U.S. patent application number 11/559060 was filed with the patent office on 2007-05-24 for process for coating articles and articles made therefrom.
This patent application is currently assigned to GENERAL ELECTRIC COMPANY. Invention is credited to David A. Helmick, Vinod Kumar Pareek.
Application Number | 20070116809 11/559060 |
Document ID | / |
Family ID | 37622247 |
Filed Date | 2007-05-24 |
United States Patent
Application |
20070116809 |
Kind Code |
A1 |
Pareek; Vinod Kumar ; et
al. |
May 24, 2007 |
PROCESS FOR COATING ARTICLES AND ARTICLES MADE THEREFROM
Abstract
In one embodiment, a coated turbine article comprising a uniform
enhanced coating on at least a portion of the turbine article,
wherein the enhanced coating comprises a coating material and a
structural enhancer, wherein the structural enhancer is selected
from the group consisting of oxide, carbide, nitride, intermetallic
material, and combinations comprising at least one of the
foregoing, wherein the structural enhancer has an average particle
size, as measured along a major axis, of about 0.01 .mu.m to about
100 .mu.m.
Inventors: |
Pareek; Vinod Kumar;
(Albany, NY) ; Helmick; David A.; (Fountain Inn,
SC) |
Correspondence
Address: |
CANTOR COLBURN, LLP
55 GRIFFIN ROAD SOUTH
BLOOMFIELD
CT
06002
US
|
Assignee: |
GENERAL ELECTRIC COMPANY
1 River Road
Schenectady
NY
12345
|
Family ID: |
37622247 |
Appl. No.: |
11/559060 |
Filed: |
November 13, 2006 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
|
11285486 |
Nov 21, 2005 |
|
|
|
11559060 |
Nov 13, 2006 |
|
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Current U.S.
Class: |
426/302 |
Current CPC
Class: |
F05D 2300/226 20130101;
C23C 4/067 20160101; Y10T 428/1209 20150115; F01D 5/284 20130101;
F05D 2230/312 20130101; Y10T 428/12931 20150115; C23C 4/06
20130101; F01D 5/288 20130101; F05D 2300/22 20130101; F05D 2230/313
20130101; Y10T 428/12854 20150115; F05D 2300/21 20130101; C23C
30/00 20130101; Y10T 428/12736 20150115; F05D 2300/228 20130101;
F05D 2230/311 20130101; Y10T 428/12847 20150115 |
Class at
Publication: |
426/302 |
International
Class: |
A23L 1/00 20060101
A23L001/00 |
Claims
1. A method of forming a coated article, comprising: forming a
mixture of a coating material and a structural enhancer selected
from the group consisting of oxide, carbide, nitride, intermetallic
material, and combinations comprising at least one of the
foregoing, wherein the mixture comprises an initial structural
enhancer concentration; heating the mixture; and propelling the
mixture at the article to form an enhanced coating, wherein the
enhanced coating has a final structural enhancer concentration that
is less than or equal to 5 vol % greater than the initial
structural enhancer concentration, based upon a total volume of the
enhanced coating.
2. The method of claim 1, further comprising controlling a particle
size of the structural enhancer.
3. The method of claim 1, further comprising controlling a
distribution of the structural enhancer in the coating.
4. The method of claim 1, wherein the mixture comprises at least
two of the structural enhancers.
5. The method of claim 1, wherein the structural enhancer has an
average particle size, as measured along a major axis, of about
0.01 .mu.m to about 100 .mu.m.
6. The method of claim 5, wherein the average particle size is
about 1 .mu.m to about 50 .mu.m.
7. The method of claim 6, wherein the average particle size is
about 5 .mu.m to about 25 .mu.m.
8. The method of claim 1, wherein the structural enhancer comprises
intermetallic material.
9. The method of claim 1, wherein the structural enhancer comprises
an oxide.
10. The method of claim 9, wherein the structural enhancer
comprises aluminum oxide.
11. The method of claim 1, wherein the structural enhancer
comprises a nitride.
12. The method of claim 1, wherein the enhanced coating comprises
MCrAlY, wherein M is selected from the group consisting of nickel,
cobalt, iron, and combinations comprising at least one of the
foregoing.
13. The method of claim 12, wherein the enhanced coating further
comprises an element selected from the group consisting of silicon,
ruthenium, iridium, osmium, gold, silver, tantalum, palladium,
rhenium, hafnium, platinum, rhodium, tungsten, alloys comprising at
least one of the foregoing, and combinations comprising at least
one of the foregoing.
