Title of Invention

"A COMPOSITE WIRE FOR PRODUCING A WEAR RESISTANT AND CORROSION RESISTANT COATING ON A SUBSTRATE"

Abstract A COMPOSITE WIRE FOR PRODUCING A WEAR RESISTANT AND CORROSION RESISTANT COATING ON A SUBSTRATE The present invention relates to a composite wire for producing a wear resistant and corrosion resistant coating on a substrate, said composite wire consisting of a tubular metallic outer sheath encapsulating a powdered inner core, said inner core compring a mixture of boron carbide of at least 35 % by weight, and chrome carbide in an amount between 67 %-233 % by weight of the amount of boron carbide.
Full Text TECHNICAL FIELD
This application claims priority to U.S. provisionaL Application No. 60/476,875, filed on June 6, 2003. The present invention relates to coatings for substrates, particularly metallic substrates. More specifically, the invention relates to composite wires or cored wires for forming wear-resistant and corrosion-resistant coatings on metallic substrates by thermal spraying processes, spray and fuse processes, or by welding techniques. The invention also relates to methods of employing the composite or cored wires to apply wear-resistant and corrosion resistant coatings to substrates.
BACKGROUND ART
Thermal spraying, i.e. the generic name for a class of processes that allow the depositing molten of semi-molten materials onto a substrate to form a wear of corrosion resistant coating, has been known in various forms for many years. Thermal spraying processes include plasma, flame, arc-plasma, arc and combustion spraying. Arc spraying is a form of thermal spraying which involves feeding two electrically conductive wires towards one another so that an arc is struck between the tips of the wires to melt the wire tips . The molten material is then atomized and sprayed onto a substrate by compressed gas.
This form of thermal spraying is widely used to provide corrosion-resistant coatings on various metallic articles. For example, U.S. Patent No, 6,156,443 (Dallaire, et al .) discloses coatings that are formed by arc spraying cored wires onto metallic articles exposed to erodent particles. 'The cored wires are composed of a sheath of ductile metal, such as iron, low


