WE CLAIM
1. A brush seal for use between a rotating component and a stationary
component in a turbomachine, the brush seal comprising:
a set of flexible bristles having a fixed end and a free end, the free end of the set of flexible bristles sealing against a radially inward surface of the stationary component, the set of flexible bristles angled axially at an axial angle of about 15 degrees to about 70 degrees with respect to the rotating component, the set of flexible bristles angled circumferentially at an angle that is less than the axial angle,
a frusto-conical retaining plate, the retaining plate extending radially outward from the rotating component at least partially along a length of the set of flexible bristles, such that the retaining plate is configured to at least partially support the set of flexible bristles on a radially inner surface of the retaining plate from centrifugal loading in an operative state of the turbomachine,
a bristle shield, the bristle shield extending radially outward from the rotating component at least partially along a length of the set of flexible bristles, such that the bristle shield is configured to at least partially shield the set of flexible bristles from flow during an operative state of the turbomachine, the set of flexible bristles located between the retaining plate and the bristle shield,
a circumferential groove in the rotating component, the circumferential groove having a downstream side and an upstream side,
a side plate attached to the upstream side of the circumferential groove, and
wherein the fixed end of the set of flexible bristles is attached to the upstream side of the circumferential groove by the side plate and the retaining plate

is attached to both the downstream and upstream side of the circumferential groove, the retaining plate being attached to the upstream side of the circumferential groove by the side plate in the rotating component.
2. The brush seal of claim 1, wherein the axial angle is about 30 degrees to about 45 degrees.
3. The brush seal of claim 1, the bristle shield extending radially outward of the retaining plate, or adjacent to the radially inward surface of the stationary component, or about the same radial distance as the retaining plate.
4. The brush seal of claim 1, wherein the set of flexible bristles is bent, and an axial position at which the fixed end of the set of flexible bristles is attached to the circumferential groove is axially displaced with respect to an axial position at which the free end of the set of flexible bristles seals against the radially inward surface of the stationary component.
5. The brush seal of claim 1, wherein the conical retaining plate is retained within the circumferential groove by a dovetail assembly, the dovetail assembly comprising:
a retaining feature disposed on a radially outer portion of the circumferential groove, and
an entry dovetail slot for inserting the set of flexible bristles into the

circumferential groove.
6. The brush seal of claim 1, the bristle shield comprising:
a second set of bristles that are stiffer and larger in diameter than the set of flexible bristles, or
one or more sheet metal members.
7. The brush seal of claim 1, the set of flexible bristles comprised of bristles having a diameter of about 2.5 mils to about 4 mils in diameter, and the bristle shield comprising bristles of about 5 mils to about 10 mils in diameter or sheet metal having a thickness of about 5 mils to about 10 mils.
8. A turbomachine comprising:
a rotating component having a circumferential groove therein, the circumferential groove having an upstream side and a downstream side;
a side plate attached to the circumferential groove,
a stationary component; and
a brush seal for use between the rotating component and the stationary component, the brush seal comprising:
a set of flexible bristles having a fixed end and a free end, the fixed
end of the set of flexible bristles is attached to the circumferential groove by
the side plate, the free end of the set of flexible bristles seals against a
radially inward surface of the stationary component, the set of flexible

bristles are angled axially at an axial angle of about 15 degrees to about 70 degrees with respect to the rotating component,
a retaining plate extending at least partially along a length of the set of flexible bristles, such that the retaining plate is configured to at least partially support the set of flexible bristles from centrifugal loading in an operative state of the turbomachine, the retaining plate is attached to the circumferential groove in the rotating component,
a bristle shield, the bristle shield extending radially outward from the rotating component at least partially along a length of the set of flexible bristles, such that the bristle shield is configured to at least partially shield the set of flexible bristles from flow during an operative state of the turbomachine, the set of flexible bristles located between the retaining plate and the bristle shield.
9. The turbomachine of claim 8, wherein the flexible bristles are angled circumferentially at an angle less than the axial angle.
10. The turbomachine of claim 9, the bristle shield comprising:
a second set of bristles that are stiffer and larger in diameter than the set of flexible bristles, or
one or more sheet metal members.
11. The turbomachine of claim 10, the set of flexible bristles comprising:

bristles having a diameter of about 2.5 mils to about 4 mils in diameter, and the bristle shield comprising bristles of about 5 mils to about 10 mils in diameter, or sheet metal having a thickness of about 5 mils to about 10 mils.
12. The turbomachine of claim 11, the bristle shield extending radially outward of the retaining plate.
13. The turbomachine of claim 12, wherein the bristle shield faces a high-pressure side of the brush seal, and the retaining plate is exposed to a downstream, low-pressure side of the brush seal.
14. The turbomachine of claim 13, wherein the set of flexible bristles is bent, and an axial position at which the fixed end of the set of flexible bristles is attached to the circumferential groove is axially displaced with respect to an axial position at which the free end of the set of flexible bristles seals against the radially inward surface of the stationary component.
15. The turbomachine of claim 8, wherein the brush seal further comprises a series of arcuate segments collectively forming a ring disposed about a circumference of the rotating component within the circumferential groove.
16. A brush seal for use between a rotating component and a stationary component in a turbomachine, a circumferential groove is in the rotating component

and a side plate is attached to the circumferential groove, the brush seal comprising: a set of flexible bristles having a fixed end and a free end, the fixed end of the set of flexible bristles is attached to the circumferential groove by the side plate, and the free end of the set of flexible bristles seals against a radially inward surface of the stationary component, the set of flexible bristles are axially angled at an angle of about 15 degrees to about 70 degrees with respect to the rotating component, and the set of flexible bristles are circumferentially angled at an angle that is less than the axial angle,
a retaining plate attached to the circumferential groove by a dovetail assembly, the retaining plate extends radially outward from the rotating component at least partially along a length of the set of flexible bristles, such that the retaining plate is configured to at least partially support the set of flexible bristles on a radially inner surface of the retaining plate from centrifugal loading in an operative state of the turbomachine,
a bristle shield, the bristle shield extending radially outward from the rotating component at least partially along a length of the set of flexible bristles, such that the bristle shield is configured to at least partially shield the set of flexible bristles from flow during an operative state of the turbomachine, the set of flexible bristles located between the retaining plate and the bristle shield.
17. The brush seal of claim 16, wherein the set of flexible bristles is bent, and an axial position at which the fixed end of the set of flexible bristles is attached to the circumferential groove is axially displaced with respect to an axial position at which

the free end of the set of flexible bristles seals against the radially inward surface of the stationary component.
18. The turbomachine of claim 16, the bristle shield comprising:
a second set of bristles that are stiffer and larger in diameter than the set of flexible bristles, or
one or more sheet metal members.
19. The brush seal of claim 18, the set of flexible bristles comprising:
bristles having a diameter of about 2.5 mils to about 4 mils in diameter, and
the bristle shield comprising bristles of about 5 mils to about 10 mils in
diameter, or sheet metal having a thickness of about 5 mils to about 10 mils.
20. The brush seal of claim 16, the bristle shield extending radially outward of
the retaining plate, or adjacent to the radially inward surface of the stationary
component, or about the same radial distance as the retaining plate.