Abstract

Mo‐based alloys with solidus temperatures around and above 2000 °C are attractive high‐temperature structural materials for future applications in the hot section of gas turbines. However, their oxidation behavior is poor due to pesting starting at 600 °C and nonprotective oxide growth at temperatures above 1000 °C. To ensure a sufficient oxidation resistance over a wide temperature range, protective coatings become inevitable. Herein, silicon coatings have been applied by magnetron sputtering on Mo‐9Si‐8B and on titan–zirconium–molybdenum alloy (TZM). The coating architecture is designed to minimize the intercolumnar gaps and porosity, thereby increasing the density. Specimens are tested at 800 and 1200 °C in air isothermally for up to 300 h. The focus is put on the chemical reactions at the coating–substrate interface, the phase formation, and the evolution of the thermally grown oxide. An initially globular SiO2 evolves into a uniform SiO2 layer providing excellent oxidation protection. The investigations reveal a rather slow interdiffusion between the coating and the alloys when tested in air. At the coating–substrate interface exclusively, the Mo3Si phase develops. Finally, the phase formation at the coating–substrate interface is studied in detail for various heat treatments in air and vacuum.

Highlights

  • Vapor on the Oxidation Behavior of the Eutectic HighTemperature Alloy Mo-20Si-52.8Ti, this issue)

  • The main emphasis of this study is to develop and characterize a single layer coating based on silicon for the Mo-9Si-8B alloy to ensure oxidation protection up to 1200 C

  • This is consistent with findings of ref. [26] where potential reasons for favored cristobalite formation at lower temperatures are discussed in detail

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Summary

Introduction

Vapor on the Oxidation Behavior of the Eutectic HighTemperature Alloy Mo-20Si-52.8Ti, this issue). Ni-based superalloy blades are progeneral oxidation behavior of Mo-based alloys is poor due to evaporation of MoO3 at temperatures below 1000 C, well known as the pesting regime,[9] and rapid oxide growth at temperatures above 1000 C. Thermal barrier layer and a bond coat to connect it to the respec- A thermochemical compatible interface between coating and tive substrate. They show excellent performance, a alloy as well as a coefficient of thermal expansion (CTE) which is close to that of the Mo-based alloys are prerequisites for a good coating performance.

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