Back to results
US 7,347,664 B2Granted
High-temperature component for a turbomachine, and a turbomachine
AssigneeSiemens Aktiengesellschaft
InventorsAndreas Kayser, Ivo Wolter
Life of this patent
Estimating the term…
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.
Claims19
A turbine blade or vane component for use in a high temperature application, comprising:
- a blade or vane airfoil portion;
- a blade or vane root portion;
- a blade or vane platform portion;
- and
- a base material,
- wherein a portion of the base material is a porous material that is filled with a viscous filler and is surrounded by a solid layer.
3 more elements
A turbine component for use in a high temperature application, comprising:
- a base material,
- wherein a portion of the base material is a porous material that is filled with a viscous filler and is surrounded by a solid layer.
A turbomachine, comprising:
- a turbine blade or vane for use in a high-temperature application;
- comprising:
- a blade or vane airfoil portion;
- a blade or vane root portion;
- a blade or vane platform portion;
- a base material,
- wherein a portion of the base material is a porous material that is filled with a viscous filler and is surrounded by a solid layer.
4 more elements
Dependencies are inferred from the claim text.