(57) The method for making a protective coating on a metal substrate including nickel
atoms comprises the steps of : electro-chemical deposition of an aluminum layer on
the substrate using a bath consisting of a ionic liquid comprising a chloroaluminate
anion and an organic cation, and vacuum heating of said substrate on which the aluminum
layer has been deposited, such that nickel atoms migrate from the substrate to the
aluminum layer, with the formation of a nickel-aluminum alloy-based protective coating.
[0001] The present invention relates to a method for making a protective coating on a metal
substrate including nickel atoms.
[0002] This metal substrate is particularly a turbine blade for use in the aeronautic field
or in gas plants for producing electric power. At the high operating temperatures
of the turbines of this kind, said coating acts as a barrier against substrate oxidation,
as well as a "bond coat" for any possible subsequent coating of one or more further
protective layers.
[0003] Said protective layer is known to be obtained by means of rather complicated and
expensive methods, particularly the "chemical vapor deposition" (CVD).
[0004] The object of the present invention is to provide a method as stated in the preamble
of the present description, which results in reduced energy consumption and is environment-friendly.
[0005] According to the invention, this object is achieved by means of a method comprising
the steps of
- electro-chemical deposition of an aluminum layer on said substrate using a bath consisting
of a ionic liquid comprising a chloroaluminate anion and an organic cation, and
- vacuum heating of said substrate on which the aluminum layer has been deposited, such
that nickel atoms migrate from said substrate to the aluminum layer, with the formation
of a nickel-aluminum alloy-based protective coating.
[0006] The inventive method has the advantages of not requiring high temperatures or the
use of dangerous gases and expensive plants, for being implemented.
[0007] The turbines coated by means of the inventive method has an improved energy performance.
This improvement - though poor in absolute terms - is nevertheless very significant
in view of the long operating life of a gas turbine. For example, an increase as low
as 1 % in the performance of a 50 MW turbine may result in about 1000 tons of gas
saved per year, which corresponds to about 200.000 Euro saved per year at present
prices. The decrease of fuel consumption further results in the additional advantage
of reducing the emission of undesired substances, such as nitrogen and carbon dioxide.
[0008] The metal substrate being used preferably contains at least 10% by weight of nickel
and can be particularly a nickel-based super-alloy, for example one of those that
are commercially known as Hastelloy, Inconel, Waspaloy, Rene (e.g. Rene 41, Rene 80,
Rene 95, Rene 104), Haynes, Incoloy, MP98T, TMS and the like.
[0009] The ionic liquid is for example a chloroaluminate of imidazole, pyridinium or ammonium.
[0010] Advantageously, the electrochemical deposition step is carried out at a temperature
ranging between 20 and 50 °C using a current density ranging between 0,5 and 2,5 A/dm
2, whereas the vacuum heating step is carried out at a temperature ranging between
900 and 1150 °C and at a pressure ranging between 1 * 10-5 and 133 * 10-5 Pa.
[0011] Typically, the aluminum layer deposited on the substrate can have a thickness ranging
between 10 and 100 µm.
[0012] An exemplary embodiment of the method according to the invention will be now provided
by way of non-limiting illustration.
EXAMPLE
[0013] A substrate consisting of a nickel alloy made of Ni 72.0%, Cr 15.5%, Fe 8.0%, Si
0.5%, Mn 1.0%, C 0.15%, Cu 0.5%, S < 0.02% is dipped in a bath of 1-butyl,3-methyl-imidazole
hepta-chloroaluminate, made of AIC1
3 and 1-butyl,3-methyl-imidazole chloride at 1:2 molar ratio. In the bath, in which
an anode made of an AI plate with a purity of more than 99% is provided, an electric
current is passed with a density of 1 A/dm
2. This electrochemical treatment is carried out for 2 hours at ambient temperature
thereby causing the formation of a 25 µm-thick aluminum coating layer on the substrate.
[0014] Subsequently, the coated substrate is removed from the bath and kept for 2 hours
at a temperature of 1120 °C and a pressure of < 133*10
-5 Pa. Thereby, a coating layer made of the A1
3Ni and A1Ni compounds is formed by interdiffusion.
[0015] Obviously, the principle of the invention being understood, the implementation details
and the embodiments thereof may be widely changed relative to what has been described
herein by way of example, without however departing from the scope of the invention
as defined in the annexed claims.
1. A method for making a protective coating on a metal substrate including nickel atoms,
comprising the steps of
- electro-chemical deposition of an aluminum layer on said substrate using a ionic
liquid bath comprising a chloroaluminate anion and an organic cation, and
- vacuum heating of said substrate on which the aluminum layer has been deposited,
such that nickel atoms migrate from said substrate to the aluminum layer, with the
formation of a nickel-aluminum alloy-based protective coating.
2. The method according to claim 1, wherein said step of electrochemical deposition is
carried out at a temperature ranging between 20 and 50 °C.
3. The method according to any preceding claim, wherein said step of electrochemical
deposition provides for the use of a current density ranging between 0.5 and 2.5 A/dm2.
4. The method according to any preceding claim, wherein said step of vacuum heating is
carried out at a temperature ranging between 900 and 1150 °C and at a pressure ranging
between 1 * 10-5 and 133 * 10-5 Pa.
5. The method according to any preceding claim, wherein said metal substrate contains
at least 10% nickel by weight.
6. The method according to any preceding claim, wherein said metal substrate is a nickel-based
super-alloy.
7. The method according to any preceding claim, wherein said ionic liquid is a chloroaluminate
of imidazole, pyridinium or ammonium.
8. The method according to any preceding claim, wherein said aluminum layer has a thickness
ranging between 10 and 100 µm.