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(19) United States
US 2016O184890A1
(12) Patent Application Publication (10) Pub. No.: US2016/0184890 A1
KOOL et al. (43) Pub. Date: Jun. 30, 2016
(54) CHROMIDE COATINGS, ARTICLES COATED
WITH CHROMIDE COATINGS, AND
PROCESSES FOR FORMING CHROMIDE
COATINGS
(71) Applicants:Lawrence Bernard KOOL, Clifton
Park, NY (US); Bhupendra Kumar
GUPTA, Cincinnati, OH (US); Mark
ROSENZWEIG, West Chester, OH
(US); Samar Jyoti KALITA, Cincinnati,
OH (US)
(72) Inventors: Lawrence Bernard KOOL, Clifton
Park, NY (US); Bhupendra Kumar
GUPTA, Cincinnati, OH (US); Mark
ROSENZWEIG, West Chester, OH
(US); Samar Jyoti KALITA, Cincinnati,
OH (US)
(73) Assignee: GENERAL ELECTRIC COMPANY.,
Schenectady, NY (US)
(21) Appl. No.: 14/585,890
(22) Filed: Dec. 30, 2014
Publication Classification
(51) Int. Cl.
B22F I/O (2006.01)
C23C I6/56 (2006.01)
C23C I6/44 (2006.01)
(52) U.S. Cl.
CPC ................. B22F I/007(2013.01); C23C I6/44
(2013.01); C23C I6/56 (2013.01)
(57) ABSTRACT
Aslurry coatingcomposition forenrichingasurfaceregion of
a metal-based Substrate with chromium includes a metallic
powder including chromium powder in the Cr(O) oxidation
state and aluminum powder, a binder including colloidal
silica to bind the metallic powder; and a stabilizer, wherein
the chromium powder comprises at least about 80% by
weight of the metallic powder and the aluminum powder
comprisesup to about 10%by weightofthe metallicpowder.
Aprocess offormingacoatingandenrichingaSurfaceregion
of a component formed of a nickel-based Superalloy with
chromium includes applying the slurry coating composition
to the Surface region ofthe component to form a slurry coat
ing on the Surface region; curing the slurry coating to form a
green coating; and sinteringthegreen coating to form acoat
ing having chromium in the alpha phase at an operating
temperature of the component between about 1200° C. to
about 1800°C.A nickel-basedsuperalloycomponentofagas
turbineenginehasacoatingandSurface regionenrichedwith
chromium formed by the process.
Patent Application Publication Jun. 30, 2016 Sheet 1 of4 US 2016/O184890 A1
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PatentApplication Publication
US 2016/0184890 A1
CHROMIDE COATINGS, ARTICLES COATED
WITH CHROMIDE COATINGS, AND
PROCESSES FOR FORMING CHROMIDE
COATINGS
BACKGROUND
0001. The present technology generally relates to protec
tivecoating systems suitableforcomponentsexposedtohigh
temperatures,suchasthehostilethermalenvironmentofagas
turbine engine. More particularly, the present technology
relatestoslurrycoatingcompositionsandprocessesforselec
tivelyenrichingSurfaceregionsofacomponent,forexample,
theunder-platformregionsonaturbineblade,with corrosion
resistant metals such as chromium.
0002 Components ofturbine engines, such as the blades
andVanes (nozzles)within theturbinesection ofagasturbine
engine, are often formed of an iron, nickel, or cobalt-base
superalloy. A turbine blade has an airfoil against which hot
combustion gases are directed during operation of the gas
turbine engine, and whose Surface is therefore subjected to
severeattackby oxidation, corrosion and erosion. The blade
further includes a platform and an under-platform or root
section separated from the airfoil by the platform that, while
not directly exposedto hotgas path, are still exposedto high
temperatures and are susceptible to oxidation and corrosion.
Turbinebladesorbucketsaretypicallyanchoredtotheperim
eterofa rotororwheelby formingthe rotortohaveslots with
dovetail cross-sections that interlock with a complementary
dovetail profile on the root section ofeach blade.
0003. Due to the severity oftheiroperatingenvironments,
turbine bladesoften requireenvironmentally protective coat
ings on the Surfaces oftheirairfoilsandplatforms exposedto
the hot gas path. Diffusion coatings Such as chromide, alu
minide, and platinum aluminide coatings are widely used as
environmental coatings in gas turbine engine applications
because oftheir oxidation resistance. Such coatings, which
aretypically appliedtothe internaland external Surfaces ofa
blade, are produced by a thermal/chemical reaction process
that results in the near-surface region ofthe Substrate being
enriched with, depending on the type ofcoating, chromium,
aluminum, platinum, etc., as well as intermetallics that form
as a result of reactions between the deposited corrosion
resistant specie?(s) andthe Substrate material. Diffusion coat
ing processes typically take place in a reduced and/or inert
atmosphere at elevated temperatures. Common processes
include pack cementation and noncontact vapor (gas phase)
deposition techniques, or by diffusing corrosion-resistant
species deposited by chemical vapor deposition (CVD) or
slurry coating.
0004. In pack cementation and noncontact vapor deposi
tiontechniques, vaporofthedesiredcorrosion-resistant coat
ingspecies (e.g.,chromium,aluminum, etc.) isgeneratedand
caused to contact Surfaces on which the coating is desired.
The vapor reacts with the surface to deposit the desired coat
ing specie?s), whicharethen diffusedintotheSurfacethrough
a heat treatment. Aluminide diffusion coatings deposited by
pack cementation or noncontact vapor deposition are often
preferred for turbine blade airfoils. The dovetails ofturbine
blades are typically machined prior to the diffusion coating
process, and may be masked during coating so thatthe dove
tail will properly assemble with the dovetail slot in the rotor
during engine build. However, during engine operation the
under-platform regions oftheblade can become corroded. In
the past, corrosion of under-platform regions of turbine
Jun. 30, 2016
blades has been addressed by applying a vapor-phase chro
mide coating. While capable of improving corrosion resis
tance, vapor-phase chromizingprocesses require masking to
prevent the chromide coating from being deposited on other
surfaces oftheblade, such as thosealready provided with an
aluminide coating. However, masking is time-consuming,
expensive, and not always effective.
0005 Slurryprocessesgenerallyentail theuseofanaque
ous or organic solvent slurry containing a volatile liquid
vehicleandapowderofthe corrosion-resistantcoatingspecie
(s) that can be sprayed or otherwise applied to a Substrate,
after which the substrate is heated to evaporate the volatile
componentsoftheslurryand,withfurtherheating, diffusethe
remainingcoatingspeciesintotheSubstrate.Anexampleofa
slurry composition is disclosed in U.S. Pat. No. 3.248,251 as
containing aluminum particulates dispersed in an aqueous,
acidic bonding solution that also contains metal chromate,
dichromateor molybdate, andphosphate (the latterofwhich
serves as a binder). The chromate ions are known to improve
corrosion resistance. One prevalent theory described in U.S.
Pat. No. 6,074,464 is that chromate ions passivate the bond
ing Solution toward aluminum and inhibit the oxidation of
metallicaluminum. Inthis manner,particulatealuminum can
be combined with the bonding solution without undesirable
reactions between the solution and aluminum.
0006. A drawback of slurry compositions of the type
taught by the priorart discussed above is the reliance on the
presence of chromates, which are considered toxic. In par
ticular, hexavalent chromium is considered to be a carcino
gen. When compositions containing this form ofchromium
are used (e.g., in spray booths), special handling procedures
that must be closely followed to satisfy health and safety
regulations can result in increased costs and decreased pro
ductivity. Therefore, attempts have been made to formulate
slurry compositions which do not rely on the presence of
chromates. For example, U.S. Pat. No. 6,150,033 describes
chromate-free coating compositions used to protect metal
Substrates Such as stainless steel. Many ofthe compositions
disclosed in this patent are based on an aqueous phosphoric
acid bonding Solution, which comprises a source of magne
sium, Zinc, and borate ions. However, chromate-free slurry
compositions can have various disadvantages, such as insta
bility overthecourse ofseveral hours (oreven minutes), and
generation of unsuitable levels of gases such as hydrogen.
