The invention relates to an aluminum-containing protective layer to protect against corrosion and erosion.
Compressor blades of stationary GTs and aircraft turbines are usually produced on the basis of heat-treated martensitic 12%-13% Cr steels and sometimes of precipitation-hardened 16%-17% Cr steels. As protection against corrosion, the blades of the front stages are protected by means of a special aluminum pigment-containing high-temperature surface coating.
The disadvantage of this coating is the relatively low erosion resistance of the layer. As a consequence thereof, not only a very complicated filtering of the air but often also a regular recoating of the blades (in the course of refurbishment) are necessary.
To solve this problem, the protective layers used to date are inspected at regular intervals for erosion damage and corrosion protection and in the course of refurbishment removal of the coating with subsequent recoating of the blades with the same system are carried out. The length of these time intervals is greatly dependent on the ambient air and the effectiveness of filter devices.
This problem is to be solved.
The object is achieved by a layer system as claimed in claim 1.
The refurbishment intervals could be lengthened by increasing the erosion resistance of the coating.
In the dependent claims, further advantageous measures which can be combined with one another in any way to achieve further advantages are listed.
The figures and the description present only examples of the invention.
Preference is given to the harder aluminum-containing particles AL* in a layer 7′ (
The single layer 7″ can, proceeding from
This likewise applies to a single layer 7′″ as per
To increase the erosion resistance, proceeding from
A further example of the invention comprises introducing aluminum into both layers (
Depending on the field of application, hard material particles H can be incorporated in the lower layers 7″ and 7″′ and in the upper layer 10′, 10″ as per
In addition, the upper layer can be provided with soft aluminum particles Al, harder, aluminum-containing particles AL* and/or hard material particles H or the upper layer 10IV can comprise only soft aluminum particles composed of aluminum or the upper layer 10V comprises both hard material particles H and relatively hard aluminum-containing particles AL*.
In
In
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Proceeding from
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The hardest erosion protection is formed by an upper layer 10V in which relatively hard aluminum particles AL* and hard material particles are present, with, depending on the field of application and degree of erosion protection, relatively hard aluminum particles AL* being present in the lower layer 7′ (
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In
In
In less erosive environments, the upper layer 10IV can, in comparison to
In particular, the outer layer is protected against erosion by the upper layer 10V comprising aluminum-containing relatively hard particles AL* and hard material particles H (
In
As hard material particles H, it is possible to use ceramic particles, preferably aluminum nitride and boron nitride, chromium carbide, aluminum oxide or mixtures thereof.
The substrate 4 (
The increase according to the invention in erosion protection is achieved by use of relatively hard, aluminum-containing particles AL* composed of an aluminum alloy, in particular a precipitation-hardened aluminum alloy, which has a 5-10-fold greater hardness and a strength which is higher by a factor of at least 5.
As precipitation-hardening alloys composed of aluminum and at least one element from the group consisting of Zn, Mg, Cu, Mn, Co, preference is given to using, in particular, the following alloys: Al—Zn, Al—Zn—Mn, Al—Mn—SC, Al—Mg—Mn, Al—Mg—Zn—Cu, Al—Cu—Mn—Zn, AlZn4.5Mg1, AlZnMgCu1.5, AlZnMgCu0.5, AlMg4.5Mn.
However, it is also possible to employ alloys having significantly higher contents of various alloying elements, e.g. having 6%-8% of zinc (Zn).
Preference is likewise given to using:
After baking of the aluminum pigment layer, a conductivity blasting with low intensity is generally carried out. Targeted pressure blasting using optimized parameters enables a high increase of aluminum particles to be additionally achieved.
The matrix material of the layers 7, 7′, 7″, 7″′, 10, 10′, 10″, 10″′, 10IV, 10V (
Number | Date | Country | Kind |
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12163734.2 | Apr 2012 | EP | regional |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2013/056537 | 3/27/2013 | WO | 00 |