Method of manufacturing a component of a turbomachine, component of a turbomachine and turbomachine
The component of the turbomachine comprises a body of the component, a bond layer covering a base surface of the body, and a top layer covering the bond layer and made of abradable ceramic material. The base surface of the component has patterned protrusions and, through two covering steps used for forming the bond layer and the top layer, also the top surface of the component has patterned protrusions. The pattern protrusions of the base surface may be obtained in different ways, for example casting, milling, grinding, electric discharge machining or additive manufacturing. The patterned protrusions belong to an abradable seal of the turbomachine, and may be shaped and sized to maintain specified clearances and to reduce flow of a working fluid within turbomachinery equipment and/or it's components.
1. A method of manufacturing a component of a turbomachine, the component comprising a body having a base surface including patterned protrusions of the base surface separated from one another by flat portions of the base surface, the patterned protrusions shaped as ridges having a trapezium shaped cross-section, the method comprising:
covering the base surface with a bond layer including patterned protrusions separated from one another by flat portions corresponding to the flat portions of the base surface; and
applying a top layer made of abradable ceramic material to cover the bond layer creating a top surface of the component that is not machined and includes patterned protrusions shaped so as to be similar to the shapes of the patterned protrusions of the base surface and the bond layer;
wherein a thickness of the applied top layer covering the flat portion of the bond layer is greater than a thickness covering the patterned protrusions of the bond layer.
2. The method of claim 1 , wherein the patterned protrusions of the base surface of the body are obtained by casting, milling, grinding, electric discharge machining or additive manufacturing.
3. The method of claim 1 , wherein the bond layer is made of Ni3Al and is obtained by diffusion.
4. The method of claim 1 , wherein the top layer is made of DVC YSZ or DVC DySZ and is applied by spraying.
5. The method of claim 1 , wherein the body is made of a nickel base superalloy.
6. A component of a turbomachine, the component comprising:
a body of the component;
a bond layer covering a base surface of the body, wherein the base surface includes patterned protrusions separated from one another by flat portions, the base surface patterned protrusions shaped as ridges having a trapezium shaped cross-section, and wherein the bond layer includes patterned protrusions separated from one another by flat portions corresponding to the flat portions of the base surface; and
a top layer covering the bond layer to form a top surface of the component that is not machined, the top layer being made of abradable ceramic material and including patterned protrusions separated from one another by a flat portion and shaped so as to be similar to the shapes of the patterned protrusions of the base surface and bond layer;
wherein a thickness of the top layer covering the flat portion of the bond layer is greater than a thickness covering the patterned protrusions of the bond layer.
7. The component of claim 6 , wherein the protrusions of the base surface and of the top surface are a set of shaped ridges parallel to each other.
8. The component of claim 7 , wherein each of the shaped ridges comprises:
a first straight section;
a second curved section contiguous with the first straight section; and
a third straight section contiguous with the second curved section.
9. The component of claim 7 , wherein each of the shaped ridges comprises two or more curved sections.
10. The component of claim 6 , wherein the body is made of a nickel base superalloy.
11. A turbomachine comprising at least one component, the component comprising:
a body of the component;
a bond layer covering a base surface of the body, wherein the base surface includes patterned protrusions separated from one another by flat portions, the base surface patterned protrusions shaped as ridges having a trapezium shaped cross-section, and wherein the bond layer includes patterned protrusions separated from one another by flat portions corresponding to the flat portions of the base surface; and
a top layer covering the bond layer to form a top surface of the component that is not machined, the top layer being made of abradable ceramic material and including patterned protrusions separated from one another by a flat portion and shaped so as to be similar to the shapes of the patterned protrusions of the base surface and bond layer;
wherein a thickness of the top layer covering the flat portion of the bond layer is greater than a thickness covering the patterned protrusions of the bond layer.
12. The turbomachine of claim 11 , wherein the protrusions of the base surface and of the top surface are a set of shaped ridges parallel to each other.
13. The turbomachine of claim 11 , wherein each of the shaped ridges comprises:
a first straight section;
a second curved section contiguous with the first straight section; and
a third straight section contiguous with the second curved section.
14. The turbomachine of claim 12 , wherein each of the shaped ridges comprises two or more curved sections.
15. The turbomachine of claim 11 , wherein the body is made of a nickel base superalloy.
16. The method of claim 3 , wherein the bond layer is obtained by solid state diffusion, liquid state diffusion, or chemical vapor diffusion.
17. The method of claim 1 , wherein the body is made of stainless steel.
18. The method of claim 1 , wherein the ridges of the base surface include three curved sections.