layer around the perimeter of the blade airfoil is investigated.</p>

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Experimental Study of the Influence of a Deposition Technology on the Structure and Properties of a Thermal Barrier Coating on Gas Turbine Engine Blades

  • 期刊论文

  • 发表日期：

    2025年6月1日

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  • V. G. Opokin,
  • R. G. Ravilov,
  • V. M. Samoilenko,
  • G. T. Pashchenko

摘要

Abstract

The influence of a deposition technology on the structure and properties of a ceramic coating on a turbine blade is studied. The proposed technical solution of satellite rotation of a blade relative to a vapor flow is found to increase the uniformity of the coating thickness and to form a thermal barrier layer on the turbine blade platform. The microstructure of the thermal barrier coating layer around the perimeter of the blade airfoil is investigated.