NiCoCrAl BASED ALLOY, A POWDER, A COATING AND A COMPONENT

Abstract

A Nickel-based alloy which includes (in wt %): Cobalt (Co) 27.0%-29.0%; Chrome (Cr) 16.0%-18.0%; Aluminum (Al) 11.6%-12.6%; Yttrium (Y) 0.3%-0.5%; Iron (Fe) 4.0%-5.0%; optionally Tantalum (Ta) 0.6%-0.8%; Molybdenum (Mo) 0.4%-0.6%; Silicon (Si) 0.4%-0.6%; and the rest Nickel (Ni).

Description

FIELD OF INVENTION

The invention relates to a composition of a NiCoCrAl based alloy, especially used for gas turbines, a powder, a coating and a component.

BACKGROUND OF INVENTION

When further increasing engine efficiency, output power, availability and reliability in current gas turbine development, it is often limited by temperature capacity and lifetime of protective coatings for protection against hot corrosion and oxidation and by bonding thermal barrier coating (TBC) on hot turbine components.

The currently used coatings hardly fulfill demands of further turbine development. On the other hand, they are either too expensive due to large amount of the expensive element Rhenium (Re). Looking at the recent development of NiCoCrAl based coating coatings worldwide, all focus are on adding a large amount of rear earth elements or precious metals such as Gd, La, Pt etc. in the coatings to achieve a higher temperature capacity and longer lifetime.

This trend is conflicting with the dramatic price increase of the elements in the market.

In NiCoCrAlY based coatings available today, one relies on Yttrium (Y) incorporation very much to have pegging and scavenge effects to increase oxidation and corrosion resistances of the coatings.

However, it has recently been reported that Yttrium oxide inclusions in the protective aluminum oxide scale on top of MCrAlY provide fast oxygen diffusion routes, and therefore, accelerate oxidation of the coating (Nijdam T J, Sloof W G. Acta Materialia 2007; 55:5980).

High Sulfur content >10ppm existed in the current MCrAlY shortens coating lifetime (Smialek J L, Jayne D T, Schaeffer J C, Murphy W H. Thin Solid Films 1994; 253:285; and Smialek J L. Metallurgical Transactions A, Physical Metallurgy and Materials Science 1991; 22A:739).

This problem has not been solved yet.

SUMMARY OF INVENTION

It is therefore an aim of the invention to overcome the problems mentioned above.

The problem is solved by an alloy, by a powder, by a coating and by a layer system.

Further advantages of the invention are listed in the dependent claims which can be combined arbitrarily with each other to yield further advantages.

DETAILED DESCRIPTION OF INVENTION

This invention is to solve the problem by using recent research results and upgraded thermodynamic modelling to design an optimized and innovative NiCoCrAlX based alloy coatings applied by means of thermal spraying in air, vacuum, or protected atmosphere, physical deposition, and plating on Nickel (Ni) or cobalt (Co) based superalloys, wherein X stands for a combination of minor elements such as Y, Si, Hf, Ta, Fe, Mo and etc..

Instead of Yttrium (Y) or partial replacement of Yttrium (Y) in the current NiCoCrAlY based coatings, other minor elements are introduced to replace partly the functions of Yttrium (Y) in order to keep Yttrium (Y) content low. The idea is also to avoid or minimize the use of the expensive elements to still meet the increased demands of today's advanced gas turbines.

Introduction of Iron (Fe) allows to stabilize the Aluminum (Al) rich phases in the microstructure or in the coating and to some extent reduces consumption rate of Aluminum (Al).

Moreover, another approach in designing and manufacturing the innovative NiCOCrAlX based coatings is to reduce Sulfur (S) content to <10ppm to further increase coating lifetime.

A coating thickness should be in the range of 30 μm to 800 μm depending on type of applications and application methods.

The new NiCoCrAlX based coating is Ni-based and possesses the following composition (in wt %): 27-29% Co, 16-18% Cr, 11.6-12.6% Al, 0.3-0.5% Y, 4.0-5.0% Fe, 0.6-0.8% Ta and optionally 0.4-0.6% Mo, 0.4-0.6% Si.

Therefore, the invention comprises NiCoCrAlYFeTa, NiCoCrAlYFeTaMo, NiCoCrAlYFeTaSi, NiCoCrAlYFeTaMoSi.

This invention results in NiCoCrAlX based coatings with a higher temperature capacity, longer life, and lower cost than the NiCoCrAlX coatings available today.

A powder with this alloy composition can be mixed with a binder and/or refractory metals or ceramics if used as an abrasive coating.

For turbine application especially a metallic substrate like a nickel or cobalt based superalloy is used on which the inventive coating is applied on.

The coating is applied especially by a thermal spray process, like APS, VPS or HVOF.

Even SLM, SLS or any AM technique is possible to apply coatings or to produce bulk components of this alloy.

A layer system at least comprises a metallic substrate, especially a Nickel based superalloy and at least a coating with the inventive alloy and optionally a ceramic layer on top the metallic bond and oxidation coating.

The ceramic layer comprises preferably a Zirconia based composition, partly or fully stabilized.

Claims

1. A Nickel-based alloy, and least comprising (in wt %), especially consisting of:

2. The Alloy according to claim 1, which comprises NiCoCrAlYFeTaMo.

3. The Alloy according to claim 1, which comprises NiCoCrAlYFeTaSi.

4. The Alloy according to claim 1, which comprises NiCoCrAlYFeTaMoSi.

5. A Powder, comprising, especially consisting of, an alloy according to claim 1, optionally comprising a binder and/or hard or ceramic particles.

6. A Coating, comprising: a composition of an alloy according to claim 1,especially having a thickness in the range of 30 μm to 800 μm.

7. A Component, comprising a metallic substrate, especially Nickel-based or Cobalt-based superalloy,a metallic coating with a composition according to claim 1,and optionallya ceramic coating above the substrate and the metallic coating.

8. The Component according to claim 7, wherein the ceramic layer comprises a Zirconia based composition, partly or fully stabilized.