Turbomachine blade with a blade tip armor cladding

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Laminated – embedded member or encased material

Reexamination Certificate

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Details

C416S24100B, C416S24100B, C415S173100, C428S610000, C428S623000, C428S627000, C428S660000, C428S666000, C428S670000

Reexamination Certificate

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07942638

ABSTRACT:
A blade of a turbomachine such as a gas turbine includes a blade vane with a blade tip and a blade base. A blade tip armor cladding is applied on the blade tip. A coating covers at least the armor cladding and includes at least one multilayer coating system, and preferably plural such coating systems stacked repetitively on one another. Each coating system includes at least two different layers stacked successively on one another, with one layer of a metal material closer to the blade tip and one layer of a ceramic material farther from the blade tip.

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