IP Library Granted Patent US 10,100,651
Granted Patent B2
US 10,100,651 · App. 15/115,917 · Granted Oct 16, 2018

Wear resistance of a high-temperature component imparted by a cobalt coating

Inventors: Bernd Burbaum (Falkensee, DE); Britta Laux (Berlin, DE)
Assignee: SIEMENS AKTIENGESELLSCHAFT
F01D5/288B32B7/02B32B9/005B32B9/041B32B15/01B32B15/013B32B15/017B32B15/043B32B15/18B32B15/20F01D5/282B32B2307/552B32B2603/00F05D2220/30F05D2240/24F05D2300/175
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Quick Facts
Patent No.
US 10,100,651
App. No.
15/115,917
Granted
Oct 16, 2018
Kind
B2
Abstract

A coated high-temperature component including a cobalt coating that has a higher carbon content is provided. A layer composed of a cobalt-based alloy is applied which is known as or is similar to substrate material, to the region of the component which is subject to the wear, wherein the component preferably comprises a nickel-based alloy as substrate material, the carbon content of which is lower than that of the cobalt-based alloy. At the high operating temperatures, carbon diffuses from the coating into the base material; this is normally undesirable, but here leads to a higher carbide proportion in the substrate and therefore to a higher hardness and therefore to an increased wear resistance.

Claims (33)

1. A component comprising:

a metallic substrate,

wherein the metallic substrate is a nickel-based superalloy or a cobalt-based superalloy, and

wherein the metallic substrate has a first carbon content; and

a layer composed of a cobalt-based alloy,

wherein the layer is applied directly to a region of the metallic substrate having increased wear and wherein the layer has a thickness of 1 μm to 100 μm,

wherein the cobalt-based alloy of the layer comprises at least chromium, nickel, and tungsten, and at least one substance selected from the group consisting of: tantalum, aluminum, and titanium,

wherein the cobalt-based alloy fails to include rhenium and fails to include yttrium,

wherein the layer has a second carbon content that is greater than the first carbon content of the metallic substrate, and

wherein the metallic substrate is coated with a metallic coating and/or a ceramic coating on the metallic coating, which adjoin the region of the metallic substrate having the increased wear, and

wherein the metallic coating comprises no carbon and wherein the metallic coating comprises NiCoCrAl, NiCoCrAlY, NiCoCrAlTa, NiCoCrAlFe, NiCoCrAlYFe, NiCoCrAlYFeTa, NiCoCrAlFeTa, or NiCoCrAlYTa, wherein the layer is at least 10% thinner than the metallic coating of the metallic substrate.

2. The component as claimed in claim 1 , wherein the region of the metallic substrate represents a flat, planar tip.

3. The component as claimed in claim 1 , wherein the region of the metallic substrate represents a tip with a freestanding wall.

4. The component as claimed in claim 1 , wherein an absolute difference in the first carbon content of the metallic substrate and the second carbon content of the layer is at least 0.03% by weight.

5. The component as claimed in claim 1 , wherein the metallic substrate is directionally solidified in columnar form and is solidified in single-crystal form.

6. The component as claimed in claim 1 , wherein the layer at most partially overlaps the metallic coating of the metallic substrate.

7. The component according to claim 1 , wherein after 100 hours of operation at 1173-1223 Kelvin, at least a portion of the second carbon content diffuses from the layer into the metallic substrate.

8. A component comprising:

a substrate having a first carbon content,

wherein the substrate is a nickel-based superalloy or a cobalt-based superalloy, and

wherein a metallic coating is applied to lateral faces of the substrate; and

a layer composed of a cobalt-based alloy, wherein the cobalt-based alloy fails to include rhenium and fails to include yttrium,

wherein the layer is applied directly to a tip region of the substrate, the tip region including a first outer freestanding wall and a second outer freestanding wall surrounding a recess, further wherein the layer is applied to the entirety of the tip region including the recess, and

wherein the layer has a second carbon content that is greater than the first carbon content of the substrate.

9. The component of claim 8 ,

wherein the nickel-based superalloy of the substrate comprises at least chromium, cobalt, tungsten, aluminum, titanium, and tantalum,

wherein the nickel-based superalloy of the substrate contains no rhenium and no yttrium,

wherein the cobalt-based alloy of the layer comprises at least chromium, nickel, and tungsten, and at least one substance selected from the group consisting of: tantalum, aluminum, and titanium.

10. The component of claim 8 , wherein the layer at most partially overlaps the metallic coating of the substrate.

11. The component of claim 8 , wherein the layer is at least 10% thinner than the metallic coating of the substrate.

12. The component of claim 8 , wherein the layer has a thickness of 1 μm to 100 μm.

13. The component of claim 12 , wherein the metallic coating comprises NiCoCrAl, NiCoCrAlY, NiCoCrAlTa, NiCoCrAlFe, NiCoCrAlYFe, NiCoCrAlYFeTa, NiCoCrAlFeTa, or NiCoCrAlYTa.

14. The component of claim 8 , wherein the metallic coating comprises no carbon.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 21, 2021
From: SIEMENS AKTIENGESELLSCHAFT
To: SIEMENS ENERGY GLOBAL GMBH & CO. KG
Reel/Frame 055997/0014 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 2, 2016
From: BURBAUM, BERND; LAUX, BRITTA
To: SIEMENS AKTIENGESELLSCHAFT
Reel/Frame 039308/0881 →
Priority Claims (1)
DE 10 2014 202 457 · Feb 11, 2014 · national
Continuity (1)
Related Publication 20170175553A1 · Jun 22, 2017