CMC BOAS arrangement
A blade outer air seal assembly includes a support structure. A blade outer air seal has a plurality of segments that extend circumferentially about an axis and mounted in the support structure via a carrier. At least one of the plurality of segments has a base portion that extends between a first circumferential side and a second circumferential side and from a first axial side to a second axial side. A first hook extends from the base portion near the first axial side and faces towards the second axial side. A second hook extends from the base portion near the second axial side and faces towards the first axial side. A slot is in the second hook configured to receive a pin.
1. A blade outer air seal assembly, comprising:
a support structure;
a blade outer air seal having a plurality of segments extending circumferentially about an axis and mounted in the support structure via a carrier, wherein the carrier has a platform and a carrier hook; and
at least one of the plurality of segments 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 near the first axial side and facing towards the second axial side and a second hook extending from the base portion near the second axial side and facing towards the first axial side, and a slot in the second hook; and
a pin extends radially through a hole in the carrier hook and the slot, wherein the pin has a first diameter and a second diameter smaller than the first diameter, the first diameter engaged with the hole on the carrier and the second diameter engaged with the slot and the first diameter is radially outward of the second diameter.
2. The blade outer air seal assembly of claim 1 , wherein the carrier platform is engaged with the first and second hooks.
3. The blade outer air seal assembly of claim 2 , wherein the platform is engaged with the first and second hooks for at least half of a circumferential width of the base portion.
4. The blade outer air seal assembly of claim 2 , wherein an intersegment seal is arranged in the platform.
5. The blade outer air seal assembly of claim 1 wherein the hole extends through the platform and the carrier hook.
6. The blade outer air seal assembly of claim 1 , wherein the pin is a split pin.
7. The blade outer air seal assembly of claim 1 , wherein the pin has a diameter between 0.125 and 0.250 inches (3.175-6.35 mm).
8. The blade outer air seal assembly of claim 1 , wherein at least one scallop is machined into the first hook and configured to receive a portion of a vane structure or the support structure.
9. The blade outer air seal assembly of claim 1 , wherein the first hook is formed having a first radius of curvature, and the second hook is formed having a second radius of curvature different from the first radius of curvature.
10. The blade outer air seal assembly of claim 9 , wherein the second radius of curvature is less than 3 inches smaller than the first radius of curvature.
11. The blade outer air seal assembly of claim 1 , wherein the carrier is formed from a metallic material.
12. The blade outer air seal assembly of claim 1 , wherein the blade outer air seal is formed from a ceramic material.
13. 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, wherein the carrier has a first carrier hook that is engaged with the support structure;
at least one 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 near the first axial side and facing towards the second axial side and a second hook extending from the base portion near the second axial side and facing towards the first axial side; and
a pin extending radially through a hole in the carrier hook and a slot on the seal segment, wherein the pin has a first diameter and a second diameter smaller than the first diameter, the first diameter engaged with the hole on the carrier and the second diameter engaged with the slot and the first diameter is radially outward of the second diameter.
14. The turbine section of claim 13 , wherein the carrier has an axially extending platform that is configured to engage the first and second hooks.
15. The turbine section of claim 13 , wherein the pin has a first diameter and a second diameter smaller than the first diameter, the first diameter engaged with a hole on the carrier and the second diameter engaged with the slot.
16. The turbine section of claim 13 , wherein the carrier is formed from a metallic material.
17. The turbine section of claim 13 , wherein the seal segment is formed from a ceramic material.
18. A method of assembling a blade outer air seal assembly, comprising:
providing a 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 near the first axial side and facing towards the second axial side and a second hook extending from the base portion near the second axial side and facing towards the first axial side;
assembling the seal segment onto a carrier in a circumferential direction wherein the carrier has a first carrier hook; and
inserting a pin in a radial direction into a hole in the first carrier hook and a slot on the seal segment, wherein the pin has a first diameter and a second diameter smaller than the first diameter, the first diameter engaged with the hole on the carrier and the second diameter engaged with the slot and the first diameter is radially outward of the second diameter.