Furthermore, chromate-free slurry compositions have been
known to thicken or partially solidify, rendering them very
difficult to apply to a substrate by spray techniques. More
over,theuse ofphosphoricacidin thecompositions may also
contribute to instability, especially if chromate compounds
are not present since the latterapparently passivates the Sur
faces ofthealuminum particles. In the absenceofchromates,
phosphoric acid may attack the metallic aluminum particles
in the slurry composition, rendering the composition ther
mally and physically unstable. Atbest. Such a slurry compo
sition will be difficultto store and apply to a substrate.
0007. In view ofthe above, there are ongoing efforts to
develop new slurrycompositionscapableofformingenviron
mentally-protective coatings on Substrates. Such composi
tions should be capable ofincorporating as much corrosion
resistantspeciesas necessary intoaSubstrate,andshouldalso
be substantially free of chromate compounds, especially
hexavalent chromium. Moreover, improved slurry composi
tionsshouldbechemically andphysically stableforextended
periods ofuseand storage, amenableto slurryapplication by
US 2016/0184890 A1
various techniques such as spraying, painting, and the like,
and should be generally compatible with other techniques
which might be used to treat a particular metal substrate, for
example, Superalloy components such as turbine blades.
SUMMARY
0008. In accordance with an example of the technology
disclosedherein,aslurry coating composition forenrichinga
Surface region of a metal-based Substrate with chromium
comprises a metallic powder including chromium powder in
the Cr(O) oxidation state and aluminum powder; a binder
including colloidal silica to bind the metallic powder; and a
stabilizer, wherein the chromium powder comprises at least
about 80% by weight ofthe metallic powderand the alumi
num powder comprises up to about 10% by weight ofthe
metallic powder.
0009. In accordance with an example of the technology
disclosedherein,amethodofformingacoatingandenriching
a Surface region of a component formed of a nickel-based
Superalloy with chromium comprises applying the slurry
coatingcompositiontotheSurfaceregionofthecomponentto
form a slurry coating on the Surface region; curing the slurry
coatingto form a green coating; and sinteringthe green coat
ing to form a coatinghaving chromium in the alphaphase at
an operating temperature of the component between about
1200° C. to about 1800° C.
0010. In accordance with an example of the technology
disclosed herein, a nickel-based Superalloy component ofa
gas turbine enginehas a coatingand Surface region enriched
with chromium formed by the process.
BRIEF DESCRIPTION OF THE DRAWINGS
0011. Theseandotherfeatures, aspects,andadvantagesof
the present technology will become better understood when
thefollowingdetailed descriptionis readwith referencetothe
accompanying drawings in which like characters represent
like parts throughout the drawings, wherein:
0012 FIG. 1 schematically depicts a turbine component
that may be coated according to the present technology;
0013 FIG. 2 depicts a coatingaccording to an exampleof
the present technology;
0014 FIG.3 depicts a coatingaccording to an exampleof
the present technology;
0015 FIG. 4 depicts a coatingaccording to an exampleof
the present technology;
0016 FIG.5 depicts a coatingaccording to an exampleof
the present technology; and
0017 FIG. 6 depicts a phase diagram ofa Ni Cralloy.
DETAILED DESCRIPTION
0018. The slurry coating compositions andprocess ofthe
presenttechnology may be usedto selectively enrich Surface
regions of Substrates with chromium, and also aluminum if
desired. One application may be the under-platform regions
onturbineblades ofgas turbineengines. Referring to FIG. 1,
ahighpressureturbineblade 10 includes anairfoil 12against
which hot combustion gases are directed during operation of
the gas turbine engine, and whose Surface is therefore Sub
jected to severe attack by oxidation, corrosion, (e.g. hot Sul
fate corrosion), and erosion. The blade 10 is anchored to a
turbine disk (not shown) with a dovetail 14 formed on a root
section oftheblade 10.Aplatform 16 separates the airfoil 12
and the dovetail 14, and the root section, its dovetail 14, and
Jun. 30, 2016
the underside of the platform 16 are referred to as under
platform regions 18 of the blade 10. Though not directly
exposed to the hot gas path of a turbine engine, the under
platform regions 18 are nonetheless Susceptible to oxidation
and corrosion that may be induced by Sulfurcontaining dirt,
debris, and/ordeposits entrained in the cooling airthat flows
aroundthe under-platform region oftheblade. Slurry coating
compositionsandprocessesofthepresenttechnology maybe
used to selectively form a chromium-containing coating on
the surfaces ofthe under-platform regions 18 oftheblade 10
ofFIG. 1, as well as surfaces ofothercomponents similarly
Subjected to oxidation and corrosion. Examples ofthe coat
ingsthatmaybeappliedby thepresenttechnology areshown
in FIGS. 2-5.
0019 Referringto FIG. 6, a Ni–Crphasediagramshows
that at temperatures from about 1200° C. (approximately
2200 F) to about 1800° C. (approximately 3270° F.), the
alpha phase ofchromium exists from about 78-100at.%. In
orderto obtainanalphaphase chromium coatingappliedto a
nickelbased Superalloy gas turbinecomponent, e.g.aturbine
blade, at operating temperatures ofthe component, the at. 96
ofthechromium in the coatingshouldbe at least78%. Given
thesimilaratomic massesofCrandNi,themetallicpowderof
the slurry coating composition may be about 80-100% by
weight Cr. The slurry coating composition may include Cr
powderintheCr(O)oxidationstate, i.e.hexavalentfree,and is
therefore not restricted as is Cr(VI), i.e. hexavalent chro
mium. The slurry powder particle size distribution may be
from about 1 to 5um.
0020. The composition of the chromium-based powder
and its amount in the slurry composition may depend on the
amount ofchromium desired for the under-platform regions
18. In general, Suitableamounts ofchromium and optionally
aluminum in the slurry composition should exceed their
respectiveamounts inthesubstratetobeprotected.Thechro
mium content ofthe slurry composition should be sufficient
to compensate for any projected loss ofchromium from the
under-platform regions 18 under expected operating condi
tions, such as temperatures, temperature/time schedules and
cycles, and environmental conditions.
0021. In addition to Cr, the metallic powder ofthe slurry
coating composition may include aluminum to provide uni
formity and enhance diffusion ofthe coating. TheAl powder
particle size distribution may be from about 10-14 um and
maybe up to about 10%, forexampleabout 1-5%, by weight
of the metallic powder. Other metals may be included to
provide enhanced oxidation resistance, phase stability, envi
ronmental resistance, and Sulfidation resistance. Metals that
may be included in the powder ofthe slurry coating compo
sition include Co, Fe, Ti, Ta, W, Re, Mo, Hf, Si, and Pt. The
powder may also contain various other elements and other
materials at impurity levels, e.g., less than about 1% by
weight.
0022. The metallic powder may constitute, by weight,
about25%toabout80%, morepreferablyabout30% toabout
50%, ofthe entire slurry composition. The powder particles
maybe in the form ofspherical particles, though otherforms
are possible as well. Such as wire, wire mesh, and those
described above for the colloidal silica. The metallicpowder
canbeusedina variety ofstandardsizes.Acceptablesizes for
the powder particles will depend on several factors. Such as
the alloy ofthe under-platform regions 18, the technique by
US 2016/0184890 A1
whichtheslurry istobeappliedto theunder-platform regions
18,andthepresenceandamounts ofotherpotential constitu
ents in the slurry.
