Abradable composition and seal of an axial-flow turbomachine compressor casing
The invention relates to a composition for an abradable seal of a turbomachine, the composition comprising an aluminum base, nickel powder, polyester powder. The invention also relates to an outer casing of a low-pressure compressor of an axial-flow turbomachine with an abradable seal surrounding an annular row of rotor blades. The seal comprises a rounded support covered with a layer of abradable material comprising a metallic phase mainly made of aluminum and with nickel in a lesser proportion. The abradable material additionally comprises from 25% to 55% of additive, such as polyester, methyl methacrylate, hexagonal boron nitride, calcium fluoride. The support is segmented, and forms an organic matrix composite outer casing of the compressor. The invention also proposes a process for producing an abradable seal by plasma spraying an Al—Ni-polyester powder.
1. A turbomachine comprising:
a rotor;
a rounded support with an inner annular surface;
at least one coating made of abradable material covering the inner annular surface of the rounded support for cooperating by abrasion with the rotor;
wherein a composition of the abradable coating includes:
a metal phase with aluminum and nickel, the metal phase comprising, by weight, at least 50% of aluminum and between 20% and 45% of nickel; and
a filler.
2. The turbomachine in accordance with claim 1 , wherein in the abradable coating, a metal phase forms a metallic matrix which is combined with the filler.
3. The turbomachine in accordance with claim 2 , wherein the metallic matrix occupies a majority of a volume of the abradable coating.
4. The turbomachine in accordance with claim 1 , wherein the rounded support is an outer shroud, the abradable coating being on the inside of the outer shroud.
5. The turbomachine in accordance with claim 1 , wherein the rounded support is an outer casing, the abradable coating being positioned inside of the outer casing.
6. The turbomachine in accordance with claim 1 , wherein the rounded support is made of an organic matrix composite material with carbon fibres, the carbon fibres being arranged as a stack, the abradable coating comprising an interface in contact with the organic matrix composite material.
7. The turbomachine in accordance with claim 1 , wherein the rounded support comprises attachment portions, the attachment portions being positioned upstream and downstream of the abradable coating.
8. The turbomachine in accordance with claim 1 , wherein the rounded support has an upstream edge and a downstream edge, the abradable coating covering the rounded support from the upstream edge to the downstream edge.
9. The turbomachine in accordance with claim 1 , the turbomachine comprising a low-pressure compressor with at least one row of rotor blades, the abradable coating being a seal of the low-pressure compressor, which surrounds the at least one row of rotor blades.
10. The turbomachine in accordance with claim 1 , the turbomachine comprising at least one annular row of stator blades with platforms attached to the rounded support, the abradable coating being in contact with the platforms of blades.
11. The turbomachine in accordance with claim 10 , wherein the abradable coating forms a leak-tight barrier that protects the rounded support between the platforms.
12. A turbomachine comprising:
a rotor;
a rounded support with an inner annular surface supporting stator vanes with fixation platforms;
at least one coating made of abradable material covering the inner annular surface of the rounded support for cooperating by abrasion with the rotor;
wherein a composition of the abradable coating includes:
a metal phase with aluminum and nickel, the metal phase comprising, by weight, at least 50% of aluminum and between 20% and 45% of nickel; and
a filler.
13. The turbomachine in accordance with claim 12 , wherein the metal phase comprises, by weight, between 55% and 80% of aluminum.
14. The turbomachine in accordance with claim 12 , wherein the metal phase comprises, by weight, between 5% and 50% of filler.
15. The turbomachine in accordance with claim 12 , wherein the filler is mineral filler.
16. The turbomachine in accordance with claim 12 , wherein the filler comprises at least one material selected from a group consisting of hexagonal boron nitride, and calcium fluoride.
17. The turbomachine in accordance with claim 12 , wherein the filler is a polymer selected from the group consisting of polyester, methyl methacrylate.
18. A turbomachine comprising:
a rotor;
rounded support with an inner annular surface;
at least one coating made of abradable material covering the inner annular surface of the rounded support for cooperating by abrasion with the rotor;
an interlayer comprising a metal strip between the inner annular surface and the coating,
wherein a composition of the abradable coating includes:
a metal phase with aluminum and nickel, the metal phase comprising, by weight, at least 50% of aluminum and at least 20% of nickel; and
a filler, the aluminum and the nickel being in contact of the metal strip.
19. The turbomachine in accordance with claim 18 , wherein the metal strip is made of a metal sheet selected from a group consisting of steel sheet and nickel sheet.