Wear protection arrangement for a turbomachine, process and compressor

US2016010488A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016010488-A1
Application numberUS-201514792941-A
CountryUS
Kind codeA1
Filing dateJul 7, 2015
Priority dateJul 8, 2014
Publication dateJan 14, 2016
Grant date

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

Official abstract text for this publication.

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.

First claim

Opening claim text (preview).

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 .

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What does patent US2016010488A1 cover?
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 betw…
Who is the assignee on this patent?
MTU Aero Engines AG
What technology area does this patent fall under?
Primary CPC classification F01D17/16. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Jan 14 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).