14. The article of claim 13, wherein the enhanced coating comprises
an element selected from the group consisting of ruthenium,
iridium, osmium, gold, silver, tantalum, palladium, rhenium,
platinum, rhodium, tungsten, alloys comprising at least one of the
foregoing, and combinations comprising at least one of the
foregoing.
15. The method of claim 1, wherein the final structural enhancer
concentration is about 1 vol % to about 25 vol %, based upon a
total volume of the enhanced coating.
16. The article of claim 15, wherein the final structural enhancer
concentration is of about 5 vol % to about 15 vol %.
17. The article of claim 1, wherein the enhanced coating has a
uniform concentration of the structural enhancer.
18. A method of forming a coated article, comprising: forming a
mixture of a coating material and a structural enhancer, wherein
the structural enhancer comprises an aluminum oxide, wherein the
mixture comprises an initial structural enhancer concentration;
heating the mixture; and propelling the mixture at the article to
form an enhanced coating, wherein the enhanced coating has a final
structural enhancer concentration that is less than or equal to 5
vol % greater than the initial structural enhancer concentration,
based upon a total volume of the enhanced coating; and wherein the
enhanced coating comprises MCrAlY, wherein M is selected from the
group consisting of nickel, cobalt, iron, and combinations
comprising at least one of the foregoing.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This application is a divisional of U.S. application Ser.
No. 11/285,486, filed on Nov. 21, 2005, which is hereby
incorporated by reference.
BACKGROUND
[0002] When exposed to high temperatures (i.e., greater than or
equal to about 1,300.degree. C.) and to oxidative environments,
metals can oxidize, corrode, and become brittle. These environments
are produced in turbines used for power generation applications.
Thermal barrier coatings (TBC), when applied to metal turbine
components, can reduce the effects that high-temperature, and
corrosive and oxidative environments have on the metal
components.
[0003] Thermal barrier coatings can comprise a metallic bond
coating and a ceramic coating. The metal bond coating can comprise
of oxidation resistant protective materials such as aluminum,
chromium, aluminum alloys, and chromium alloys. For example, the
metallic bond coating can comprise of chromium, aluminum, yttrium,
or combinations of the forgoing, such as MCrAlY where M is nickel,
cobalt, or iron (U.S. Pat. No. 4,034,142 to Hecht, and U.S. Pat.
No. 4,585,481 to Gupta et al. describe some coating materials).
These metallic bond coatings can be applied by thermal spraying
techniques.
[0004] The family of thermal spray processes includes detonation
gun deposition, high velocity oxy-fuel deposition (HVOF) and its
variants such as high velocity air-fuel, plasma spray, flame spray,
and electric wire arc spray. In most thermal coating processes a
material in powder, wire, or rod form (e.g., metal) is heated to
near or somewhat above its melting point and droplets of the
material accelerated in a gas stream. The droplets are directed
against the surface of a substrate to be coated where they adhere
and flow into thin lamellar particles called splats.
[0005] In a typical detonation gun deposition process, a mixture of
oxygen and a fuel such as acetylene along with a pulse of powder of
the coating material is injected into a barrel, such as a barrel of
about 25 millimeters (mm) in diameter and over a meter long. The
gas mixture is detonated, and the detonation wave moving down the
barrel heats the powder to near or somewhat above its melting point
and accelerates it to a velocity of about 750 meters per second
(m/sec). The molten, or nearly molten, droplets of material strike
the surface of the substrate to be coated and flow into strongly
bonded splats. After each detonation, the barrel is generally
purged with an inert gas such as nitrogen, and the process repeated
many times a second. Detonation gun coatings typically have a
porosity of less than two volume percent with very high cohesive
strength as well as very high bond strength to the substrate.
[0006] In high velocity oxy-fuel and related coating processes,
oxygen, air or another source of oxygen, is used to burn a fuel
such as hydrogen, propane, propylene, acetylene, or kerosene, in a
combustion chamber and the gaseous combustion products allowed to
expand through a nozzle. The gas velocity may be supersonic.
Powdered coating material is injected into the nozzle and heated to
near or above its melting point and accelerated to a relatively
high velocity, such as up to about 600 m/sec. for some coating
systems. The temperature and velocity of the gas stream through the
nozzle, and ultimately the powder particles, can be controlled by
varying the composition and flow rate of the gases or liquids into
the gun. The molten particles impinge on the surface to be coated
and flow into fairly densely packed splats that are well bonded to
the substrate and each other.