1
carbon steel, or ductile stainless steel, and a core
coarse ferroboron particles. The resulting coatings are designed
to include iron boride phases having mean sizes equal to or
larger than the sizes at the erodent particles.
Another thermal spraying proecess is described in U.S. Patent
Mo. 5,837,336 (Daliaire, et al.), which discloses a process for
producing composite coatings comprising fine titanium diboride
particles or crystals distributed throughout a stainleass steel
matrix by are spraying cored wires onto a metallic substrate. The
cored wires typically comprise a stainless steel outer sheath and
an inner core of compacted powders including titanium diboride
and a metal or metal alloy. The particles or crystals in these
gs impart hardnese to the soft stainless steel matrix and
the resistance of the coatings to hard abrasive media.
The metal components of the cored wires used to form the
coatings disclosed in both U.S, Patent Nos. S,156,443 (Dallaire,
et a.l.) and 5,837,326 (Dallaire, et al.) are not highly alloyed,
and consequently the coatings tend to be susceptible to corrosion
attack in certain high temperature corrosive conditions, such as in
boiler applications.
Generally, the binder metal (i.e,, the metal of the outer
sheath) in a wear-rosistant coating is critical to the
performance of the coating in, corrosive conditions such as
those encountered in boilers, For example, coatings with ironbased
binder alloys, such as Armacor Mw, exhibit extensive
binder-material. corrosion in boiler conditions, resulting in
wear of the coatings. The consequent weaKening of the
can also lead to premature coating failure due to complete
of the protective layer. Furthermore, the magnetic
of these coatings prevent thickness
using standard equipment, such as Elcometers.
U.S. Patent Wo. 4,741,974 (Longo, et al.) disclosen a
e wire for forming wear resistant coatings wherein the
wire i s formed of. an alloy sheath having iron, nickel, or
cobalt as a major component. The core of the composites wire is
formed of powder that includes boron or boron carbide. Due to
its extremo hardness, boron carbide is employed in coatings
where. wear or abrasion is of primary concern. However, as with
other conventional composite wires, in high- temperature
corrosive environment, the wear resistant coatings may
experience accelerated wear.
DISCLOSORE OF. THE
Accordingly, a composites wire ie provided for producing a
wear resistant and corrosion resistant coating on a substrate by
thermal spraying, spray and fuses, or welding techniques. While
the coating produced by tho composite wire ot the present
invention is suitable for all temperature ranges, the physical
properties of the coating are particularly well suited, for hightemperature
erosion- corrosion environments. The reeultant
coating exhibits good hardness toughness, and bonding
characteristios. The composite wire generally comprises a
metallic outer sheath and an inner core containing boron carbide
(BC) and chrome carbide (CrC) . The metallic outer sheath may be
formed of an essentially pure metal or on alloy. As stated above,
the binder is generally considered to be critical to the performance
of a coating and the binder selection will depend -upon several
factors including the environment to which the coated substrate will
be exposed . The composite wire of the present invention is
manufactured by conventional techniques wherein the specially
formulated powder core is encapsulated by the outer sheath, The
terms "composite wire" and "cored wire" are used aynonymously herein
to describe such a w i r e . T h e chrome carbide/boron carbide
formulation of the inner core provides a substantial improvement to
conventional coatings deposited by conventional composite wires.
The combination of chorme carbide and boron carbide gives added wear
rosistance, increases metal binder hardness. improves bonding of the
coating to the substrate, and inhibits oxide formation.
The outer sheath may be constructed of any metal or alloy.
Suitable binder material includes, but is not limited ho, iron,
carbon and low alloy steels, stainless steels, nickel, nickel
alloys, such as nickel -copper, nickel-cbromium, nickel-chrome -iron,
and nickel -molybdenum alloys, copper, brasees, bronzes, aluminum
bronzes, aluminum, aluminum alloys (ixxx - 7xxx) , titanium, titanium
alloya, cobalt alloya, molybdenum and nolybdenum alloys, tantalum
and tantalum alloys. The combination of these binder with the
inner core powder of the present invention resulte in coatings
having superior physical properties over conventional coatings,
In addition to the composite wires discussed above, a method
of forming a wear resistant and corrosion resistant coating on a
substrate is also provided. The method generally include the
steps of providing a composite wire having and outor sheath
formed from a metal or alloy, and an inner core comprising boron
carbide and chrome carbide; and coating a substrste by employing
the composite wire in conjunction with thermal spraying, spray
and fuse or welding techniques,
BREIF DESCRIPTION OF THE
Figure I is an electron micrograph of a cross section of an
alloy 625 arc sprayed coating.
Figure 2 is an ojectron micrograph of a cross section of an
alloy 625/BC-CrC are sprayed coating,
BEST MODE FOR CARRYING OUT THE
In the following detailed description of the preferred
embodiments , it is to be understood that other embodiments may be
utilized and structural changes may bts made without departing
from the scope of the present invention.
The coatings according to the present invention are
specifically designed for articles subjected to wear and/or
corrosion. Such article include, for example, boiler tubes,
hydraulic piston rods/ pump casings, rollers in the paper and
steel industry, wear plates, journals and shafts, and turbine
blades and casings.
In one; application, the coatings are designed to protect
boiler tubes against erosion-corrosicn related wantage and arc
applied to the boiler tubes by means of a conventional arc
spraying apparatus. However, it will be appreciated from the
description bo low that the coatings could also be applied to
the boiler tubes by other thermal spraying apparatus employing
wires as the feed material using fusing equipment, or by suitable
