Utilization of discontinuous fibers for improving properties of high temperature insulation of ceramic matrix composites
View Patent ↗An insulating material 14 adapted for use in a high temperature environment for coating a turbine component is provided. The insulating material comprises a plurality of geometric shapes 18 . The insulating material further comprises a binder for binding together the geometric shapes. A plurality of discontinuous fibers is added to the binder. The discontinuous fibers are adapted to controllably affect one or more properties of the insulating material. For example, non-fugitive chopped fibers 50 may be added to affect a tensile strength property of the insulating material, and fugitive chopped fibers 52 may be added to affect a density property of the insulating material.
1. An insulating material adapted for use in a high temperature environment for coating a turbine component, said material comprising:
a plurality of geometric shapes comprising a three-dimensional array of hollow ceramic spheres;
a binder for binding together the geometric shapes; and
a first plurality of discontinuous fibers comprising ceramic fibers added to said binder, said discontinuous fibers adapted to controllably affect one or more properties of said insulating material.
2. The material of claim 1 wherein said plurality of ceramic fibers comprises a combination of oxide and non-oxide ceramic fibers.
3. The material of claim 1 wherein an amount of said ceramic fibers ranges from about 5% of volume of the insulating material to about 30% of volume of the insulating material.
4. The material of claim 1 wherein a length of said ceramic fibers ranges from about 150 μm to approximately 1000 μm.
5. The material of claim 1 wherein a length of said ceramic fibers ranges from about 250 μm to approximately 500 μm.
6. The material of claim 1 further comprising a second plurality of discontinuous fibers comprising a plurality of fugitive fibers.
7. The material of claim 6 wherein said plurality of fugitive fibers is selected from the group consisting of carbon-based fibers, graphite-based fibers, polymeric-based fibers, and any combination of the foregoing types of fugitive fibers.
8. The material of claim 6 wherein a concentration of said ceramic fibers is selected to controllably affect a tensile strength property of the insulating material, and a concentration of said fugitive fibers is selected to controllably affect a density property of the insulating material.
9. The material of claim 6 wherein said geometric shapes comprise a three-dimensional array of partially filled spheres in lieu of hollow ceramic spheres.
10. The material of claim 1 wherein the insulating material comprises a first layer having a first concentration of discontinuous ceramic fibers, and further comprises at least a second layer having a second concentration of discontinuous ceramic fibers, and wherein the value of the first concentration is distinct from the value of the second concentration.
11. The material of claim 1 wherein the amount of ceramic fibers in the insulating material is selected to define a gradient, wherein said gradient varies as a function of a distance relative to an interface boundary between said insulating material and a ceramic matrix composite material.
12. An insulating material adapted for use in a high temperature environment for coating a turbine component, said material comprising:
a plurality of geometric shapes comprising a three-dimensional array of hollow ceramic spheres;
a binder for binding together the geometric shapes;
a plurality of discontinuous fibers comprising ceramic fibers added to said binder to reduce propagation of fractures in said insulating material; and
a plurality of discontinuous fugitive fibers, wherein a concentration of said ceramic fibers is selected to controllably affect a tensile strength property of the insulating material, and a concentration of said fugitive fibers is selected to controllably affect a bulk density of the insulating material.