[0007] In the plasma spray coating process a gas is partially
ionized by an electric arc as it flows around a tungsten cathode
and through a relatively short converging and diverging nozzle. The
temperature of the plasma at its core may exceed 30,000 K and the
velocity of the gas may be supersonic. Coating material, usually in
the form of powder, is injected into the gas plasma and is heated
to near or above its melting point and accelerated to a velocity
that may reach about 600 m/sec. The rate of heat transfer to the
coating material and the ultimate temperature of the coating
material are a function of the flow rate and composition of the gas
plasma as well as the torch design and powder injection technique.
The molten particles are projected against the surface to be coated
forming adherent splats.
[0008] In the flame spray coating process, oxygen and a fuel such
as acetylene are combusted in a torch. Powder, wire, or rod, is
injected into the flame where it is melted and accelerated.
Particle velocities may reach about 300 m/sec. The maximum
temperature of the gas and ultimately the coating material is a
function of the flow rate and composition of the gases used and the
torch design. Again, the molten particles are projected against the
surface to be coated forming adherent splats.
[0009] Thermal spray coating processes have been used for many
years to deposit layered coatings. These coatings consist of
discrete layers of different composition and properties. For
example, the coating may be a simple duplex coating consisting of a
layer of a metal alloy such as nickel-chromium adjacent to the
substrate with a layer of zirconia over it.
[0010] The coating processes can be used to apply thermal barrier
coatings (TBC) and/or environmental barrier coatings (EBC) to
components of turbines, engines, and the like, to protect the
components from the harsh operating environments. To protect
turbine components in these combustion environments, a class of
coatings has been developed based on the formula MCrAlY where M
represents a transition metal such as iron, cobalt, or nickel. A
current problem exists when MCrAlY coatings are used in integrated
gasification combined cycle (IGCC) systems. IGCC systems use an
innovative process, which uses coal to produce power. The process
is cleaner and more economically efficient than other processes
that use coal to produce power. The process involves treating coal
and reforming coal to a gas mixture that includes hydrogen gas
(H.sub.2), carbon monoxide (CO), and carbon particulates. This gas
mixture is combusted with oxygen in a turbine to produce power. The
carbon particulates, however, collide with the coated turbine
components and erode the components and/or coatings, and thereby
shorten the effective operating life of the components.
[0011] Therefore, there exists a need for coatings that can provide
improved protection for turbine components.
SUMMARY OF THE INVENTION
[0012] Disclosed herein are methods for coating articles and
articles made therefrom. In one embodiment, a coated turbine
article comprising a uniform enhanced coating on at least a portion
of the turbine article, wherein the enhanced coating comprises a
coating material and a structural enhancer, wherein the structural
enhancer is selected from the group consisting of oxide, carbide,
nitride, intermetallic material, and combinations comprising at
least one of the foregoing, wherein the structural enhancer has an
average particle size, as measured along a major axis, of about 1
.mu.m to about 100 .mu.m.
[0013] In another embodiment, a coated turbine article comprises a
article formed from the process comprising: forming a mixture of a
coating material and a structural enhancer selected from the group
consisting of oxide, carbide, nitride, intermetallic material, and
combinations comprising at least one of the foregoing, wherein the
mixture comprises an initial structural enhancer concentration;
heating the mixture; and propelling the mixture at the article to
form the enhance coating, wherein the enhanced coating has a final
structural enhancer concentration that less than or equal to 5 vol
% greater than the initial structural enhancer concentration, based
upon a total volume of the enhanced coating.
[0014] The above described and other features are exemplified by
the following detailed description and appended claims.
DETAILED DESCRIPTION
[0015] The terms "first," "second," and the like, herein do not
denote any order, quantity, or importance, but rather are used to
distinguish one element from another, and the terms "a" and "an"
herein do not denote a limitation of quantity, but rather denote
the presence of at least one of the referenced item. The modifier
"about" used in connection with a quantity is inclusive of the
stated value and has the meaning dictated by the context, (e.g.,
includes the degree of error associated with measurement of the
particular quantity). The suffix "(s)" as used herein is intended
to include both the singular and the plural of the term that it
modifies, thereby including one or more of that term (e.g., the
metal(s) includes one or more colorants). Ranges disclosed herein
are inclusive and independently combinable (e.g., ranges of "up to
about 25 wt %, or, more specifically, about 5 wt % to about 20 wt
%", is inclusive of the endpoints and all intermediate values of
the ranges of "about 5 wt % to about 25 wt %," etc). The notation
".+-.10%" means that the indicated measurement may be from an
amount that is minus 10% to an amount that is plus 10% of the
stated value.
