Combination of blade tip cladding and erosion-resistant layer and method for the production thereof

Patent metadata

Field	Value
Publication number	US-2016333705-A1
Application number	US-201615149368-A
Country	US
Kind code	A1
Filing date	May 9, 2016
Priority date	May 12, 2015
Publication date	Nov 17, 2016
Grant date	—

Abstract

A method for producing a blade for a turbomachine, the blade having a blade tip cladding on its blade tip and an erosion-resistant layer at least on its blade airfoil, wherein firstly a blade tip cladding is applied on the blade tip, subsequently a poorly adhering sublayer is deposited on the blade tip cladding, and then the erosion-resistant layer is produced on the poorly adhering sublayer and the blade airfoil, the poorly adhering sublayer being removed again together with the erosion-resistant layer following completion of the erosion-resistant layer. The invention also relates to a blade for a turbomachine, the blade having a blade tip cladding on its blade tip and an erosion-resistant layer at least on its blade airfoil. The blade tip cladding comprises a metal matrix with incorporated hard material particles and an oxide layer arranged on the metal matrix.

First claim

What is claimed is:

1 . A method for producing a blade for a turbomachine, which blade comprises a blade tip cladding on its blade tip and an erosion-resistant layer at least on its blade airfoil, wherein the method comprises firstly applying a blade tip cladding on the blade tip, subsequently depositing on the blade tip cladding a poorly adhering sublayer, and thereafter forming the erosion-resistant layer on the poorly adhering sublayer and the blade airfoil, the poorly adhering sublayer being removed together with the erosion-resistant layer following completion of the erosion-resistant layer.

2 . The method of claim 1 , wherein the poorly adhering sublayer has an adhesion which is selected to be sufficiently high so that the poorly adhering sublayer is not detached before or during deposition of the erosion-resistant layer, and sufficiently low to allow for simple detachment of the poorly adhering sublayer.

3 . The method of claim 1 , wherein, as the poorly adhering sublayer, a metal layer is deposited on an oxide layer produced beforehand on the blade tip cladding.

4 . The method of claim 3 , wherein the oxide layer is produced electrolytically by anodic oxidation of the blade tip cladding.

5 . The method of claim 3 , wherein the poorly adhering sublayer is produced by electrodeposition of metal.

6 . The method of claim 5 , wherein the metal comprises nickel.

7 . The method of claim 4 , wherein the poorly adhering sublayer is produced by electrodeposition of metal.

8 . The method of claim 1 , wherein the blade tip cladding is produced by electrodeposition of a nickel matrix with incorporated hard material particles.

9 . The method of claim 8 , wherein the hard particles comprise particles of boron nitride.

10 . The method of claim 1 , wherein the erosion-resistant layer is deposited by physical vapor deposition.

11 . The method of claim 10 , wherein the erosion-resistant layer is deposited by evaporation coating.

12 . The method of claim 1 , wherein the blade is cleaned before the deposition of the erosion-resistant layer.

13 . The method of claim 12 , wherein the blade is cleaned by sputtering.

14 . The method of claim 1 , wherein the erosion-resistant layer deposited on the blade tip cladding is mechanically removed with the poorly adhering sublayer after deposition of the erosion-resistant layer.

15 . The method of claim 14 , wherein the erosion-resistant layer deposited on the blade tip cladding is mechanically removed with the poorly adhering sublayer during cleaning of the blade.

16 . A blade for a turbomachine, wherein the blade comprises a blade tip cladding on its blade tip and an erosion-resistant layer at least on its blade airfoil, the blade tip cladding comprising a metal matrix with incorporated hard material particles and an oxide layer being arranged on the metal matrix.

17 . The blade of claim 16 , wherein the oxide layer has a thickness of less than or equal to 0.1 μm.

18 . The blade of claim 16 , wherein the oxide layer has a thickness of less than or equal to 50 nm.

19 . The blade of claim 16 , wherein the oxide layer has a thickness of less than or equal to 10 nm.

20 . The blade of claim 16 , wherein the blade tip cladding is surrounded by the erosion-resistant layer and/or is embedded therein.

Assignees

• MTU Aero Engines AG

Inventors

• Uihlein Thomas
• Linska Josef
• Stolle Ralf

Classifications

• F05D2300/16

  Other metals not provided for in groups F05D2300/11 - F05D2300/15 · CPC title

• F05D2300/6032

  Metal matrix composites [MMC] · CPC title

• F05D2230/313

  by physical vapour deposition · CPC title

• F05D2240/307

  related to the tip of a rotor blade · CPC title

• F01D11/122

  with erodable or abradable material (blades having cutting or grinding tips F01D5/20) · CPC title