Compact brush seal
A seal structure may comprise a cavity defined at least partially by an axial surface and a radial surface. A brush seal may be disposed in the cavity. The brush seal may comprise a bristle pack and a backing plate coupled to the bristle pack. A first surface of the backing plate may contact the axial surface, and a second surface of the backing plate may contact the radial surface.
1. A seal structure, comprising:
a cavity defined at least partially by an axial surface and a radial surface; and
a brush seal disposed in the cavity, the brush seal comprising:
a bristle pack including a first end contacting the axial surface and a second end contacting the radial surface, and
a backing plate coupled to the bristle pack, wherein a first surface of the backing plate contacts the axial surface and a second surface of the backing plate contacts the radial surface, and wherein the second end of the bristle pack is configured to extend past the second surface of the backing plate.
2. The seal structure of claim 1 , further comprising a retention structure coupled to the bristle pack opposite the backing plate.
3. The seal structure of claim 2 , further comprising a spring in operable communication with the retention structure, wherein the spring forces the bristle pack toward the axial surface.
4. The seal structure of claim 3 , wherein the spring comprises at least one of a wave spring or a leaf spring.
5. The seal structure of claim 3 , wherein the spring comprises a support structure disposed radially outward of the retention structure.
6. The seal structure of claim 1 , wherein a first distance extending from the first end of the bristle pack to the first surface of the backing plate is less than or equal to 0.010 inches, and wherein a second distance extending from the second end of the bristle pack to the second surface of the backing plate is less than or equal to 0.010 inches.
7. The seal structure of claim 1 , wherein the seal structure further comprises a weld bonding the bristle pack to the backing plate, and wherein a first length the bristle pack extending from the weld to the axial surface of the cavity is different from a second length of the bristle pack extending from the weld to the radial surface of the cavity.
8. The seal structure of claim 1 , wherein the first surface of the backing plate is parallel to the axial surface of the cavity, and the second surface of the backing plate is parallel to the radial surface of the cavity.
9. The seal structure of claim 1 , wherein the backing plate comprises at least one of a cobalt alloy or a nickel alloy.
10. A seal structure for a gas turbine engine, comprising:
a vane;
a blade outer air seal (BOAS) adjacent to the vane; and
a brush seal disposed in a cavity defined at least partially by a first surface of the BOAS and a second surface of the vane, the brush seal comprising:
a bristle pack including a first end contacting the first surface of the BOAS and a second end contacting the second surface of the vane, and
a backing plate coupled to the bristle pack, wherein a first surface of the backing plate contacts the first surface of the BOAS and a second surface of the backing plate contacts the second surface of the vane, and wherein the first end of the bristle pack is configured to extend past the first surface of the backing plate, and wherein the second end of the bristle pack is configured to extend past the second surface of the backing plate.
11. The seal structure of claim 10 , wherein the first surface of the BOAS comprises a radial surface of the BOAS, and wherein the second surface of the vane comprises a first axial surface of the vane.
12. The seal structure of claim 11 , further comprising a spring in operable communication with the brush seal, wherein the spring is located between the brush seal and a second axial surface of the BOAS.
13. The seal structure of claim 12 , wherein the spring comprises a support structure disposed radially outward of a biasing portion of the spring.
14. The seal structure of claim 10 , wherein the first surface of the BOAS comprises a first radial surface of the BOAS, and wherein the second surface of the vane comprises a second radial surface of the vane.
15. The seal structure of claim 10 , wherein the first end of the bristle pack extends a first length beyond the first surface of the backing plate, and wherein the second end of the bristle pack extends a second length beyond the second surface of the backing plate.
16. The seal structure of claim 15 , wherein the first length is different from the second length.
17. The seal structure of claim 10 , wherein the first surface of the backing plate is oriented substantially orthogonal to the second surface of the backing plate.
18. A seal structure, comprising:
a vane;
a blade outer air seal (BOAS) adjacent to the vane; and
a brush seal disposed in a cavity defined at least partially by a proximal radial surface of the BOAS and an axial surface of the vane, the brush seal comprising:
a bristle pack including a first end contacting the proximal radial surface of the BOAS and a second end contacting the axial surface of the vane, and
a backing plate coupled to the bristle pack, wherein a first surface of the backing plate contacts the axial surface of the vane and a second surface of the backing plate contacts the proximal radial surface of the BOAS, and wherein the first end of the bristle pack is configured to extend past the second surface of the backing plate.
19. The seal structure of claim 18 , further comprising a spring in operable communication with the brush seal.
20. The seal structure of claim 19 , wherein the spring comprises a support structure disposed radially outward of a biasing portion of the spring.