welding techniques. Are opraying methods and apparatus are well
documented in the art, see for example, U.S, PatentNos.
5,155,443 (Dallaire, et al.) 5,837,326 (Dallaire, ct al.);
European Patent No. EP 0 522 438 [Zurccki et a l . ) ; and PCT
Patent No. WO 90/00574 (Seitz), the disclosures of which are
incorporated by reference.
The coatings of the present invention are formed from
composite wires, which are fed through a conventional arc
spraying apparatus, such as the apparatus disclosed in PCT Patent
No, WO 01/08810 (Seitz), the diaclonure of which is incorporated
herein by reference.
The composite wires of the present invention comprise an
outer sheath formed from a metal ox alloy. In one embodiment of
the invention, which is particularity for the high temperature
erosion-corrosion environment found in boiler application, the
cored wires comprise an outer tubular sheath formed from a chromium
bearing/ nickel base alloy such as an alloy 625, and an inner
core, which comprises boron carbide and chrome carbide.
The preferred inner core formulation preferably comprises
chrome carbide in an amount between about 25% and about 400% by
weight of the amount of boron carbide. In other words, the ratio of
carome carbide to boron carbide preferably ranges between about 1:1
to about 4:1. More preferably, the inner core comprises chrome
carbide in an amount between about 67% and about 230% by weight of
the amount of boron carbides. In other words, the ratio of chrome
carbide to boron carbide preferably rariges between about 1:1.5 to
about 2,3:1. In one preferred embodiment, the inner core comprises
about 100% by weight, of chrome carbide relative to the amount of
boron carbide, in other words the amounts of chrome carbide and
boron carbide are substantially equivalent.
The chrome carbide in the inner core incerases the wear
resistance at the deposited coating or weld overlay, The chrome
carbide is retained during the thermal apraying or welding, and is
present in molten form within the coating structure during
application. However, this benefit accrues on a eliding scale - the
more chrome carbide used the better the result, but at the expense
of displacing boron carbide and its benaficial effects. Conversely
most of the boron carbide does not appear to survive as a carbide
during application of the coating. The boron carbide breaks up in
the arc as uncontaminated boron and carbon, which both have
hardening effects. The hardening effect increases the
of: the metal of the outer steath through alloying and/or
diffusion procesees. Some of the larger particles of boron carbide
may curvive the are. Those particles add to the wear resistance,
much like the chrome carbide, but the resistance achieved with large
part idea of boron carbide is not as effective as that achieved with
chrome carbide. Furthermore, the boron carbide inhibits the
formation of oxides in the molten outer sheath during spraying. To
achieve this result, a sufficient amount of boron carbide should be
present in the inner core. Preferably, at leapt about 35% by weight
of the inner core should consist of boron carbide to achieve verylow
oxide formation. However, this; benefit accruen on a sliding
scale - the more boron carbide used the better the result, but at
the expense of displacing chrome carbide eind its beneficial effects.
In addition to preventing oxiclst formation, the boron carbide
6
also lowers the melting temperature of the binder material (except
for aluminum, which already has a low molting point) and improves
the properties of the metal matrix making up the
deposited coating. This gives fusing and self-fluxing properties to
the coating. Furthemore, there is an increase in the temperature
range of the liquid phase (i.e./ during melting or freezing).
The increased range improves the spray and also
improves the fusing characteristics.
In addition to the qualities described above, the coatings
of the present invention are to install and maintain.
The boron additions in the metal binder matrix and the chromes
carbide hard-phase morphology make repairs to the coatings
relatively easy. Added to this, the high bond strength and the
low coating residual allow existing coatings to be grit
blasted without diabonding the surrounding material.
While the inner coro formulation of the prasent invention
centers around chrome carbide and boror carbide the inner core
contain additional materials, additional may
includes carbides, such ae tungsten carbide, titanium carbide,
vanadium carbide, and the like; oxides, such ao aluminum oxide,
chronic oxide, zirconium oxide, raid and boridcn, such as
clii'orae boride, nickel borido., iron, boride, and the liko. The inner
core may also ir.clude additional metiil , such as alxuninum,
nickel, chrome, or alloy powder, or e powders, such as
tungsten carbide nickel arid chrome carbide tucke.1 chrome .
The of the chromium carbide and boron carbide will
have an effect on the physical properties of the applied coating.
Generally, the finer the grains of the , the more homogenous
the coating will be and generally the better the wear and corrosion
properties. However, the cost and manufacturing constraints will
limit the lower end of the grain size range. U.S. Patent No.
4,741,971 (Longor et al.), the disclosure of which is hereby
incorporated by reference, discloses thct effect of grain size with
to boron carbide.
EXAMPLES
A composite wires of the present invention was formed with
an outer sheath comprising of alloy 625 and an inner
core comprising a substantially equivalent mixture of chromes
carbide and boron carbide, INCONEL alloy 625 is a product of
the Special Metals Corporation and contain 0,3.% C/ 0,51- Mn, 5.00
Fe, 0.02 P, 0.0151- S/ 0.5% Si, 0.5-1 Cu, 58% min Ki, 0,4% Al,
0.41 Ti, 20.0% -23.0% Cr, 3,15-4.15% Nb+Ta, 8,0%10,0% Mo. This
composite wire provided coatings with good toughness
characteristics, low oxicleo, and good woar due to
the novel carbide formulation of the inner core. In addition,
there was an increase in the hardnese of the metal binder due to
the boron content The coatings also exhibited good bonding
characteristics. The following table illustrates the improved
wear resistant of a coatings deposited by a composite wire of the
present invention (row 3 and row 4] compared to the wear
