Sealing assembly
A sealing assembly ( 100 ) for at least partially sealing a gap ( 102 ) leading to a void ( 104 ) between first and second members ( 110, 120 ), the first and second members forming part of a gas-washed surface of a jet engine, wherein the sealing assembly comprises: a bridging portion ( 130 ) couplable to one of the first and second members and movable to engage the other of the first and second members so as to block off the void between the first and second members from the gas-washed surface.
1. A sealing assembly for at least partially sealing a gap leading to a void between first and second members, the first and second members forming part of a gas-washed surface of a gas turbine, wherein the sealing assembly comprises:
a bridging portion couplable to one of the first and second members and engaging the other of the first and second members so as to block off the void between the first and second members from the gas-washed surface,
the bridging portion being adapted to have a movable configuration in which relative movement between at least a part of the bridging portion and the other of the first and second members is permitted and a permanent locked configuration in which relative movement between the at least a part of the bridging portion and the other of the first and second members is prevented, wherein in the locked configuration the bridging portion is locked by a cured filler that directly contacts the first and second members and the bridging portion.
2. A sealing assembly as claimed in claim 1 , wherein the bridging portion is slidably coupled to the first member such that the bridging portion is slidably movable to engage the second member.
3. A sealing assembly as claimed in claim 2 , wherein the bridging portion comprises a groove for receiving a corresponding tongue in the first member, the groove being arranged such that the bridging portion is slidably movable to engage the second member.
4. A sealing assembly as claimed in claim 2 , wherein the bridging portion comprises a tongue for insertion into a corresponding groove in the first member, the tongue being arranged such that the bridging portion is slidably movable to engage the second member.
5. A sealing assembly as claimed in claim 2 , wherein the bridging portion comprises first and second ends for insertion into corresponding grooves in the first member, the ends being arranged such that the bridging portion is slidably movable to engage the second member.
6. A sealing assembly as claimed in claim 1 , wherein the bridging portion is integral to the first member.
7. A sealing assembly as claimed in claim 1 , wherein the bridging portion is flexible.
8. A sealing assembly as claimed in claim 7 , wherein the bridging portion comprises a plurality of bristles.
9. A sealing assembly as claimed in claim 1 , wherein the bridging portion is slidably disposed about a perimeter of the second member.
10. A sealing assembly as claimed in claim 9 , wherein the bridging portion comprises a shoulder adapted to receive a corresponding shoulder in the first member.
11. A sealing assembly as claimed in claim 1 , wherein the first and second members are movable relative to each other.
12. A gas turbine comprising a sealing assembly as claimed in claim 1 .
13. A method of installing a sealing assembly for at least partially sealing a gap leading to a void between first and second members, the first and second members forming part of a gas-washed surface of a gas turbine, wherein the method comprises:
providing a bridging portion coupled to one of the first and second members, the bridging portion being adapted to have a movable configuration in which relative movement between at least a part of the bridging portion and the other of the first and second members is permitted and a permanent locked configuration in which relative movement between the at least a part of the bridging portion and the other of the first and second members is prevented, applying a filler directly to the first and second members and the bridging portion and curing the filler to put the bridging portion into its locked configuration.
14. A method according to claim 13 , wherein the filler is applied to the first and second members.
15. A sealing assembly according to claim 14 , wherein the first member is a vane and the second member is an infill panel.
16. A sealing assembly according to claim 14 , wherein the bridging portion is a foamed material.
17. A sealing assembly according to claim 1 , wherein the first member is a vane and the second member is an infill panel adjacent to the vane.
18. A sealing assembly according to claim 17 , wherein the bridging portion is a foamed material.