CMC BOAS arrangement

1. A blade outer air seal, comprising:

a base portion extending between a first circumferential side and a second circumferential side and from a first axial side to a second axial side, a first hook extending from the base portion and circumferentially spaced from a second hook extending from the base portion, the first and second hooks extending along the base portion in an axial direction, wherein the first and second hooks extend circumferentially inward toward one another, wherein the first circumferential side has a protrusion and the second circumferential side has a groove.

2. The blade outer air seal of claim 1 , wherein the base portion extends aft of the first ad second hooks in the axial direction.

3. The blade outer air seal of claim 1 , wherein the protrusion and the groove extend along the axial length.

4. The blade outer air seal of claim 1 , wherein the blade outer air seal is formed from a ceramic material.

5. A turbine section for a gas turbine engine, comprising:

a turbine blade extending radially outwardly to a radially outer tip and for rotation about an axis of rotation;

a blade outer air seal having a plurality of segments mounted in a support structure via a carrier, the plurality of segments arranged circumferentially about the axis of rotation and radially outward of the outer tip;

each seal segment having a base portion extending between a first circumferential side and a second circumferential side and from a first axial side to a second axial side, a first hook extending from the base portion and circumferentially spaced from a second hook, the first and second hooks extending along an axial length of the base portion, wherein the first and second hooks extend circumferentially inward toward one another, wherein the first circumferential side has a protrusion and the second circumferential side has a groove.

6. The turbine section of claim 5 , wherein the carrier has an axially extending platform that is configured to engage the first and second hooks.

7. The turbine section of claim 6 , wherein the carrier has first and second tabs extending circumferentially from the platform.

8. The turbine section of claim 5 , wherein the carrier has a first carrier hook that is engaged with the support structure.

9. The turbine section of claim 8 , wherein the first carrier hook extends circumferentially.

10. The turbine section of claim 8 , wherein the carrier has a second carrier hook that is engaged with the support structure, the second carrier hook axially spaced from the first carrier hook.

11. The turbine section of claim 5 , wherein the protrusion of each seal segment is engaged with the groove of an adjacent seal segment.

12. The turbine section of claim 5 , wherein a brush seal is arranged along a trailing edge of the seal segment and carrier.

13. The turbine section of claim 12 , wherein a wear liner is arranged between the carrier and the brush seal.

14. The turbine section of claim 5 , wherein a vane platform is engaged with a forward side of the carrier and the seal segment.

15. The turbine section of claim 5 , wherein a spring seal is arranged between each of the plurality of segments, the spring seal extending in an axial direction.

16. The turbine section of claim 15 , wherein the spring seal is arranged within the groove of each seal segment.

17. The turbine section of claim 15 , wherein the spring seal is generally S shaped.

18. The turbine section of claim 5 , wherein the carrier is formed from a metallic material.

19. The turbine section of claim 5 , wherein the seal segment is formed from a ceramic material.

20. The turbine section of claim 5 , wherein a gap is formed between the first circumferential side and the second circumferential side.