ce of other coatings;
ASTM G6S Wear Test (1S minutes):
Coatings Height Lose (grams lost:/6QOO wheel
1) Bc Cr B (Arc) 0.429
2) pe Cr No Mn B (HVOF) 0.319
3) CrC/BC - Alloy 625 (Arc) 0,285
4) CrC/BC - Fe Cr (rc) 0.212
After PuDJpqf
3} CrC/BC - Alloy 6?,5 (Arc) 0.184
4) CrC/BC - Pe Cr (Arc) 0,165
Note that coatings of the present invention, as
above/ have low oxide content and thus have superior fusing
chracteristics. The wear resistances of the CrC/BC - Alloy 625
coating and the CrC/BC - Fa Cr coating were subtantially improved
upon fusing,
In addition to the improvement to wear resistance, the
overall strength of the metal binder was also substantially
increased. The coating deposited with the Alloy 625
composite wire exhibited an average hardness measurement of 003.2
100 g/Vickcrs/10 seconds. whereas, coatings of pure alloy 62S are
typically on the order of 280-350 3,00 g/Vickers/10 seconds.
To illustrate bond strength , clean, bright smooth
steel coupons were coated, without any surface roughness, to
establish how thick a coating could be sprayed before spalling
occurred {i,e., bond failure). The first coupon was are sprayed
with pure alloy 625 and the second coupon was sprayed with a
composite wire comprising an alloy 625 outer sheath and an inner
core comprising 40% by weight boron carbide arid 60% by weight
chromium carbide. The first coupon exhibited delamination at 300
whereas the coating applied in accordance with the present
invention way sprayed up to 2000 um without any appearance of
spalling.
Example 3:
Two clean steel coupons were coated, with grit-blasted
surfaces; the first with pure alloy 625 and the second with a
composite wire comprising an alloy 625 outer sheath and an inner
core comprising 400 by weight boron carbide and 60% by weight
chromium carbide. The coupons were necnanically damaged by
cracking off the coating with a hammer and chisel. The pure 625
coating was peeled off of the first coupon as a continuous layer,
while the composite wire sprayed coating could not be disjoined
from the coupon. Rather, the composite wire sprayed coupon only
sustained damage to the impact site thus illustrating the high
bond strength.
As stated above, in addition to good toughneas, wear
resistance, increased metal blinder hardness, and improved bonding of
Che coating to the substrate, the inner core formulation, of the
present invention also inhibits oxide formation. This
characteristic of the boron carbide/chrome carbide formulation is
illustrated in Figures l and 2.
Figure .1 shows a cross-sectional electron micrograph of a
coating sprayed with pure alloy 62S. The coating exhibits high
oxide content, which shows up in the micrograph as grey bands. Due
to the high oxide content, the alloy 635 coating will not fuse or
melt as alloy 625 would fuse or melit if it were oxide free.
Conversely, as can be sesn in Figure 2, the coating sprayed with an
alloy 62S/boron carbide-chrome carbide composite wire exhibits far
less oxide content and can be easily remeltod and fused.
While- alloy 625 in a preferred alloy for the outer sheath in
ccrcain high tempearature erosion-corrosion Applications,
alternative metals and alloy can alscs be employed. For examples,
alternative chrome bearing nickel baao alloys include alloy C-
276, alloy 586, or alloy 59Q. INCONEI/ C-276, alloy 68G, and
alloy 6.90, which are all produced by the Special Metals
Corporation contains: 0.021- C, 1.0% Mn, 4.0%-7vO% P&t 0.04% 2,
0.03% S, 0.08% Si, 0.5% Cu, bal. N.I, 2,5% Co, l4.16.5 Cr,
15.0%-17.0% Mo, 3.0%-4.5% W (JKCONEL C-27); 0.01% C, 1.0* Mn,
5.0% Fo, 0.02% P, 0.02% 8, 0.08% Si, 0.5% Cu, b a l . , O.S^ Al
0.2S% Ti, 19.0%23.0% Cr, 15,0%-17.C% Mo, 3.0%-4.4% W. (1NCONJ3L*
alloy 686); and 0.02% C, 1,0% Mn, 7.0%-11.0% Pe, 0,015% S, 0.5%
Si, 0.5% Cu, bal. Hi, 27%-31% Cr (INCONEL" alloy 690), Nickel
copper allloys, such aa alloy 400, alloy R-405, and the like, and
nickel molybdenum alloys much as, alloy B, alloy B-2, and the
like, may also be employed depending en the required physical
properties of the resulting coating and the environment to which
t-he coating will be exposed.
As stnted above, the metal, binder material is not limited to
nickel base alloys?, rather the outer sheath way be constructed of
any metal or alloy. Additional suitable binder material includes,
but is not limited to, iron, carbon and low alloy steels, stainless
steels, nickel, coppe.r, copper alloys (o.g./ brasses, bronzes, and
aluminum bronazes), aluminum, aluminum alloys (e.g., aluminumcopper,
nl aluminum-manganese, a aluminum-manganese -magaesium,
aluminum- silicon, aluminum- manganese-magniesium-chrorme aluminumm
- s i l i c o n , a n d a l u m i n u m - z i n c - c o p p e r ) ,
titanium, titanium alloys (e..g., titanium alloyed with palladium,:
molybdenum, nickel, aluminum, vanadium, niobium, tantalum, tin,
55 ir con ium, chromium and iron), cobalt, cobalt alloys (c.ci,, cobalt
alloyed with chromium, nickel, molybdenum and tungsten), zirconium,
zirconium alloys, tantalum and tantalum alloys. The combination of
any of thcae binders with the inner core powder ol the present
invention moults in coatings having superior phyaical properties
over conventional contings.
The cored wires may be formed in a conventional manner by
placing the mix of carbides, which need not be an agglomerated
mix, onto an alloy 62,5 strip, or a strip o£ some other outer
sheath alloy, which is drawn continuously through a plurality of
wire drawing dics to form an outer wire sheath around an inner
core. The final outer diameter of the cored wire will
upon the application for which it is used. For most
applications, the cored wire final diameter ranges between about 0.6
mm to about 6.4 mm. Conventional cored wire manufacturing
techniques are discloaed in U.S, Patent Application MOM, 6,156,443
(Dallaire et al.) »nd 6,S13,72B (Hughea ct al.), of which both
disclosures are hereby incorporated by reference.
Although the present invention has been described in terms
of specific embodiments, it io anticipated that alteration and
modifications there of will no doubt become apparent to those
skilled in the art. It is there fore intended that, the following
claims be interpreted as covering all alterations
modifications that fall within the truss spirit and scope of the




