U.S. patent number 3,773,549 [Application Number 05/203,364] was granted by the patent office on 1973-11-20 for ceramic coated porous metal structure and process therefor.
This patent grant is currently assigned to Union Carbide Corporation. Invention is credited to Raymond J. Elbert, Ernest G. Farrier.
United States Patent |
3,773,549 |
Elbert , et al. |
November 20, 1973 |
**Please see images for:
( Certificate of Correction ) ** |
CERAMIC COATED POROUS METAL STRUCTURE AND PROCESS THEREFOR
Abstract
A porous metal structure, and process therefor, having a thin
coating of a ceramic material deposited on its surface and on the
internal walls of all accessible pores which substantially improves
the oxidation resistant characteristics of the structure while
effecitvely maintaining its mechanical properties.
Inventors: |
Elbert; Raymond J. (Middleburg
Heights, OH), Farrier; Ernest G. (Parma, OH) |
Assignee: |
Union Carbide Corporation (New
York, NY)
|
Family
ID: |
22753679 |
Appl.
No.: |
05/203,364 |
Filed: |
November 30, 1971 |
Current U.S.
Class: |
428/357; 427/247;
106/38.27; 427/376.4; 427/376.5; 428/433 |
Current CPC
Class: |
C23C
24/00 (20130101); C23F 15/00 (20130101); Y10T
428/29 (20150115) |
Current International
Class: |
C23F
15/00 (20060101); C23C 24/00 (20060101); B44d
001/02 () |
Field of
Search: |
;117/129,99,5.3
;75/2R,2F ;106/38.27 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Whitby; Edward G.
Claims
What is claimed is:
1. A process for coating porous metal structures having a nominal
pore size no greater than 100 microns with an oxidation resistant
ceramic-containing material comprising the steps:
a. preparing a colloidal-like suspension of a finely ground
ceramic-containing material in a liquid suspending vehicle;
b. depositing a layer of the colloidal-like suspension of step (a)
on the surface of the porous metal structure;
c. removing substantially all of the liquid suspending vehicle,
thereby leaving the ceramic-containing material substantially
dispersed on the wall surfaces of the porous structure; and
d. heating the ceramic-containing deposited porous metal structure
to a temperature below the melting point of the metal components of
the porous metal structure but sufficient to cause said
ceramic-containing material to fuse and wet the wall surfaces of
said porous metal structure.
2. The process as in claim 1 wherein the steps (a) through (d) are
repeated at least once.
3. The process as in claim 1 wherein the steps (a) through (c) are
repeated at least once before step (d) is performed.
4. The process as in claim 1 wherein in step (c) said liquid
suspending vehicle is substantially removed at room
temperature.
5. The process as in claim 1 wherein in step (a) said
ceramic-containing material is selected from at least one of the
groups consisting of oxides, carbides, borides, nitrides, and
silicides of aluminum, magnesium, sodium, lithium, beryllium,
cesium, titanium, zirconium, hafnium, tungsten, molybdenum, iron
and cobalt.
6. The process as in claim 1 wherein in step (a) said
ceramic-containing material is selected from at least one of the
groups consisting of silicon dioxide, chromium oxide, titanium
oxide, aluminum oxide, boron oxide, sodium oxide, and potassium
nitrate.
7. The process as in claim 5 wherein in step (a) said
ceramic-containing material has a softening range at a temperature
between about 1600.degree. F and about 2300.degree. F; and wherein
in step (d) said porous metal material is heated to a temperature
between about 1800.degree. F and about 2400.degree. F.
8. The process as in claim 5 wherein in step (a) said finely ground
ceramic-containing material is sized between about 0.01 micron and
about 10 microns.
9. The process as in claim 5 wherein in step (a) said liquid
suspending vehicle is selected from at least one of the groups
consisting of alcohol, an alcohol-containing liquid, methanol,
acetone, heptane, and kerosene.
10. The process as in claim 5 wherein the colloidal suspension of
step (a) has a viscosity of between about 100 centipoises and about
1 centipoise.
11. The process of claim 5 wherein said coated porous metal
structure is intended for abradable seal applications and wherein
in step (d) said layer of ceramic coating material is between about
0.01 micron and about 10 microns.
