Intersegment seal for blade outer air seal
A blade outer air seal assembly includes a blade outer air seal segment that has a base portion that extends from a first axial side to a second axial side and from a first circumferential side to a second circumferential side. An intersegment seal is arranged adjacent the first circumferential side. The intersegment seal has a first seal portion and a second seal portion connected by a rib.
1. A blade outer air seal assembly, comprising:
a blade outer air seal segment having a base portion extending from a first axial side to a second axial side and from a first circumferential side to a second circumferential side; and
an intersegment seal arranged adjacent the first circumferential side, the intersegment seal having a first seal portion and a second seal portion connected by a rib, the rib extends along a length of the first seal portion in an axial direction, wherein the first and second seal portions and the rib form an H shape in a plane extending in the circumferential direction; and
wherein the blade outer air seal segment has a circumferentially extending slot at the first circumferential side, and at least a portion of the first seal portion is arranged within the circumferentially extending slot.
2. The blade outer air seal assembly of claim 1 , wherein the intersegment seal is formed from a ceramic matrix composite material.
3. The blade outer air seal assembly of claim 1 , wherein the first seal portion is generally rectangular having a first length in the axial direction and a first width in the circumferential direction.
4. The blade outer air seal assembly of claim 3 , wherein the second seal portion has a second length in the axial direction that is smaller than the first length of the first seal portion.
5. The blade outer air seal assembly of claim 3 , wherein the second seal portion has a second width in the circumferential direction that is the same as the first width of the first seal portion.
6. The blade outer air seal assembly of claim 1 , wherein the first seal portion has a first thickness and the second seal portion has a second thickness that is the same as the first thickness.
7. The blade outer air seal assembly of claim 1 , wherein the second seal portion has a radially extending wall.
8. The blade outer air seal assembly of claim 7 , wherein the radially extending wall extends a width of the second seal portion in the circumferential direction.
9. The blade outer air seal assembly of claim 7 , wherein the radially extending wall is at an aft end of the second seal portion.
10. The blade outer air seal assembly of claim 1 , wherein the second seal portion is arranged adjacent a radially outer surface of the base portion.
11. The blade outer air seal assembly of claim 10 , wherein the second seal portion is arranged radially outward of the radially outer surface of the base portion.
12. The blade outer air seal assembly of claim 1 , wherein the first and second portions have a thickness between 0.01 and 0.04 inches (0.254 and 1.016 mm).
13. The blade outer air seal assembly of claim 1 , wherein the blade outer air seal segment is a ceramic matrix composite material.
14. The blade outer air seal assembly of claim 1 , wherein the first seal portion extends axially beyond the second seal portion.
15. The blade outer air seal assembly of claim 1 , wherein the second seal portion has a chamfer.
16. The blade outer air seal assembly of claim 1 , wherein the first and second seal portions extend circumferentially outward of the rib.
17. The blade outer air seal assembly of claim 1 , wherein the blade outer air seal segment has a first axial wall axially spaced from a second axial wall, the first and second axial walls extending from the base portion, and an outer wall extends between the first and second axial walls.