We claim:
1. A composite wire for producing a wear resistant and corrosion resistant coating on a substrate, said composite wire consisting of a tubular metallic outer sheath encapsulating an inner core characterized in that the inner core is powdered and said inner core comprises a mixture of boron carbide of at least 35% by weight, and chrome carbide in an amount between 67% and 233% by weight of the amount of boron carbide.
2. The composite wire as claimed in claim 1, wherein the outer sheath is formed of an essentially pure metal.
3. The composite wire as claimed in claim 1, wherein the outer sheath is formed of an alloy comprising a base metal.
4. The composite wire as claimed in claim 3, wherein the base metal of the alloy is selected from the group consisting of iron, nickel, aluminum, molybdenum, tantalum, copper, and titanium.
5. The composite wire as claimed in claim 3, wherein the alloy is a nickel based alloy.
6. The composite wire as claimed in claim 5, wherein the nickel base alloy contains chromium.
7. The composite wire as claimed in claim 6, wherein the nickel base alloy contains at least 40 % by weight of nickel.
8. The composite wire as claimed in claim 7, wherein the nickel based alloy contains molybdenum.
9. The composite wire as claimed in claim 8, wherein the nickel based alloy is an alloy 625.
10. The composite wire as claimed in claim 1, wherein the inner core contains substantially equivalent amounts of chrome carbide and boron carbide.
11. A method of forming a wear resistant and corrosion resistant coating on a substrate comprising the steps of: providing a composite wire as claimed in any of claims 1-16 and employing the wire to form the coating on the substrate.
12. The method as claimed in claim 17, wherein the step of employing the wire to form the coating comprises thermally spraying the wires onto the substrate.
13. The method as claimed in claim 17, wherein the step of employing the wire to form the coating comprises spraying the wires onto the substrate and fusing the coating.
14. The method as claimed in claim 17, wherein the step of employing the wire to form the coating comprises depositing the wires onto the substrate by welding techniques.

