Method of replacing damaged aerofoil
A method of replacing a damaged blade ( 12 A) of an integrally bladed rotor assembly ( 10 ) including a disc ( 14 ) and a plurality of blades ( 12 ) extending outwardly from the disc ( 14 ) includes the steps of; removing the damaged blade ( 12 A) to leave a blade stub ( 16 ) projecting from the disc ( 14 ); depositing a collar ( 22 ) of metal around the blade stub ( 16 ) at a position physically separated from the disc ( 14 ); attaching a replacement blade ( 12 B) to the stub ( 16 ) by linear friction welding; and removing the collar ( 22 ). A body ( 20 ) of a material may be deposited between the disc ( 14 ) and the collar ( 22 ) to protect the disc ( 14 ) from damage.
1. A method of replacing a damaged blade of an integrally bladed rotor assembly including a disc and a plurality of blades extending outwardly from the disc, the method including the steps of:
removing the damaged blade to leave a blade stub projecting from the disc;
depositing a body of material around the blade stub adjacent to the disc;
forming a collar of metal around the blade stub at a position that is physically seperated from the disc by depositing a molten metal, wherein the material of the body is different from that collar;
attaching a replacement blade to the stub by linear friction welding; and removing the collar.
2. A method according to claim 1 wherein the rotor assembly includes an original weld plane defining the position where a blade was welded to the disc and the damaged blade is removed radially outwards of the original weld plane.
3. A method according to claim 2 wherein the collar surrounds the original weld plane.
4. A method according to claim 1 wherein the metal is deposited by shaped metal deposition, plasma, laser powder, or laser wire deposition.
5. A method according to claim 1 wherein the collar is annular and includes a central opening through which the blade stub passes.
6. A method according to claim 1 in which the material of the body is a polymer or heat resistant coating.
7. A method according to claim 1 in which the body of material is deposited before the deposition of molten metal forming the collar.
8. A method according to claim 1 in which the metal forming the collar is deposited onto the body of material such that it sandwiches the body of material between itself and the disc.
9. A method according to claim 1 in which the linear friction welding process involves oscillating the blade tangentially relative to the disc.
10. A method according to claim 1 in which the collar is removed by machining.
11. A method according to claim 1 in which the resulting blade has substantially the same shape as the original blade.
12. A method according to claim 1 , wherein the metal comprises a low melting point alloy.
13. A method according to claim 1 , wherein the metal comprises a bismuth alloy.
14. A method of replacing a damaged blade of an integrally bladed rotor assembly including a disc and a plurality of blades extending outwardly from the disc, the method including the steps of:
removing the damaged blade to leave a blade stub projecting from the disc;
forming a collar of metal around the blade stub at a position that is physically separated from the disc by depositing a molten metal;
depositing a body of material around the blade stub adjacent to the disc, said material being different from that of the collar;
attaching a replacement blade to the stub by linear friction welding;
and removing the collar,
wherein the body of material is deposited before the deposition of the collar.
15. A method of replacing a damaged blade of an integrally bladed rotor assembly including a disc and a plurality of blades extending outwardly from the disc, the method including the steps of:
removing the damaged blade to leave a blade stub projecting from the disc;
forming a collar of metal around the blade stub at a position that is physically separated from the disc by depositing a molten metal;
depositing a body of material around the blade stub adjacent to the disc, said material being different from that of the collar;
attaching a replacement blade to the stub by linear friction welding;
and removing the collar,
wherein the body of material is deposited before the deposition of the metal to form the collar such that the body of material is sandwiched between the collar and the disc.
16. A method of replacing a damaged blade of an integrally bladed rotor assembly including a disc and a plurality of blades extending outwardly from the disc, the method including the steps of:
removing the damaged blade to leave a blade stub projecting from the disc;
depositing a body of material around the blade stub adiacent to the disc;
forming a collar of metal around the blade stub at a position that is physically separated from the disc by depositing a molten metal by shaped metal deposition, plasma, laser powder, or laser wire deposition, wherein the material of the body is different from that of the collar;
attaching a replacement blade to the stub by linear friction welding; and removing the collar.