Invention Grant
US07347664B2 High-temperature component for a turbomachine, and a turbomachine 失效
用于涡轮机的高温部件和涡轮机

High-temperature component for a turbomachine, and a turbomachine
Abstract:
The invention provides a high-temperature component for a turbomachine, in particular for a blade or vane having a main blade or vane part and a blade or vane root, the high-temperature component at least partially comprising, as base material, a porous material which is filled with a viscous filler and is surrounded by a solid layer.
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