15. The method as claimed in claim 17, wherein the outer sheath is formed of an essentially pure metal.
16. The method as claimed in claim 17, wherein the outer sheath is formed of an alloy comprisng a base metal.
17. The method as claimed in claim 22, wherein the base metal of the alloy is selected from the group consisting of iron, nickel, aluminum, molybdenum, tantalum, copper, and titanium.
18. The method as claimed in claim 22, wherein the alloy is a nickel base alloy.
19. The method as claimed in claim 24, wherein the nickel base alloy contains chromium.
20. The method as claimed in claim 25, wherein the nickel base alloy contains at least 40 % by weight of nickel.
21. The method as claimed in claim 26, wherein the nickel base alloy contains molybdenum.
22. The method as claimed in claim 27, wherein the nickel base alloy is an alloy 625.
23. A substrate having a coating formed in accordance with the method as claimed in any of claims 11-22.

Documents:

5540-DELNP-2005-Abstract-(26-12-2008).pdf

5540-delnp-2005-abstract.pdf

5540-delnp-2005-Assignment-(02-05-2011).pdf

5540-DELNP-2005-Claims-(14-01-2009).pdf

5540-DELNP-2005-Claims-(26-12-2008).pdf

5540-delnp-2005-claims.pdf

5540-delnp-2005-Correspondence-Others-(02-05-2011).pdf

5540-DELNP-2005-Correspondence-Others-(14-01-2009).pdf

5540-DELNP-2005-Correspondence-Others-(26-12-2008).pdf

5540-delnp-2005-correspondence-others.pdf

5540-DELNP-2005-Description (Complete)-(26-12-2008).pdf

5540-delnp-2005-description (complete).pdf

5540-DELNP-2005-Drawings-(26-12-2008).pdf

5540-delnp-2005-drawings.pdf

5540-delnp-2005-Form-1-(02-05-2011).pdf

5540-DELNP-2005-Form-1-(26-12-2008).pdf

5540-delnp-2005-form-1.pdf

5540-delnp-2005-form-13-(21-11-2006).pdf

5540-delnp-2005-form-13.pdf

5540-delnp-2005-Form-16-(02-05-2011).pdf

5540-delnp-2005-form-18.pdf

5540-delnp-2005-Form-2-(02-05-2011).pdf

5540-DELNP-2005-Form-2-(26-12-2008).pdf

5540-delnp-2005-form-2.pdf

5540-DELNP-2005-Form-3-(26-12-2008).pdf

5540-delnp-2005-form-3.pdf

5540-delnp-2005-form-5.pdf

5540-delnp-2005-GPA-(02-05-2011).pdf

5540-DELNP-2005-GPA-(26-12-2008).pdf

5540-delnp-2005-Petition Others-(15-05-2012).pdf


Patent Number 233629
Indian Patent Application Number 5540/DELNP/2005
PG Journal Number 17/2009
Publication Date 24-Apr-2009
Grant Date 31-Mar-2009
Date of Filing 30-Nov-2005
Name of Patentee SEITZ, MICHAEL, WALTER
Applicant Address 7442 TALL PINES DRIVE, HOUSTON, TX 77088, USA.
Inventors:
# Inventor's Name Inventor's Address
1 SEITZ, MICHAEL, WALTER 7442 TALL PINES DRIVE, HOUSTON, TX 77088, USA.
PCT International Classification Number C23C 4/06
PCT International Application Number PCT/US2004/016748
PCT International Filing date 2004-05-27
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 60/476,875 2003-06-06 U.S.A.