Silicon carbide composition for turbine blade tips

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part

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4151734, 4151744, 416241B, 416241R, 428404, 428698, 427450, 427452, F01D 1114, F01D 1108, B64C 1116, B64C 2746

Patent

active

059972483

ABSTRACT:
A granular composition is applied to tips of rotor blades utilized in a gas turbine engine wherein the blade tips rub against an abradable ceramic layer. Individual grains each have a core of silicon carbide and a layer of aluminum nitride on the core. A layer of a cladding metal may be bonded to the aluminum nitride. The composition also may include particles of cubic boron nitride and/or particles of metal alloy blended with the grains of silicon carbide.

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