12. The process in claim 5 wherein said coated porous metal
structure is intended for bearing applications and wherein in step
(d) said ceramic-containing material is between about 1 micron and
about 30 microns thick.
13. A porous metal structure having a nominal pore size no greater
than 100 microns and having an oxidation resistant coating of a
ceramic-containing material, said coating being deposited
substantially on the wall surfaces of the pores in said porous
metal structure thereby providing a barrier which substantially
minimizes the attack of gases on the metal.
14. The porous metal structure of claim 13 intended for abradable
seal applications wherein said oxidation resistant coating is
between about 0.01 micron and about 10 microns thick.
15. The porous metal structure of claim 13 intended for bearing
application wherein said oxidation resistant coating is between
about 1 micron and about 30 microns thick.
Description
FIELD OF THE INVENTION
This invention relates to ceramic coated porous metal structures
admirably suited for use in oxidation environments as abradable
seals, bearings or bearing retainers, and filters.
DESCRIPTION OF PRIOR ART
There are many methods presently being utilized for forming porous
bodies using powdered metallurgic techniques. Generally, powder
metallurgical processes involve the steps of shaping metal powder
into green compacts by such techniques as loose packing,
compaction, extrusion, rolling or the like, and then consolidating
the green composite so formed by the mechanism of sintering. Many
of these processes are described in "Treatise on Powder Metallurgy"
by C. G. Goetzel, Interscience Publishers, Inc., New York, N.Y.
(1949), and "Fundamental Principles of Powder Metallurgy" by W. D.
Jones, Edward Arnold Publishers, London, England (1960). Further
methods for fabricating porous metal sheets and the like are
disclosed in U.S. Pat. No. 3,433,532, in copending U.S. application
Ser. No. 798,142 by R. J. Elbert filed Feb. 10, 1969 now U.S. Pat.
No. 3,577,226, in copending U.S. application Ser. No. 164,516 by R.
J. Elbert filed July 21, 1971, and in copending U.S. application
Ser. No. 128,182 by R. J. Elbert, et al., filed Mar. 25, 1971.
Porous metal structures, such as porous sheets, are admirably
suited for use in such applications as filters, abradable seals,
sound suppression structures, bearings and bearing retainers,
energy absorbing material and the like. One disadvantage of porous
structures, however, is that the metal component of the structure,
while being relatively oxidation resistant when present in the bulk
state in the temperature range of up to 1000.degree.C, is subject
to oxidation when fabricated into a porous state because of its
fine structure and extensive surface area. Thus, porous metal
structures are somewhat limited in their applications to uses
wherein they will not be exposed to high temperature oxidizing
environments. Abradable seals and bearing materials which are
designed for aerospace applications or the like are intended to be
subjected to oxidation environments thus curtailing their useful
and functional life. This limited life usage for porous metal
structures intended for use in oxidation environments necessitates
the additional expenditure of time and money for replacing such
structures after a relatively short period of operational time and
consequently weakens the reception accorded these structures in the
aerospace or like industry. To compensate for this limited life
usage, it has been recommended that oxidation coatings, such as
metal oxides, be applied to the porous structures. However, if the
commercially available oxidation coatings deposited by known
techniques are employed on these porous metal structures, the
abradability of such structures will be seriously affected when
they are intended for use in abradable seal applications, and
likewise, the lubricant filling characteristics of bearings, and
bearing retainers will also be affected.
One of the primary objectives of this invention is to provide an
oxidation resistant coating for porous metal structures composed of
a ceramic-containing material which will not adversely affect the
abradability of porous metal structures when intended for abradable
seal applications and will extend the maximum oxidation protection
temperature of porous structures intended for bearing
applications.
SUMMARY OF THE INVENTION
Broadly stated, the invention relates to an oxidation resistant
ceramic-containing coating for porous metal structures that will
not substantially affect the abradability of such structures when
intended for abradable seal application usage, nor substantially
affect the characteristics required of porous structures intended
for bearing application or filter usage.
