Honeycomb seal and method
A seal for a turbo machine is provided. The seal includes a plurality of honeycomb cells, at least one circumferential groove within the plurality of honeycomb cells, and at least one swirl brake within the at least one groove.
1. A seal for a turbo machine, the seal comprising:
a plurality of honeycomb cells;
at least one circumferential groove within the plurality of honeycomb cells; and
a plurality of vanes within the at least one groove,
wherein the at least one groove has a first side wall, a second side wall, and each of the plurality of vanes extends axially between the first and second side walls of the at least one groove.
2. The seal of claim 1 wherein the plurality of honeycomb cells are spaced from the at least one groove.
3. The seal of claim 1 wherein the plurality of honeycomb cells include a plurality of partial honeycomb cells extending from the first and second side walls of the at least one groove.
4. The seal of claim 1 wherein each vane tapers in at least one of a radial direction and an axial direction.
5. The seal of claim 1 wherein each vane has a constant thickness in a direction extending from the first side wall to the second side wall of the at least one groove.
6. The seal of claim 5 wherein a top surface of the plurality of honeycomb cells defines a first cylinder and a top surface of each of the vanes define a second cylinder, wherein the first cylinder and the second cylinder are coaxial.
7. The seal of claim 6 wherein the at least one groove has a groove depth and the plurality of honeycomb cells have a cell height, and wherein the groove depth is greater than the cell height.
8. A turbo machine comprising:
a turbo machine stator;
a turbo machine rotor rotatable relative to the turbo machine stator; and
a seal between the stator and the rotor;
wherein the seal comprises a plurality of honeycomb cells, a groove within, the plurality of honeycomb cells, and a plurality of vanes within the groove, and
wherein the groove has a first side wall, a second side wall, and each of the plurality of vanes extends axially between the first and second side walls of the at least one groove.
9. A method of manufacturing a seal for a turbo machine, the method comprising:
forming a groove in a seal body of the seal, wherein the groove has a first side wall, a second side wall;
forming a plurality of honeycomb cells in the seal body; and
providing a plurality of vanes within the groove, each of the plurality of vanes extending axially between the first and second side walls of the at least one groove.
10. The seal of claim 1 wherein both the first and second side walls of the at least one groove are separated from the plurality of honeycomb cells by a margin area.