Blade outer air seal with face seal
A blade outer air seal includes a carrier, a ceramic seal segment, and a face seal. The ceramic seal segment is supported on the carrier and has first and second axial ends, first and second circumferential sides, an inner side, and an outer side. The face seal is carried on the ceramic seal segment at the first axial end. The face seal has a radial seal wall and a tongue that extends axially from the radial seal wall.
1. A blade outer air seal comprising:
a carrier;
a ceramic seal segment supported on the carrier, the ceramic seal segment having first and second axial ends, first and second circumferential sides, an inner side, an outer side, and first and second inward-facing dovetail hooks that project from the outer side; and
a face seal carried on the ceramic seal segment at the first axial end, the face seal having a radial seal wall and a tongue extending axially from the radial seal wall and between the first and second inward-facing dovetail hooks.
2. The blade outer air seal as recited in claim 1 , wherein the face seal is coextensive with the first axial end of the ceramic seal segment.
3. The blade outer air seal as recited in claim 2 , wherein the tongue is non-coextensive with the radial seal wall.
4. The blade outer air seal as recited in claim 1 , wherein the tongue is carried on the outer side of the ceramic seal segment.
5. The blade outer air seal as recited in claim 1 , wherein the first axial end of the ceramic seal segment includes an axial slot, and the tongue extends into the axial slot.
6. The blade outer air seal as recited in claim 1 , wherein the face seal is spring-loaded.
7. The blade outer air seal as recited in claim 1 , further comprising an inter-segment seal arranged along one of the first and second circumferential sides of the ceramic seal segment, wherein the carrier includes an axial stop, and the axial stop and the face seal limit axial movement of the inter-segment seal.
8. The blade outer air seal as recited in claim 7 , wherein the radial seal wall includes a retainer arm adjacent the tongue, and the retainer arm limits axial movement of the inter-segment seal.
9. The blade outer air seal as recited in claim 1 , wherein the ceramic seal segment is axially receivable onto the carrier.
10. A blade outer air seal comprising:
a carrier;
a ceramic seal segment supported on the carrier, the ceramic seal segment having first and second axial ends, first and second circumferential sides, an inner side, and an outer side, the ceramic seal segment being axially receivable onto the carrier;
a face seal carried on the ceramic seal segment at the first axial end; and
an inter-segment seal arranged along one of the first and second circumferential sides, the face seal limiting axial movement of the inter-segment seal.
11. The blade outer air seal as recited in claim 10 , wherein the carrier includes an axial stop opposite the face seal, wherein the face seal and the axial stop limit axial movement of the inter-segment seal.
12. The blade outer air seal as recited in claim 10 , wherein the face seal includes a radial seal wall that has an axially-facing surface, a tongue that projects axially from the radial seal wall, the radial seal wall includes a retainer arm adjacent the tongue, and the retainer arm limits axial movement of the inter-segment seal.
13. The blade outer air seal as recited in claim 12 , wherein the first axial end of the ceramic seal segment includes an axial slot, and the tongue extends into the axial slot.
14. The blade outer air seal as recited in claim 12 , wherein the tongue is non-coextensive with the radial seal wall.
15. The blade outer air seal as recited in claim 14 , wherein the radial seal wall is coextensive with the first axial end of the ceramic seal segment.
16. The blade outer air seal as recited in claim 12 , wherein the ceramic seal segment includes first and second inward-facing dovetail hooks that project from the outer side, and the tongue is carried on the outer side of the ceramic seal segment and extends between the first and second inward-facing dovetail hooks.
17. A gas turbine engine comprising:
a compressor section;
a combustor in fluid communication with the compressor section; and
a turbine section in fluid communication with the combustor,
the turbine section including a plurality of blade outer air seals, each said blade outer air seal comprising:
a carrier,
a ceramic seal segment supported on the carrier, the ceramic seal segment having first and second axial ends, first and second circumferential sides, a radially inner side, and a radially outer side, and
a face seal carried on the ceramic seal segment at the first axial end, the face seal having a radial seal wall and a tongue extending axially from the radial seal wall the tongue being radially trapped between the carrier and the radially outer side of the ceramic seal segment.
18. The engine as recited in claim 17 , wherein the face seal is coextensive with the first axial end of the ceramic seal segment.
19. The engine as recited in claim 18 , wherein the tongue extends between first and second inward-facing dovetail hooks of the ceramic seal segment.