Basically, the process for applying an oxidation resistant ceramic
coating on a porous metal structure would initially entail
preparing a colloidal-like suspension of a finely ground
ceramic-containing material in a liquid suspending vehicle. The
colloidal-like suspension can then be deposited on a porous metal
structure to be coated, after which the coated structure is dried
to substantially remove the liquid suspending vehicle thereby
leaving a dispersed deposition of the ceramic-containing material
on the walls of the accessible pores throughout the structure.
Thereafter, the ceramic-containing material dispersed on the porous
metal structure is heated to a temperature below the melting point
of the metal components of the porous metal structure, but
sufficient to cause the ceramic-containing material to fuse and wet
the wall surfaces of the pores in the structure. Thus, the porous
metal structure will have a ceramic coating which will act as a
barrier so as to minimize attack of foreign gases, such as oxygen,
on the metal.
The above process of depositing and drying the colloidal-like
suspension on the porous metal structure can be repeated so as to
obtain a desired degree of coating or to increase the coating
thickness. A ceramic-containing coating on porous structures
usually between about 0.01 micron and about 10 microns thick and
preferably between about 0.01 micron and about 5 microns thick
would be admirably suited for abradable seal applications. For
bearings and bearing retainer applications, a ceramic-containing
coating on porous structures between about 1 micron and about 30
microns would be suitable. The exact coating thickness on a porous
metal structure for a particular application can be determined by
any artisan, familiar with porous materials, using the process of
this invention.
Colloidal-like suspension is intended to mean a suspension of
finely ground particles wherein said particles are substantially
uniformly dispersed throughout the suspending liquid and are sized
to less than 10 micron particle size.
A porous metal structure having a nominal pore size of 100 microns
or less can be fabricated by known techniques using any metal or
metal alloy that is available in powdered, flaked, or fibrous form
and that can be sintered with substantially uniformly controlled
pore sizes ranging anywhere from submicronic to 100 microns and
higher. Examples of alloy compositions suitable for porous metal
abradable seals include such alloys as Hastelloy X, Haynes 25,
Haynes 188, DH 242, Type 347 Stainless Steel, Type 430 Stainless
Steel, Waspalloy, NiCrBl alloys, FeCrAl Y alloys, and the like.
A ceramic-containing material is intended to include such materials
as ceramics, ceramals, cermets, metamics, glass and glass ceramics,
in any and all proportions and combinations. Ceramics are basically
a class of inorganic, nonmetallic substances as opposed to organic
or metallic substances. All ceramic materials will not be suitable
as coatings for porous metal structures but only those which have a
melting point below that of the particular metal or metal alloy
used in the fabrication of the porous metal structures and which
adhere to the surface during thermal cycling. Thus, once the metal
or metal alloy component of a porous metal structure is determined,
a suitable ceramic-containing material can be selected as the
coating material. For example, when at least one base component of
a porous metal structure is selected from the group consisting of
nickel, chromium, cobalt, and iron, a suitable ceramic-containing
material could be selected from at least one material selected from
the group consisting of silicon dioxide, chromium oxide, titanium
oxide, aluminum oxide, boron oxide, sodium oxide, and potassium
nitrate. Depending on the particular component selected for the
porous metal structure, various other ceramic groups can be used
such as the oxides, carbides, borides, nitrides, and silicides of
such materials as aluminum, magnesium, sodium, lithium, beryllium,
cesium, titanium, zirconium, hafnium, tungsten, molybdenum, iron,
cobalt, and the like.
A preferred method of coating porous metal structures is to first
pulverize the ceramic-containing material and then suspend it in a
liquid suspending vehicle to form a colloidal-like suspension. The
liquid suspending vehicle with the substantially dispersed
ceramic-containing material can then be deposited on the surface of
a porous structure by any conventional technique such as painting,
spraying, rolling, or dipping the structure into the colloidal-like
suspension. The technique for depositing the colloidal-like
suspension on and in the porous structure should be adequate so
that a layer of the solution is applied to the surface of the
porous structure including the internal walls of accessible pores.
The coated porous metal structure can be slightly heated, or dried
at room temperature, so as to substantially remove the liquid
suspending vehicle from the ceramic-containing material so that the
latter will be left adhering to the surface of the porous
structure. Thereafter, the structure is subjected to a heated
environment at a temperature sufficient to cause the
ceramic-containing material to assume a molten state whereupon it
will fuse and wet the surface of the porous structure providing the
substantially uniform layer thereon. Thus, in the operational mode
of the coated porous metal structure, the walls of the internal
pores will be substantially protected against the penetration of
foreign gases, such as oxygen.