0023 Theslurrycoatingcompositionsofthepresenttech
nology may include a binder, for example, a non-organic
binder. One binder that may be used is colloidal silica. The
term “colloidal silica” is meantto embrace any dispersion of
fineparticlesofsilicainamediumofwateroranothersolvent,
with waterbeingpreferredsuchthattheslurrycomposition is
a water-based (aqueous) system. Dispersions of colloidal
silica are available from various chemical manufacturers in
eitheracidicorbasic form. Moreover, variousshapesofsilica
particles can be used, e.g., spherical, hollow, porous, rod,
plate, flake, or fibrous, as well as amorphous silica powder.
Theparticles may have an average particle size in a range of
about 10 nanometers to about 100 nanometers. Commercial
examples of colloidal silica are available under the names
LudoxR) from Sigma-Aldrich Co. LLC and Remasol(R) from
REMETCorporation, ofUtica, N.Y., USA.
0024. The amount ofcolloidal silica present in the com
position will depend on various factors, for example, the
amount of metallic powder used and the presence (and
amount) ofany other constituents in the slurry, for example,
an organic stabilizer as discussed below. Colloidal silica
appears tofunction primarily as a very effective binder in the
slurry composition. Processing conditions are also a consid
eration, forexample, how the slurry is formedandapplied to
the under-platform regions 18. The colloidal silica may be
present at a level in the range ofabout 1% to about 25% by
weight, based on silica solids as a percentage ofthe entire
composition. In especially preferred embodiments, the
amountis in the rangeofabout 10% toabout20% by weight.
0025. In addition to the metallic powder and colloidal
silica,theslurry compositions mayfurtherinclude othercon
stituents, for example wetting agents and metal powder sta
bilizers. One example of a wetting agent and Stabilizer is
glycerol, CH3(OH), sometimes referred to as 'glycerin” or
“glycerine.” Glycerol can readily be obtained from fats, i.e.,
glycerides. Itisbelievedthatglycerolisespeciallyeffectiveat
passivating aluminum within the slurry.
0026 Suitableamountsforthestabilizerintheslurrycom
positionarebelievedtobein a rangeofabout0.1% byweight
to about 20% by weight, for example about 0.5% to about
15% by weight, based on the total weight ofthe slurry com
position. The amount of stabilizer will depend on various
factors includingthespecifictypeofstabilizerused,itswater
miscibility, the effectofthe stabilizeron the viscosity ofthe
slurry composition, the amount of metallic powder in the
slurry composition, the particle sizes ofthe metallic powder,
the surface-to-volume ratio ofthe powder particles, the spe
cific techniqueused topreparethe slurry, andthepresence of
any other components in the slurry composition. For
example, ifused in Sufficient quantities, the stabilizer might
becapableofpreventing or minimizinganyundesirable reac
tion between the metallic powder and any phosphoric acid
presentin the slurry. The organic stabilizer maybepresent in
anamountsufficienttochemicallystabilizethe metallicpow
der during contact with water or any other aqueous compo
nents ofthe slurry, meaning that slurry remains substantially
free of undesirable chemical reactions, including those that
would increase the Viscosity and/ortemperature ofthe com
position to unacceptable levels. For example, unacceptable
increases in temperature or viscosity are those which could
prevent the slurry composition from being easily applied to
Jun. 30, 2016
the under-platform regions 18, e.g., by spraying. As a very
general guideline, compositions deemed to be unstable are
those that exhibit (e.g., aftera short induction period) a tem
perature increase ofgreater than about 10° C. within about
one minute, or greater than about 30° C. within about ten
minutes. In thealternative (orin conjunction with atempera
tureincrease), thesecompositions mayalsoexhibitunaccept
able increases in viscosity overa similar time period.
0027. The slurry compositions may also contain various
other ingredients as well, including compounds known to
those involved in slurry preparations. Examples include
thickening agents, dispersants, deflocculants, anti-settling
agents, anti-foaming agents, plasticizers, emollients, Surfac
tants,andlubricants. Ingeneral.Suchadditivesmaybeusedat
alevel inthe rangeofabout0.01%byweightto about 10%by
weight,based on the weight ofthe entire slurry composition.
0028. As mentionedabove, theslurrycomposition maybe
aqueous. In other words, it includes a liquid carrier (e.g., the
medium in which the colloidal silica is employed) that is
primarily orentirely water. As usedherein, “aqueous” refers
to slurry compositions in which atleastabout 65% and pref
erably at least about 80% of the volatile components are
water. Thus,a limitedamount ofotherliquids maybeused in
admixture with the water. Examples of the other liquids or
“carriers' includealcohols, forexample, loweralcohols with
1-4 carbon atoms in the main chain, suchasethanol. Haloge
natedhydrocarbonsolventsareanotherexample. Selectionof
a particular carrier composition will depend on various fac
tors, such astheevaporation rate requiredduring treatmentof
theunder-platform regions 18withtheslurry,theeffectofthe
carrier on the adhesion of the slurry to the under-platform
regions 18, the solubility ofadditives and other components
in the carrier, the “dispersability” ofpowders in the carrier,
thecarrier's ability to wet the under-platform regions 18and
modify the rheology of the slurry composition, as well as
handling requirements, cost requirements, and environmen
tal/safety concerns.
0029. A suitable amount of liquid carrier employed is
usually the minimum amount Sufficient to keep the Solid
componentsoftheslurryinSuspension.Amountsgreaterthan
that level may be used to adjust the viscosity of the slurry
composition, depending on the technique used to apply the
composition. In general, the liquid carrier will typically con
stitute about 10% by weight to about 30% by weight, for
example about 20% by weight, ofthe entire slurry composi
tion. It should be noted that the slurry is termed a solid-in
liquid emulsion.
0030 The use of this slurry composition is especially
advantageous for enhancing the chromium content (and
optionally the aluminum content) of the under-platform
regions 18 turbine blades 10 formed ofsuperalloy materials,
though its application to other metal Substrates is also within
the scope ofthe invention. The term "superalloy' is usually
intended to embrace complex cobalt, nickel, and iron-based
alloys that include one or more otherelements, such as chro
mium,rhenium,aluminum,tungsten,molybdenum,titanium,
etc. Superalloys are described in many references, including
U.S. Pat. No. 5,399,313, which is incorporated herein by
reference. The actual configurationofblades treatedwith the
slurry composition of this invention may vary widely, and
therefore can differ from that shown in FIG. 1.
0031. The slurry coatings can be applied to the under
platform regions 18 by a variety oftechniques known in the
art. Someexamples ofthedepositiontechniquesslip-casting,
US 2016/0184890 A1
brush-painting, dipping, spraying, pouring, rolling, or spin
coating onto the Surfaces ofthe under-platform regions 18.
Spray-coating is onewaytoapply theslurry coatingto under
platform regions 18 ofthe turbine blade 10. The viscosity of
thecoatingcanbereadilyadjustedforsprayingby varyingthe
amount ofliquid carrier used.
0032. The slurry can be applied as one layer or multiple
layers. Multiple layers may sometimes be required to deliver
the desiredamountofchromium metal to the under-platform
regions 18. Ifa series oflayers is used, a heat treatment may
be performed after each layer is deposited to accelerate
removalofthevolatilecomponents.Afterthefullthicknessof
theslurryhasbeenapplied,the slurrycoatingmaybeallowed
to “air dry” before further processing to form the final coat
ing.Alternativelyand/oradditionally,aheattreatmentmaybe
carried out to further remove volatile materials, such as the
organic solvents andwater. An exemplary heatingregimen is
about five minutes to about two hoursata temperature in the
rangeofabout80° C. to about200° C. (about 176°F. to about
392 F.). Longer heating times can compensate for lower
heating temperatures, and Vice versa.