[0016] Metallic coating structural integrity can be enhanced by
combining structural enhancer(s) (e.g., carbide(s) and/or oxide(s))
into the coatings. However, when a thermal spray process is
controlled (e.g., temperature) to form the structural enhancers
(e.g., oxides) as the coating materials are sprayed at the
component, the distribution of the structural enhancer(s), as well
as the particle sizes of the structural enhancer(s) is not fully
controlled. Disclosed herein is a method for forming an enhanced
barrier coating on a component and the components made therefrom.
This process enables control of the structural enhancer(s)'
particle size as well as enabling uniform distribution of the
structural enhancer(s) throughout desired area(s) of the coating.
As used herein, "uniform" and "uniform distribution" refers to a
change in concentration across the entire area of the enhanced
coating comprising that material of less than or equal to 5 volume
percent (vol %). For example, if the enhanced coating is deposited
on a leading edge of a component while a different coating is
deposited on the remainder of the component, a change in
concentration throughout the enhanced coating will be less than or
equal to 5 vol %.
[0017] The thermal spray process (e.g., HVOF, plasma spray (such as
low pressure plasma spraying, vacuum plasma spraying, and so
forth), or a combination comprising at least one of the forgoing
processes) comprises mixing coating material(s) with the structural
enhancer(s), e.g., prior to introduction to the spray stream and/or
in the spray stream. Desirably, less than or equal to about 5 vol
%, or, more specifically, less than or equal to about 2 vol % of
the coating material(s) convert to oxides and/or carbides during
the coating process. Therefore, the concentration of the enhanced
coating is controlled. In other words, this process enables control
of the particular structural enhancer(s), including desired
particle sizes and size distributions, and combines those
structural enhancer(s) with the coating material(s) to form a
mixture that can produce an enhanced coating with a chosen
composition (e.g., the concentration of the structural enhancer(s)
can be controlled).
[0018] The process comprises introducing the mixture to the
combustion chamber, spray stream, and/or so forth (depending upon
the particular spray process), and sufficiently heating the mixture
to enable the particles to splat on and adhere to the component.
For example, and HVOF process can be employed where oxygen and fuel
combust and propel the mixture at the component. In order to
control the production of oxides and/or carbides in the spray as
the mixture is propelled at the component, the spray conditions can
be controlled. The spray can be controlled such that the
temperature of the particles (e.g., coating material(s) and
structural enhancer(s)) being propelled at the component is a
temperature sufficient to soften the particles such that they
adhere to the component and less than a temperature that causes
oxidation of the coating material(s), with the specific temperature
dependent upon the type of coating material(s) and structural
enhancer(s). For example, the coating temperature can be less than
or equal to about 1,500.degree. C., or, more specifically, less
than or equal to about 1,200.degree. C., or, even more
specifically, about 750.degree. C. to about 1,100.degree. C. The
temperature can be controlled such that the concentration of
structural enhancer(s) can change from the mixture to the enhanced
coating by less than or equal to about 5 vol %, or, more
specifically, less than or equal to about 2 vol %, or, even more
specifically, less than or equal to about 1 vol %. For example, if
the mixture comprises 10 vol % structural enhancer(s), based upon
the total volume of the mixture, the final coating will comprise
less than or equal to about 15 vol % structural enhancer(s), based
upon the total volume of the enhanced coating.
[0019] The coating material(s) to form the barrier coatings (e.g.,
thermal barrier coatings and/or environmental barrier coatings) can
include nickel (Ni), cobalt (Co), iron (Fe), chromium (Cr),
aluminum (Al), yttrium (Y), alloys comprising at least one of the
foregoing, as well as combinations comprising at least one of the
foregoing, e.g., the coating can comprise MCrAlY (where M comprises
nickel, cobalt, iron, and combinations comprising at least one of
the forgoing). An MCrAlY coating can further comprise elements such
as silicon (Si), ruthenium (Ru), iridium (Ir), osmium (Os), gold
(Au), silver (Ag), tantalum (Ta), palladium (Pd), rhenium (Re),
hafnium (Hf), platinum (Pt), rhodium (Rh), tungsten (W), alloys
comprising at least one of the foregoing, as well as combinations
comprising at least one of the foregoing.
[0020] Structural enhancer(s) that can be mixed with the coating
material(s) include oxide(s), carbide(s), nitride(s),
intermetallic(s) (e.g., a stoichiometric metallic compound), and so
forth, as well as combinations comprising at least one of the
foregoing. Possible oxides include alumina, zirconia, silica, and
so forth, as well as combinations comprising at least one of the
foregoing. These oxides can be stabilized, for example, with
stabilizers such as yttrium, barium, magnesium, calcium, strontium,
beryllium, a lanthanide element, and so forth, as well as
combinations comprising at least one of the foregoing stabilizers;
e.g., yttria stabilized zirconia.
