Segmented compressor inner band for variable vanes in gas turbine engines
US-2024280032-A1 · Aug 22, 2024 · US
US2016010488A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016010488-A1 |
| Application number | US-201514792941-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jul 7, 2015 |
| Priority date | Jul 8, 2014 |
| Publication date | Jan 14, 2016 |
| Grant date | — |
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The present invention relates to a wear protection arrangement for a turbomachine, comprising at least one adjustable guide vane, a casing in which the guide vane is arranged in an adjustable manner, an inner ring, made from a metallic material, in or on which the guide vane is arranged in an adjustable manner, a first gap between an inner guide vane tab and the inner ring and a second gap between an outer guide vane tab and the casing, at least one wear protection coating, wherein the wear protection coating(s) is/are connected to the inner ring and/or to the inner guide vane tab and the wear protection coating(s) forms or form the first gap, at least in certain regions, and/or the wear protection coating(s) is/are connected to the casing and/or to the outer guide vane tab and the wear protection coating(s) forms/form the second gap, at least in certain regions. The invention further relates to a method for applying an abradable wear protection coating and for applying an abrasive wear protection coating and to a compressor for a turbomachine having a wear protection arrangement.
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1 .- 14 . (canceled) 15 . A wear protection arrangement for a turbomachine, wherein the arrangement comprises at least one adjustable guide vane, a casing in which the at least one guide vane is arranged in an adjustable manner, an inner ring made from a metallic material, in or on which ring the at least one guide vane is arranged in an adjustable manner, a first gap between an inner guide vane tab and the inner ring and a second gap between an outer guide vane tab and the casing, one or more wear protection coatings connected to the inner ring and/or to the inner guide vane tab and forming the first gap, at least in certain regions, and/or one or more wear protection coatings connected to the casing and/or to the outer guide vane tab and forming the second gap, at least in certain regions. 16 . The wear protection arrangement of claim 15 , wherein the one or more wear protection coatings are abradable or abrasive. 17 . The wear protection arrangement of claim 16 , wherein the one or more wear protection coatings are abradable. 18 . The wear protection arrangement of claim 16 , wherein the one or more wear protection coatings are abrasive. 19 . The wear protection arrangement of claim 17 , wherein the one or more wear protection coatings are or comprise a porous metal matrix. 20 . The wear protection arrangement of claim 19 , wherein the metal matrix comprises at least one of aluminum, an aluminum-silicon alloy, nickel, a nickel-chromium-aluminum alloy. 21 . The wear protection arrangement of claim 19 , wherein a pore fraction of the porous metal matrix is from 3% to 35%. 22 . The wear protection arrangement of claim 20 , wherein a pore fraction of the porous metal matrix is from 3% to 35%. 23 . The wear protection arrangement of claim 17 , wherein the wear protection coating comprises a porous metal matrix and a solid lubricant. 24 . The wear protection arrangement of claim 23 , wherein the metal matrix comprises at least one of aluminum, an aluminum-silicon alloy, nickel, a nickel-chromium-aluminum alloy. 25 . The wear protection arrangement of claim 23 , wherein a pore fraction of the porous metal matrix is from 3% to 35%. 26 . The wear protection arrangement of claim 24 , wherein a pore fraction of the porous metal matrix is from 3% to 35%. 27 . The wear protection arrangement of claim 17 , wherein the wear protection coating has a thickness of from 0.1 mm to 2 mm. 28 . The wear protection arrangement of claim 18 , wherein the wear protection coating comprises a carbidic, nitridic and/or carbonitridic material. 29 . The wear protection arrangement of claim 18 , wherein the wear protection coating has a composition represented by (M1) a (M2) b N c C d , wherein N is nitrogen and C is carbon, M1 and M2 comprise at least one of aluminum, titanium, zirconium, chromium, tungsten, and the stoichiometric factors a, b, c, d are each zero, one, two, three or four, at least one of a, b, c, d being greater than zero. 30 . The wear protection arrangement of claim 29 , wherein the one or more wear protection coatings comprise one or more layers, multiple layers having the same or different compositions (M1) a (M2) b N c C d . 31 . The wear protection arrangement of claim 29 , wherein the one or more wear protection coatings comprise at least one metal matrix with embedded particles, which particles having a composition represented by (M1) a (M2) b N c C d , wherein N is nitrogen and C is carbon, M1 and M2 comprise at least one or aluminum, titanium, zirconium, chromium, tungsten, and the stoichiometric factors a, b, c, d are each zero, one, two, three or four, at least one of a, b, c, d being greater than zero. 32 . A method for applying one or more abradable wear protection coatings to the inner ring and/or the casing of the wear protection arrangement of claim 17 , wherein the method comprises applying the one or more wear protection coatings by thermal spraying. 33 . A method for applying one or more abrasive wear protection coatings to the inner guide vane tab and/or to the outer guide vane tab of the wear protection arrangement of claim 18 , wherein the method comprises applying the one or more wear protection coatings by thermal spraying, physical vapor deposition (PVD) or chemical vapor deposition (CVD). 34 . A compressor for a turbomachine, wherein the compressor comprises at least one wear protection arrangement according to claim 15 .
by means of nozzle vanes · CPC title
Coating · CPC title
Nitrides · CPC title
Aluminium alloys, e.g. AlCuMgPb · CPC title
Coating; Surface treatment · CPC title
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