Blade outer air seal with centrally mounted seal arc segments
View Patent ↗A seal system includes a segmented annular seal support that has carriage arc segments arranged circumferentially in circumferential carriage joints, and a segmented annular seal that includes seal arc segments arranged end-to-end in circumferential seal joints. The circumferential seal joints are circumferentially offset from the circumferential carriage joints.
1. A seal system comprising:
a segmented annular seal support including carriage arc segments arranged circumferentially in circumferential carriage joints; and
a segmented annular seal including seal arc segments arranged end-to-end in circumferential seal joints, wherein the circumferential seal joints are circumferentially offset from the circumferential carriage joints,
wherein each of the carriage arc segments includes respective circumferential carriage ends and a respective support member circumferentially intermediate the respective circumferential carriage ends, the support member radially supporting two of the seal arc segments, and each of the carriage arc segments includes a respective spring member on the respective support member radially biasing both of the two of the seal arc segments.
2. The seal system as recited in claim 1 , wherein the segmented annular seal support includes a number X of the carriage arc segments, the segmented annular seal includes a number Y of the seal arc segments, and the number X equals the number Y.
3. The seal system as recited in claim 1 , wherein each circumferential seal joint is approximately circumferentially centered between two of the circumferential carriage joints.
4. The seal system as recited in claim 1 , wherein the support member supports each of the two of the seal arc segments in a respective ramped interface such that each of the two of the seal arc segments is circumferentially moveable.
5. The seal system as recited in claim 1 , wherein each of the carriage arc segments includes a radially inner side wall, first and second axial side walls that extend radially-outwardly from the radially inner side wall, and a third axial side wall that extends radially-inwardly from the radially inner side wall.
6. The seal system as recited in claim 5 , wherein the radially inner side wall defines a periphery and rails located at the periphery.
7. The seal system as recited in claim 5 , wherein the first and second axial side walls include at least one hook support.
8. The seal system as recited in claim 1 , wherein the circumferential offset between the circumferential seal joints and the circumferential carriage joints define tortuous passages between a radially inner side of the segmented annular seal and a radially outer side of the segmented annular seal support.
9. The seal system as recited in claim 1 , wherein the spring member includes first and second arms that extend in opposed circumferential directions from a central spring portion, the first arm radially biasing one of the two of the seal arc segments and the second arm radially biasing the other the two seal arc segments.
10. The seal system as recited in claim 9 , wherein the central spring portion is concentric with the support member.
11. A gas turbine engine comprising:
a rotor section including a rotor having a plurality of blades and at least one annular seal system circumscribing the rotor, the annular seal assembly comprising:
a segmented annular seal support including carriage arc segments arranged circumferentially in circumferential carriage joints, and
a segmented annular seal including seal arc segments arranged end-to-end in circumferential seal joints, wherein the circumferential seal joints are circumferentially offset from the circumferential carriage joints,
wherein each of the carriage arc segments includes respective circumferential carriage ends and a respective support member circumferentially intermediate the respective circumferential carriage ends, the support member radially supporting two of the seal arc segments, and each of the carriage arc segments includes a respective spring member on the respective support member radially biasing both of the two of the seal arc segments.
12. The gas turbine engine as recited in claim 11 , wherein the segmented annular seal support includes a number X of the carriage arc segments, the segmented annular seal includes a number Y of the seal arc segments, and the number X equals the number Y.
13. The gas turbine engine as recited in claim 11 , wherein each circumferential seal joint is approximately circumferentially centered between two of the circumferential carriage joints.
14. The gas turbine engine as recited in claim 11 , wherein the support member supports each of the two of the seal arc segments in a respective ramped interface such that each of the two of the seal arc segments is circumferentially moveable.
15. The gas turbine engine as recited in claim 11 , wherein the spring member includes first and second arms that extend in opposed circumferential directions from a central spring portion, the first arm radially biasing one of the two of the seal arc segments and the second arm radially biasing the other the two seal arc segments.
16. The gas turbine engine as recited in claim 15 , wherein the central spring portion is concentric with the support member.
17. A method of assembling a seal system, the method comprising:
mounting a segmented annular seal support in a gas turbine engine, the segmented annular seal support including carriage arc segments arranged circumferentially in circumferential carriage joints; and
mounting a segmented annular seal into the engine, the segmented annular seal including seal arc segments arranged end-to-end in circumferential seal joints, wherein the mounting includes axially inserting each of the seal arc segments into the segmented annular seal support such that the circumferential seal joints are circumferentially offset from the circumferential carriage joints,
wherein each of the carriage arc segments includes respective circumferential carriage ends and a respective support member circumferentially intermediate the respective circumferential carriage ends, the support member radially supporting two of the seal arc segments, and
radially biasing both of the two of the seal arc segments using a spring on the support member.
18. The method as recited in claim 17 , wherein the axial inserting includes moving each of the seal arc segments into the segmented annular seal until the seal arc segment abuts adjacent axial side walls of two of the carriage arc segments.
19. The method as recited in claim 17 , wherein the mounting of the segmented annular seal support in the gas turbine engine includes hanging each of the carriage arc segments on a case structure of the gas turbine engine.