[0021] The structural enhancer(s) can have an average particle
size, as measured along a major axis, of up to about 100 micrometer
(.mu.m) or so (e.g., about 0.01 .mu.m to about 100 .mu.m), or, more
specifically, about 1 .mu.m to about 50 .mu.m, or, even more
specifically, about 5 .mu.m to about 25 .mu.m. Since the structural
enhancer(s) are mixed with the coating material(s) prior to
introduction to the spray stream, the particles size is both the
particles size of the structural enhancer(s) in the mixture and in
the enhanced coating.
[0022] The structural enhancer(s) can be present in a sufficient
amount to enhance the structural integrity of the coating against
physical erosion. For example, the structural enhancer(s) can be
present in an amount of less than or equal to about 25 vol %, or,
more specifically, about 1 vol % to about 15 vol %, or, even more
specifically, about 5 vol % to about 10 vol %, based upon the total
volume of the enhanced coating. The particular concentration of the
structural enhancer(s) can be determined based upon the particular
component and the operating conditions for that component. For
example, whether the component is blade, vane, stator, nozzle,
bucket, etc., in a turbine (e.g., in an IGCC system), and the
component's location in the system, e.g., first stage, second
stage, and so forth, can affect the desired coating composition as
well as the amount and location of the enhanced coating on the
component. For example, the present coating can be particularly
useful on first stage components, e.g., components that tend to
experience higher erosion rats than other turbine components.
[0023] As with the enhanced coating composition, the enhanced
coating thickness can be chosen based upon the particular
component, the operating conditions for that component, and the
location of the coating on that component. The enhanced coating
thickness can be about 0.05 millimeters (mm) to about 0.75 mm or
so, or, more specifically, about 0.1 mm to about 0.5 mm, or, even
more specifically, about 0.15 mm to about 0.3 mm.
[0024] Optionally, once the enhanced coating has been applied to
the component, the component can be further processed, e.g., to
improve the bond between the coating material and the substrate.
For example, the component with the enhanced coating can be heat
treated, e.g., to enable the formation of chemical bonding. The
heat treating can be at temperatures of about 900.degree. C.
(1,650.degree. F.) to about 1,200.degree. C. (2,190.degree. F.),
e.g., about 1,100.degree. C. (2,012.degree. F.) for about 0.5 hours
to about 6 hours or so, under a vacuum or in an inert environment
(e.g., with an inert gas that will not chemically interact with the
coating).
EXAMPLES
[0025] Deposition can be accomplished using a methods such as
plasma spraying (low pressure plasma spraying (LPPS), vacuum plasma
spraying (VPS) and/or HVOF), e.g., with a thermal spray gun
manufactured by Sulzer Metco. In the deposition, MCrAlY and
structural enhancer particles can be mixed in a ratio of 80 vol %
to 20 vol %, respectively, in a hopper. The particle sizes of the
MCrAlY powder and the structural enhancer can be about 0.01 .mu.m
to about 100 .mu.m. The powder mixture can then be fed from the
hopper to the gun where it is heated and accelerated onto a
component disposed in the hot gas path. The coating can be applied
to a nominal thickness of 10 mils with a constant volume percentage
of structural enhancer particles through the thickness and the
coverage area. This process has been found particularly useful for
components used in turbines in IGCC plants.
[0026] The enhanced coatings and process of forming these coatings
can be used in numerous applications, including to coat turbine
components or portions thereof. More specifically, the enhanced
coatings can be utilized in components exposed to the hot gas path
of the turbine engine including those used in IGCC systems. In IGCC
systems, a synthesis gas is first reformed from coal and then
combusted inside a turbine engine. The combustion stream often
comprises carbon particulates that can impinge on the turbine
components, causing physical erosion. By forming depositing the
enhanced coatings on portions of the components susceptible to this
erosion, the life of the component can be substantially
enhanced.
[0027] While the invention has been described with reference to a
preferred embodiment, it will be understood by those skilled in the
art that various changes may be made and equivalents may be
substituted for elements thereof without departing from the scope
of the invention. In addition, many modifications may be made to
adapt a particular situation or material to the teachings of the
invention without departing from essential scope thereof.
Therefore, it is intended that the invention not be limited to the
particular embodiment disclosed as the best mode contemplated for
carrying out this invention, but that the invention will include
all embodiments falling within the scope of the appended
claims.
* * * * *