0033. The uniformly applied slurry coating may also be
'cured to provideagreen coating. Forexample, the compo
nent or article (e.g. turbine blade) with the applied slurry
coating may be heated to about 150° C. for one hour. Such
treatmentmaybesufficienttoremove volatiles,e.g. waterand
glycerol, from the slurry coating.
0034. Thegreencoating may thenbeheated to a tempera
ture sufficient to sinter the slurry coating and diffuse the
chromium (and, ifpresent, aluminum and/or other metallic
species) into the near-surface regions ofthe under-platform
regions 18 andto sinterthe green coatinginto a final coating.
As used herein, a “near-Surface region'extendsto a depth of
up to about 200 um into the surface of the under-platform
regions 18, typicallya depthofabout75 um and preferablyat
least 25um into the Surface, and includes both a chromium
enriched region closestto the Surface and an area ofinterdif
fusion immediately below theenriched region. Temperatures
required forthis chromizing step (i.e., the diffusiontempera
ture) will depend on various factors, including the composi
tion ofthe under-platform regions 18, the specific composi
tion and thickness of the slurry, and the desired depth of
enhanced chromium concentration. Usually the diffusion
temperature is within the range ofabout 650° C. to about
1100° C. (about 1200° F. to about 2010 F), for example
about800° C. to about950° C.(about 1472°F. toabout 1742
F.). These temperatures are also high enough to completely
remove (by vaporization or pyrolysis) any organic com
pounds present, including stabilizers such as glycerol. The
diffusion heattreatmentcanbe carried outbyany convenient
technique, including heating in a vacuum or inert gas within
a OVC.
0035. The time required for the diffusion heat treatment
will depend on the factors described above. Generally, the
time will range from about thirty minutes to about eight
hours. In some instances, a graduatedheattreatmentis desir
able. As a very general example, the temperature could be
raised to about 650° C., held there for a period oftime, and
then increased in steps to about 850° C. Alternatively, the
temperature could initially be raised to a threshold tempera
turesuch as 650° C. and then raisedcontinuously, e.g., about
1° C. per minute, to reach a temperature ofabout 850° C. in
about 200 minutes.
Jun. 30, 2016
0036 Alternatively, thegreencoating maybe subjected to
a packCVD vapor phase chromide process to form the final
coating. Processparametersoftemperature,gas flow rate,and
chromium chloride concentration may be selected to control
thedepositionrate.Thetransformationofthegreencoatingto
the final coating by the packCVD process allows forthe use
ofless aluminum and provides a reduction in the porosity of
the final coating. A thicker coating, for example a coating
havinga thicknessofup toabout 1.75 mil (about45 nm), may
beproduced by the pack CVD process. The pack CVD pro
cess is also less sensitive to the slurry powder particle size
distribution because ofthe reduced porosity ofthe coating.
The coating also has a metallurgical bond with the Substrate
ofthecomponentorarticlebecauseitisa diffusion bond.The
coating also provides an alpha chromium structure which is
highly corrosion resistant.
0037. It is to be understood that not necessarily all such
objects or advantages described above may be achieved in
accordance with any particular example. Thus, the systems
and techniques describedherein may beembodiedorcarried
out in a manner that achieves or optimizes one advantage or
group of advantages as taught herein without necessarily
achieving other objects or advantages as may be taught or
Suggested herein.
0038. While only certain features ofthe present technol
ogy have been illustrated and described herein, many modi
fications and changes will occur to those skilled in the art. It
is, therefore, to be understood that the appended claims are
intended to coverall Such modifications and changes.
What is claimed is:
1. A slurry coating composition for enriching a surface
region ofa metal-based substrate with chromium, the slurry
coating composition comprising:
a metallic powderincludingchromiumpowderintheCr(O)
oxidation state and aluminum powder,
abinderincludingcolloidal silicato bind themetallicpow
der; and
a stabilizer, wherein the chromium powder comprises at
least about 80% by weight of the metallic powder and
the aluminum powder comprises up to about 10% by
weight ofthe metallic powder.
2. The slurry coating composition according to claim 1,
whereinaparticlesizedistributionofthechromiumpowderis
about 1 to 5um.
3. The slurry coating composition according to claim 1,
whereinaparticlesizedistributionofthealuminumpowderis
about 10 to 14 um.
4. The slurry coating composition according to claim 1,
wherein the metallic powder is present in the slurry coating
composition ata rangeofabout 25% by weight toabout80%
by weight ofthe slurry coating composition.
5. The slurry coating composition according to claim 1,
whereinthecolloidalsilicacomprisesaliquid carrierselected
from the group consisting of water, alcohols, halogenated
hydrocarbon solvents, and compatible mixtures thereof.
6. The slurry coating composition according to claim 1,
wherein the colloidal silica is present in the slurry coating
composition at a range ofabout 1% by weight to about 25%
by weight, based on silica Solids as apercentage ofthe slurry
coating composition.
7. The slurry coating composition according to claim 1,
wherein the silica in the colloidal silica has an average par
ticle size in the range ofabout 10 nanometers to about 100
nanometerS.
US 2016/0184890 A1
8. The slurry coating composition according to claim 1,
wherein the stabilizer is present at a range ofabout 0.1% by
weight to about 20% by weight.
9. A process offorming a coating and enriching a Surface
region ofa component formed ofa nickel-based Superalloy
with chromium, the process comprising:
applyingtheslurrycoatingcompositionaccordingtoclaim
1 to the Surfaceregion ofthe componenttoforma slurry
coating on the Surface region;
curing the slurry coating to form a green coating; and
sintering the green coating to form a coating having chro
mium in the alphaphase at an operatingtemperature of
the component between about 1200° C. to about 1800°
C.
10. The process according to claim 9, wherein curing the
slurry coating comprises heating the coated component at
about 150° C. for about one hour.
11.Theprocessaccordingto claim.9,wherein sinteringthe
green coating comprises Subjecting the coated component to
a packCVD vapor phase chromide process.
11.Theprocessaccordingto claim.9,wherein sinteringthe
green coatingdiffusesthe metallicchromium intotheSurface
region at a depth of between about 25 um to about 200
micrometers.
12. The process according to claim 9, wherein sintering
comprises heating the coated component to between about
650° C. to about 1100° C.
13. A nickel-based Superalloy component ofa gas turbine
engine having a coating and Surface region enriched with
chromium formed by the process ofclaim 9.
14. The component according to claim 13, wherein the
coating is at least about 45 um thick.
15. A slurry coating composition for enriching a Surface
region ofa metal-based substrate with chromium, the slurry
coating composition comprising:
Jun. 30, 2016
a metallic powderincludingchromiumpowderintheCr(O)
oxidation state powder;
abinderincludingcolloidal silicato bind themetallicpow
der; and
a stabilizer.
16.A process offorminga coating andenrichingasurface
region ofa component formed ofa nickel-based Superalloy
with chromium, the process comprising:
applyingthe slurrycoatingcompositionaccordingtoclaim
15 to the surface region of the component to form a
slurry coating on the Surface region;
curing the slurry coating to form a green coating; and
sintering the green coating to form a coating having chro
mium in the alphaphaseat an operating temperature of
the component between about 1200° C. to about 1800°
C.
17. A slurry coating composition for enriching a surface
region ofa metal-based substrate with chromium, the slurry
coating composition consisting of:
a metallic powderincludingchromiumpowderintheCr(O)
oxidation state;
abinderincludingcolloidal silicato bind themetallicpow
der; and
a stabilizer.
18.A process offorminga coating andenrichingasurface
region ofa component formed ofa nickel-based Superalloy
with chromium, the process comprising:
applyingthe slurrycoatingcompositionaccordingtoclaim
17 to the surface region of the component to form a
slurry coating on the Surface region;
curing the slurry coating to form a green coating; and
sintering the green coating to form a coating having chro
mium in the alphaphaseat an operating temperature of
the component between about 1200° C. to about 1800°
C.

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Us20160184890 a1

  • 1. (19) United States US 2016O184890A1 (12) Patent Application Publication (10) Pub. No.: US2016/0184890 A1 KOOL et al. (43) Pub. Date: Jun. 30, 2016 (54) CHROMIDE COATINGS, ARTICLES COATED WITH CHROMIDE COATINGS, AND PROCESSES FOR FORMING CHROMIDE COATINGS (71) Applicants:Lawrence Bernard KOOL, Clifton Park, NY (US); Bhupendra Kumar GUPTA, Cincinnati, OH (US); Mark ROSENZWEIG, West Chester, OH (US); Samar Jyoti KALITA, Cincinnati, OH (US) (72) Inventors: Lawrence Bernard KOOL, Clifton Park, NY (US); Bhupendra Kumar GUPTA, Cincinnati, OH (US); Mark ROSENZWEIG, West Chester, OH (US); Samar Jyoti KALITA, Cincinnati, OH (US) (73) Assignee: GENERAL ELECTRIC COMPANY., Schenectady, NY (US) (21) Appl. No.: 14/585,890 (22) Filed: Dec. 30, 2014 Publication Classification (51) Int. Cl. B22F I/O (2006.01) C23C I6/56 (2006.01) C23C I6/44 (2006.01) (52) U.S. Cl. CPC ................. B22F I/007(2013.01); C23C I6/44 (2013.01); C23C I6/56 (2013.01) (57) ABSTRACT Aslurry coatingcomposition forenrichingasurfaceregion of a metal-based Substrate with chromium includes a metallic powder including chromium powder in the Cr(O) oxidation state and aluminum powder, a binder including colloidal silica to bind the metallic powder; and a stabilizer, wherein the chromium powder comprises at least about 80% by weight of the metallic powder and the aluminum powder comprisesup to about 10%by weightofthe metallicpowder. Aprocess offormingacoatingandenrichingaSurfaceregion of a component formed of a nickel-based Superalloy with chromium includes applying the slurry coating composition to the Surface region ofthe component to form a slurry coat ing on the Surface region; curing the slurry coating to form a green coating; and sinteringthegreen coating to form acoat ing having chromium in the alpha phase at an operating temperature of the component between about 1200° C. to about 1800°C.A nickel-basedsuperalloycomponentofagas turbineenginehasacoatingandSurface regionenrichedwith chromium formed by the process.
  • 2. Patent Application Publication Jun. 30, 2016 Sheet 1 of4 US 2016/O184890 A1 FIG. 1
  • 3. Patent Application Publication Jun. 30, 2016 Sheet 2 of4 US 2016/O184890 A1 S S & r& 8 $S S &
  • 4. Patent Application Publication Jun. 30, 2016 Sheet 3 of4 US 2016/O184890 A1
  • 5. US 2016/O184890 A1 008 w VESWH,VINE)IS000|| Jun. 30, 2016 Sheet 4 of4 SWH WHTW 00y??O 000Z PatentApplication Publication
  • 6. US 2016/0184890 A1 CHROMIDE COATINGS, ARTICLES COATED WITH CHROMIDE COATINGS, AND PROCESSES FOR FORMING CHROMIDE COATINGS BACKGROUND 0001. The present technology generally relates to protec tivecoating systems suitableforcomponentsexposedtohigh temperatures,suchasthehostilethermalenvironmentofagas turbine engine. More particularly, the present technology relatestoslurrycoatingcompositionsandprocessesforselec tivelyenrichingSurfaceregionsofacomponent,forexample, theunder-platformregionsonaturbineblade,with corrosion resistant metals such as chromium. 0002 Components ofturbine engines, such as the blades andVanes (nozzles)within theturbinesection ofagasturbine engine, are often formed of an iron, nickel, or cobalt-base superalloy. A turbine blade has an airfoil against which hot combustion gases are directed during operation of the gas turbine engine, and whose Surface is therefore subjected to severeattackby oxidation, corrosion and erosion. The blade further includes a platform and an under-platform or root section separated from the airfoil by the platform that, while not directly exposedto hotgas path, are still exposedto high temperatures and are susceptible to oxidation and corrosion. Turbinebladesorbucketsaretypicallyanchoredtotheperim eterofa rotororwheelby formingthe rotortohaveslots with dovetail cross-sections that interlock with a complementary dovetail profile on the root section ofeach blade. 0003. Due to the severity oftheiroperatingenvironments, turbine bladesoften requireenvironmentally protective coat ings on the Surfaces oftheirairfoilsandplatforms exposedto the hot gas path. Diffusion coatings Such as chromide, alu minide, and platinum aluminide coatings are widely used as environmental coatings in gas turbine engine applications because oftheir oxidation resistance. Such coatings, which aretypically appliedtothe internaland external Surfaces ofa blade, are produced by a thermal/chemical reaction process that results in the near-surface region ofthe Substrate being enriched with, depending on the type ofcoating, chromium, aluminum, platinum, etc., as well as intermetallics that form as a result of reactions between the deposited corrosion resistant specie?(s) andthe Substrate material. Diffusion coat ing processes typically take place in a reduced and/or inert atmosphere at elevated temperatures. Common processes include pack cementation and noncontact vapor (gas phase) deposition techniques, or by diffusing corrosion-resistant species deposited by chemical vapor deposition (CVD) or slurry coating. 0004. In pack cementation and noncontact vapor deposi tiontechniques, vaporofthedesiredcorrosion-resistant coat ingspecies (e.g.,chromium,aluminum, etc.) isgeneratedand caused to contact Surfaces on which the coating is desired. The vapor reacts with the surface to deposit the desired coat ing specie?s), whicharethen diffusedintotheSurfacethrough a heat treatment. Aluminide diffusion coatings deposited by pack cementation or noncontact vapor deposition are often preferred for turbine blade airfoils. The dovetails ofturbine blades are typically machined prior to the diffusion coating process, and may be masked during coating so thatthe dove tail will properly assemble with the dovetail slot in the rotor during engine build. However, during engine operation the under-platform regions oftheblade can become corroded. In the past, corrosion of under-platform regions of turbine Jun. 30, 2016 blades has been addressed by applying a vapor-phase chro mide coating. While capable of improving corrosion resis tance, vapor-phase chromizingprocesses require masking to prevent the chromide coating from being deposited on other surfaces oftheblade, such as thosealready provided with an aluminide coating. However, masking is time-consuming, expensive, and not always effective. 0005 Slurryprocessesgenerallyentail theuseofanaque ous or organic solvent slurry containing a volatile liquid vehicleandapowderofthe corrosion-resistantcoatingspecie (s) that can be sprayed or otherwise applied to a Substrate, after which the substrate is heated to evaporate the volatile componentsoftheslurryand,withfurtherheating, diffusethe remainingcoatingspeciesintotheSubstrate.Anexampleofa slurry composition is disclosed in U.S. Pat. No. 3.248,251 as containing aluminum particulates dispersed in an aqueous, acidic bonding solution that also contains metal chromate, dichromateor molybdate, andphosphate (the latterofwhich serves as a binder). The chromate ions are known to improve corrosion resistance. One prevalent theory described in U.S. Pat. No. 6,074,464 is that chromate ions passivate the bond ing Solution toward aluminum and inhibit the oxidation of metallicaluminum. Inthis manner,particulatealuminum can be combined with the bonding solution without undesirable reactions between the solution and aluminum. 0006. A drawback of slurry compositions of the type taught by the priorart discussed above is the reliance on the presence of chromates, which are considered toxic. In par ticular, hexavalent chromium is considered to be a carcino gen. When compositions containing this form ofchromium are used (e.g., in spray booths), special handling procedures that must be closely followed to satisfy health and safety regulations can result in increased costs and decreased pro ductivity. Therefore, attempts have been made to formulate slurry compositions which do not rely on the presence of chromates. For example, U.S. Pat. No. 6,150,033 describes chromate-free coating compositions used to protect metal Substrates Such as stainless steel. Many ofthe compositions disclosed in this patent are based on an aqueous phosphoric acid bonding Solution, which comprises a source of magne sium, Zinc, and borate ions. However, chromate-free slurry compositions can have various disadvantages, such as insta bility overthecourse ofseveral hours (oreven minutes), and generation of unsuitable levels of gases such as hydrogen. Furthermore, chromate-free slurry compositions have been known to thicken or partially solidify, rendering them very difficult to apply to a substrate by spray techniques. More over,theuse ofphosphoricacidin thecompositions may also contribute to instability, especially if chromate compounds are not present since the latterapparently passivates the Sur faces ofthealuminum particles. In the absenceofchromates, phosphoric acid may attack the metallic aluminum particles in the slurry composition, rendering the composition ther mally and physically unstable. Atbest. Such a slurry compo sition will be difficultto store and apply to a substrate. 0007. In view ofthe above, there are ongoing efforts to develop new slurrycompositionscapableofformingenviron mentally-protective coatings on Substrates. Such composi tions should be capable ofincorporating as much corrosion resistantspeciesas necessary intoaSubstrate,andshouldalso be substantially free of chromate compounds, especially hexavalent chromium. Moreover, improved slurry composi tionsshouldbechemically andphysically stableforextended periods ofuseand storage, amenableto slurryapplication by
  • 7. US 2016/0184890 A1 various techniques such as spraying, painting, and the like, and should be generally compatible with other techniques which might be used to treat a particular metal substrate, for example, Superalloy components such as turbine blades. SUMMARY 0008. In accordance with an example of the technology disclosedherein,aslurry coating composition forenrichinga Surface region of a metal-based Substrate with chromium comprises a metallic powder including chromium powder in the Cr(O) oxidation state and aluminum powder; a binder including colloidal silica to bind the metallic powder; and a stabilizer, wherein the chromium powder comprises at least about 80% by weight ofthe metallic powderand the alumi num powder comprises up to about 10% by weight ofthe metallic powder. 0009. In accordance with an example of the technology disclosedherein,amethodofformingacoatingandenriching a Surface region of a component formed of a nickel-based Superalloy with chromium comprises applying the slurry coatingcompositiontotheSurfaceregionofthecomponentto form a slurry coating on the Surface region; curing the slurry coatingto form a green coating; and sinteringthe green coat ing to form a coatinghaving chromium in the alphaphase at an operating temperature of the component between about 1200° C. to about 1800° C. 0010. In accordance with an example of the technology disclosed herein, a nickel-based Superalloy component ofa gas turbine enginehas a coatingand Surface region enriched with chromium formed by the process. BRIEF DESCRIPTION OF THE DRAWINGS 0011. Theseandotherfeatures, aspects,andadvantagesof the present technology will become better understood when thefollowingdetailed descriptionis readwith referencetothe accompanying drawings in which like characters represent like parts throughout the drawings, wherein: 0012 FIG. 1 schematically depicts a turbine component that may be coated according to the present technology; 0013 FIG. 2 depicts a coatingaccording to an exampleof the present technology; 0014 FIG.3 depicts a coatingaccording to an exampleof the present technology; 0015 FIG. 4 depicts a coatingaccording to an exampleof the present technology; 0016 FIG.5 depicts a coatingaccording to an exampleof the present technology; and 0017 FIG. 6 depicts a phase diagram ofa Ni Cralloy. DETAILED DESCRIPTION 0018. The slurry coating compositions andprocess ofthe presenttechnology may be usedto selectively enrich Surface regions of Substrates with chromium, and also aluminum if desired. One application may be the under-platform regions onturbineblades ofgas turbineengines. Referring to FIG. 1, ahighpressureturbineblade 10 includes anairfoil 12against which hot combustion gases are directed during operation of the gas turbine engine, and whose Surface is therefore Sub jected to severe attack by oxidation, corrosion, (e.g. hot Sul fate corrosion), and erosion. The blade 10 is anchored to a turbine disk (not shown) with a dovetail 14 formed on a root section oftheblade 10.Aplatform 16 separates the airfoil 12 and the dovetail 14, and the root section, its dovetail 14, and Jun. 30, 2016 the underside of the platform 16 are referred to as under platform regions 18 of the blade 10. Though not directly exposed to the hot gas path of a turbine engine, the under platform regions 18 are nonetheless Susceptible to oxidation and corrosion that may be induced by Sulfurcontaining dirt, debris, and/ordeposits entrained in the cooling airthat flows aroundthe under-platform region oftheblade. Slurry coating compositionsandprocessesofthepresenttechnology maybe used to selectively form a chromium-containing coating on the surfaces ofthe under-platform regions 18 oftheblade 10 ofFIG. 1, as well as surfaces ofothercomponents similarly Subjected to oxidation and corrosion. Examples ofthe coat ingsthatmaybeappliedby thepresenttechnology areshown in FIGS. 2-5. 0019 Referringto FIG. 6, a Ni–Crphasediagramshows that at temperatures from about 1200° C. (approximately 2200 F) to about 1800° C. (approximately 3270° F.), the alpha phase ofchromium exists from about 78-100at.%. In orderto obtainanalphaphase chromium coatingappliedto a nickelbased Superalloy gas turbinecomponent, e.g.aturbine blade, at operating temperatures ofthe component, the at. 96 ofthechromium in the coatingshouldbe at least78%. Given thesimilaratomic massesofCrandNi,themetallicpowderof the slurry coating composition may be about 80-100% by weight Cr. The slurry coating composition may include Cr powderintheCr(O)oxidationstate, i.e.hexavalentfree,and is therefore not restricted as is Cr(VI), i.e. hexavalent chro mium. The slurry powder particle size distribution may be from about 1 to 5um. 0020. The composition of the chromium-based powder and its amount in the slurry composition may depend on the amount ofchromium desired for the under-platform regions 18. In general, Suitableamounts ofchromium and optionally aluminum in the slurry composition should exceed their respectiveamounts inthesubstratetobeprotected.Thechro mium content ofthe slurry composition should be sufficient to compensate for any projected loss ofchromium from the under-platform regions 18 under expected operating condi tions, such as temperatures, temperature/time schedules and cycles, and environmental conditions. 0021. In addition to Cr, the metallic powder ofthe slurry coating composition may include aluminum to provide uni formity and enhance diffusion ofthe coating. TheAl powder particle size distribution may be from about 10-14 um and maybe up to about 10%, forexampleabout 1-5%, by weight of the metallic powder. Other metals may be included to provide enhanced oxidation resistance, phase stability, envi ronmental resistance, and Sulfidation resistance. Metals that may be included in the powder ofthe slurry coating compo sition include Co, Fe, Ti, Ta, W, Re, Mo, Hf, Si, and Pt. The powder may also contain various other elements and other materials at impurity levels, e.g., less than about 1% by weight. 0022. The metallic powder may constitute, by weight, about25%toabout80%, morepreferablyabout30% toabout 50%, ofthe entire slurry composition. The powder particles maybe in the form ofspherical particles, though otherforms are possible as well. Such as wire, wire mesh, and those described above for the colloidal silica. The metallicpowder canbeusedina variety ofstandardsizes.Acceptablesizes for the powder particles will depend on several factors. Such as the alloy ofthe under-platform regions 18, the technique by
  • 8. US 2016/0184890 A1 whichtheslurry istobeappliedto theunder-platform regions 18,andthepresenceandamounts ofotherpotential constitu ents in the slurry. 0023 Theslurrycoatingcompositionsofthepresenttech nology may include a binder, for example, a non-organic binder. One binder that may be used is colloidal silica. The term “colloidal silica” is meantto embrace any dispersion of fineparticlesofsilicainamediumofwateroranothersolvent, with waterbeingpreferredsuchthattheslurrycomposition is a water-based (aqueous) system. Dispersions of colloidal silica are available from various chemical manufacturers in eitheracidicorbasic form. Moreover, variousshapesofsilica particles can be used, e.g., spherical, hollow, porous, rod, plate, flake, or fibrous, as well as amorphous silica powder. Theparticles may have an average particle size in a range of about 10 nanometers to about 100 nanometers. Commercial examples of colloidal silica are available under the names LudoxR) from Sigma-Aldrich Co. LLC and Remasol(R) from REMETCorporation, ofUtica, N.Y., USA. 0024. The amount ofcolloidal silica present in the com position will depend on various factors, for example, the amount of metallic powder used and the presence (and amount) ofany other constituents in the slurry, for example, an organic stabilizer as discussed below. Colloidal silica appears tofunction primarily as a very effective binder in the slurry composition. Processing conditions are also a consid eration, forexample, how the slurry is formedandapplied to the under-platform regions 18. The colloidal silica may be present at a level in the range ofabout 1% to about 25% by weight, based on silica solids as a percentage ofthe entire composition. In especially preferred embodiments, the amountis in the rangeofabout 10% toabout20% by weight. 0025. In addition to the metallic powder and colloidal silica,theslurry compositions mayfurtherinclude othercon stituents, for example wetting agents and metal powder sta bilizers. One example of a wetting agent and Stabilizer is glycerol, CH3(OH), sometimes referred to as 'glycerin” or “glycerine.” Glycerol can readily be obtained from fats, i.e., glycerides. Itisbelievedthatglycerolisespeciallyeffectiveat passivating aluminum within the slurry. 0026 Suitableamountsforthestabilizerintheslurrycom positionarebelievedtobein a rangeofabout0.1% byweight to about 20% by weight, for example about 0.5% to about 15% by weight, based on the total weight ofthe slurry com position. The amount of stabilizer will depend on various factors includingthespecifictypeofstabilizerused,itswater miscibility, the effectofthe stabilizeron the viscosity ofthe slurry composition, the amount of metallic powder in the slurry composition, the particle sizes ofthe metallic powder, the surface-to-volume ratio ofthe powder particles, the spe cific techniqueused topreparethe slurry, andthepresence of any other components in the slurry composition. For example, ifused in Sufficient quantities, the stabilizer might becapableofpreventing or minimizinganyundesirable reac tion between the metallic powder and any phosphoric acid presentin the slurry. The organic stabilizer maybepresent in anamountsufficienttochemicallystabilizethe metallicpow der during contact with water or any other aqueous compo nents ofthe slurry, meaning that slurry remains substantially free of undesirable chemical reactions, including those that would increase the Viscosity and/ortemperature ofthe com position to unacceptable levels. For example, unacceptable increases in temperature or viscosity are those which could prevent the slurry composition from being easily applied to Jun. 30, 2016 the under-platform regions 18, e.g., by spraying. As a very general guideline, compositions deemed to be unstable are those that exhibit (e.g., aftera short induction period) a tem perature increase ofgreater than about 10° C. within about one minute, or greater than about 30° C. within about ten minutes. In thealternative (orin conjunction with atempera tureincrease), thesecompositions mayalsoexhibitunaccept able increases in viscosity overa similar time period. 0027. The slurry compositions may also contain various other ingredients as well, including compounds known to those involved in slurry preparations. Examples include thickening agents, dispersants, deflocculants, anti-settling agents, anti-foaming agents, plasticizers, emollients, Surfac tants,andlubricants. Ingeneral.Suchadditivesmaybeusedat alevel inthe rangeofabout0.01%byweightto about 10%by weight,based on the weight ofthe entire slurry composition. 0028. As mentionedabove, theslurrycomposition maybe aqueous. In other words, it includes a liquid carrier (e.g., the medium in which the colloidal silica is employed) that is primarily orentirely water. As usedherein, “aqueous” refers to slurry compositions in which atleastabout 65% and pref erably at least about 80% of the volatile components are water. Thus,a limitedamount ofotherliquids maybeused in admixture with the water. Examples of the other liquids or “carriers' includealcohols, forexample, loweralcohols with 1-4 carbon atoms in the main chain, suchasethanol. Haloge natedhydrocarbonsolventsareanotherexample. Selectionof a particular carrier composition will depend on various fac tors, such astheevaporation rate requiredduring treatmentof theunder-platform regions 18withtheslurry,theeffectofthe carrier on the adhesion of the slurry to the under-platform regions 18, the solubility ofadditives and other components in the carrier, the “dispersability” ofpowders in the carrier, thecarrier's ability to wet the under-platform regions 18and modify the rheology of the slurry composition, as well as handling requirements, cost requirements, and environmen tal/safety concerns. 0029. A suitable amount of liquid carrier employed is usually the minimum amount Sufficient to keep the Solid componentsoftheslurryinSuspension.Amountsgreaterthan that level may be used to adjust the viscosity of the slurry composition, depending on the technique used to apply the composition. In general, the liquid carrier will typically con stitute about 10% by weight to about 30% by weight, for example about 20% by weight, ofthe entire slurry composi tion. It should be noted that the slurry is termed a solid-in liquid emulsion. 0030 The use of this slurry composition is especially advantageous for enhancing the chromium content (and optionally the aluminum content) of the under-platform regions 18 turbine blades 10 formed ofsuperalloy materials, though its application to other metal Substrates is also within the scope ofthe invention. The term "superalloy' is usually intended to embrace complex cobalt, nickel, and iron-based alloys that include one or more otherelements, such as chro mium,rhenium,aluminum,tungsten,molybdenum,titanium, etc. Superalloys are described in many references, including U.S. Pat. No. 5,399,313, which is incorporated herein by reference. The actual configurationofblades treatedwith the slurry composition of this invention may vary widely, and therefore can differ from that shown in FIG. 1. 0031. The slurry coatings can be applied to the under platform regions 18 by a variety oftechniques known in the art. Someexamples ofthedepositiontechniquesslip-casting,
  • 9. US 2016/0184890 A1 brush-painting, dipping, spraying, pouring, rolling, or spin coating onto the Surfaces ofthe under-platform regions 18. Spray-coating is onewaytoapply theslurry coatingto under platform regions 18 ofthe turbine blade 10. The viscosity of thecoatingcanbereadilyadjustedforsprayingby varyingthe amount ofliquid carrier used. 0032. The slurry can be applied as one layer or multiple layers. Multiple layers may sometimes be required to deliver the desiredamountofchromium metal to the under-platform regions 18. Ifa series oflayers is used, a heat treatment may be performed after each layer is deposited to accelerate removalofthevolatilecomponents.Afterthefullthicknessof theslurryhasbeenapplied,the slurrycoatingmaybeallowed to “air dry” before further processing to form the final coat ing.Alternativelyand/oradditionally,aheattreatmentmaybe carried out to further remove volatile materials, such as the organic solvents andwater. An exemplary heatingregimen is about five minutes to about two hoursata temperature in the rangeofabout80° C. to about200° C. (about 176°F. to about 392 F.). Longer heating times can compensate for lower heating temperatures, and Vice versa. 0033. The uniformly applied slurry coating may also be 'cured to provideagreen coating. Forexample, the compo nent or article (e.g. turbine blade) with the applied slurry coating may be heated to about 150° C. for one hour. Such treatmentmaybesufficienttoremove volatiles,e.g. waterand glycerol, from the slurry coating. 0034. Thegreencoating may thenbeheated to a tempera ture sufficient to sinter the slurry coating and diffuse the chromium (and, ifpresent, aluminum and/or other metallic species) into the near-surface regions ofthe under-platform regions 18 andto sinterthe green coatinginto a final coating. As used herein, a “near-Surface region'extendsto a depth of up to about 200 um into the surface of the under-platform regions 18, typicallya depthofabout75 um and preferablyat least 25um into the Surface, and includes both a chromium enriched region closestto the Surface and an area ofinterdif fusion immediately below theenriched region. Temperatures required forthis chromizing step (i.e., the diffusiontempera ture) will depend on various factors, including the composi tion ofthe under-platform regions 18, the specific composi tion and thickness of the slurry, and the desired depth of enhanced chromium concentration. Usually the diffusion temperature is within the range ofabout 650° C. to about 1100° C. (about 1200° F. to about 2010 F), for example about800° C. to about950° C.(about 1472°F. toabout 1742 F.). These temperatures are also high enough to completely remove (by vaporization or pyrolysis) any organic com pounds present, including stabilizers such as glycerol. The diffusion heattreatmentcanbe carried outbyany convenient technique, including heating in a vacuum or inert gas within a OVC. 0035. The time required for the diffusion heat treatment will depend on the factors described above. Generally, the time will range from about thirty minutes to about eight hours. In some instances, a graduatedheattreatmentis desir able. As a very general example, the temperature could be raised to about 650° C., held there for a period oftime, and then increased in steps to about 850° C. Alternatively, the temperature could initially be raised to a threshold tempera turesuch as 650° C. and then raisedcontinuously, e.g., about 1° C. per minute, to reach a temperature ofabout 850° C. in about 200 minutes. Jun. 30, 2016 0036 Alternatively, thegreencoating maybe subjected to a packCVD vapor phase chromide process to form the final coating. Processparametersoftemperature,gas flow rate,and chromium chloride concentration may be selected to control thedepositionrate.Thetransformationofthegreencoatingto the final coating by the packCVD process allows forthe use ofless aluminum and provides a reduction in the porosity of the final coating. A thicker coating, for example a coating havinga thicknessofup toabout 1.75 mil (about45 nm), may beproduced by the pack CVD process. The pack CVD pro cess is also less sensitive to the slurry powder particle size distribution because ofthe reduced porosity ofthe coating. The coating also has a metallurgical bond with the Substrate ofthecomponentorarticlebecauseitisa diffusion bond.The coating also provides an alpha chromium structure which is highly corrosion resistant. 0037. It is to be understood that not necessarily all such objects or advantages described above may be achieved in accordance with any particular example. Thus, the systems and techniques describedherein may beembodiedorcarried out in a manner that achieves or optimizes one advantage or group of advantages as taught herein without necessarily achieving other objects or advantages as may be taught or Suggested herein. 0038. While only certain features ofthe present technol ogy have been illustrated and described herein, many modi fications and changes will occur to those skilled in the art. It is, therefore, to be understood that the appended claims are intended to coverall Such modifications and changes. What is claimed is: 1. A slurry coating composition for enriching a surface region ofa metal-based substrate with chromium, the slurry coating composition comprising: a metallic powderincludingchromiumpowderintheCr(O) oxidation state and aluminum powder, abinderincludingcolloidal silicato bind themetallicpow der; and a stabilizer, wherein the chromium powder comprises at least about 80% by weight of the metallic powder and the aluminum powder comprises up to about 10% by weight ofthe metallic powder. 2. The slurry coating composition according to claim 1, whereinaparticlesizedistributionofthechromiumpowderis about 1 to 5um. 3. The slurry coating composition according to claim 1, whereinaparticlesizedistributionofthealuminumpowderis about 10 to 14 um. 4. The slurry coating composition according to claim 1, wherein the metallic powder is present in the slurry coating composition ata rangeofabout 25% by weight toabout80% by weight ofthe slurry coating composition. 5. The slurry coating composition according to claim 1, whereinthecolloidalsilicacomprisesaliquid carrierselected from the group consisting of water, alcohols, halogenated hydrocarbon solvents, and compatible mixtures thereof. 6. The slurry coating composition according to claim 1, wherein the colloidal silica is present in the slurry coating composition at a range ofabout 1% by weight to about 25% by weight, based on silica Solids as apercentage ofthe slurry coating composition. 7. The slurry coating composition according to claim 1, wherein the silica in the colloidal silica has an average par ticle size in the range ofabout 10 nanometers to about 100 nanometerS.
  • 10. US 2016/0184890 A1 8. The slurry coating composition according to claim 1, wherein the stabilizer is present at a range ofabout 0.1% by weight to about 20% by weight. 9. A process offorming a coating and enriching a Surface region ofa component formed ofa nickel-based Superalloy with chromium, the process comprising: applyingtheslurrycoatingcompositionaccordingtoclaim 1 to the Surfaceregion ofthe componenttoforma slurry coating on the Surface region; curing the slurry coating to form a green coating; and sintering the green coating to form a coating having chro mium in the alphaphase at an operatingtemperature of the component between about 1200° C. to about 1800° C. 10. The process according to claim 9, wherein curing the slurry coating comprises heating the coated component at about 150° C. for about one hour. 11.Theprocessaccordingto claim.9,wherein sinteringthe green coating comprises Subjecting the coated component to a packCVD vapor phase chromide process. 11.Theprocessaccordingto claim.9,wherein sinteringthe green coatingdiffusesthe metallicchromium intotheSurface region at a depth of between about 25 um to about 200 micrometers. 12. The process according to claim 9, wherein sintering comprises heating the coated component to between about 650° C. to about 1100° C. 13. A nickel-based Superalloy component ofa gas turbine engine having a coating and Surface region enriched with chromium formed by the process ofclaim 9. 14. The component according to claim 13, wherein the coating is at least about 45 um thick. 15. A slurry coating composition for enriching a Surface region ofa metal-based substrate with chromium, the slurry coating composition comprising: Jun. 30, 2016 a metallic powderincludingchromiumpowderintheCr(O) oxidation state powder; abinderincludingcolloidal silicato bind themetallicpow der; and a stabilizer. 16.A process offorminga coating andenrichingasurface region ofa component formed ofa nickel-based Superalloy with chromium, the process comprising: applyingthe slurrycoatingcompositionaccordingtoclaim 15 to the surface region of the component to form a slurry coating on the Surface region; curing the slurry coating to form a green coating; and sintering the green coating to form a coating having chro mium in the alphaphaseat an operating temperature of the component between about 1200° C. to about 1800° C. 17. A slurry coating composition for enriching a surface region ofa metal-based substrate with chromium, the slurry coating composition consisting of: a metallic powderincludingchromiumpowderintheCr(O) oxidation state; abinderincludingcolloidal silicato bind themetallicpow der; and a stabilizer. 18.A process offorminga coating andenrichingasurface region ofa component formed ofa nickel-based Superalloy with chromium, the process comprising: applyingthe slurrycoatingcompositionaccordingtoclaim 17 to the surface region of the component to form a slurry coating on the Surface region; curing the slurry coating to form a green coating; and sintering the green coating to form a coating having chro mium in the alphaphaseat an operating temperature of the component between about 1200° C. to about 1800° C.