In order to achieve a ceramic-containing coating which can be
deposited as a thin layer on a porous metal structure, it is
necessary to initially pulverize the ceramic-containing material to
a size smaller than about 10 microns and preferably less than about
1 micron. It is to be understood that the exact size of the
pulverized ceramic-containing material is somewhat dependent on the
pore size of the porous metal structure to be coated. Thus, when
coating a porous metal structure having a nominal pore size of
about 100 microns, it will be desirable to pulverize the
ceramic-containing material to less than about 10 microns, while
coating a porous metal structure with a nominal pore size of 10
microns will preferably require the ceramic-containing material to
be pulverized to less than about 1 micron. The purpose for
pulverizing the ceramic-containing material to a fine fraction is
to enable the material to be deposited within the walls of
accessible pores in the porous metal structure without
substantially plugging the pores.
The liquid suspending vehicle can be any liquid capable of
suspending the selected pulverized ceramic-containing material in a
substantially uniformly dispersed manner and which is capable of
wetting the metal or metal alloy of the porous structure. The
liquid suspending vehicle is added in a sufficient amount to form a
slurry with the pulverized ceramic-containing material so that when
the colloidal-like suspension is deposited on and in the porous
metal structures, it will be substantially removed from the porous
metal structure thereby leaving the pulverized ceramic-containing
material dispersed on the wall surfaces of the accessible pores in
the porous metal structure. It is recommended that the viscosity of
the colloidal-like suspension be about 100 centipoises or less and
preferably about 10 centipoises. Suitable liquid suspending
vehicles are alcohol, alcohol containing liquids, methanol,
acetone, heptane, and kerosene.
A preferred embodiment of this invention would be to select a
ceramic-containing material which has a softening range rather than
a melting temperature, such softening temperature range being the
preferred operating temperature of the coated porous metal
structure. Thus, glass type ceramics are admirably suited for use
in this invention and preferably those materials having a soft or
molten state at temperatures between about 1600.degree.F and
2300.degree.F. Once the ceramic-containing material having good
oxidation resistant properties is selected, it is finely pulverized
and suspended in a slurry or colloidal-like suspension which will
wet and fill the pores of the porous structure. For example,
ceramic-containing materials can be pulverized to a submicron
particle size in a liquid suspending vehicle using nickel base
alloy balls in a nickel based alloy container so as to minimize
contamination. The mixture can be ball milled for a time sufficient
to cause the resulting mixture to approach a colloidal suspension,
that being evidenced by no visible separation of the
ceramic-containing material in the liquid. The colloidal-like
suspension can then be diluted with a liquid suspending vehicle,
preferably the same used in the mill operation, to obtain a
viscosity of between about 100 centipoises and about 1 centipoise
and preferably about 10 centipoises. The viscosity of the
colloidal-like suspension can be varied depending on the porous
metal structure to be coated.
After depositing the coating material, the colloid coated porous
structure is then exposed to ambient so as to evaporate
substantially all of the liquid suspending vehicle thereby leaving
the ceramic-containing material substantially uniformly disposed on
the wall surface of the pores in the structure. The
ceramic-containing coated porous structure is then heated to the
molten state temperature of the ceramic-containing material
whereupon the ceramic-containing material substantially fuses and
wets the wall surfaces of the accessible pores in the porous
structure thus forming a thin protective coating on and within the
structure. Ceramic-containing materials having a softening range
between about 1600.degree.F and 2300.degree.F should be heated to
between about 1800.degree.F and 2400.degree.F. As stated above,
this temperature should be below the melting temperature of the
metal components in the porous metal structure. The coated porous
structure is thereafter cooled and ready for its intended
application.
When the porous metal structures are intended for abradable seal
applications, a ceramic-containing material having good oxidation
resistant properties at between about 1200.degree.F and about
2000.degree.F and being soft or molten at temperatures between
1600.degree.F and 2000.degree.F is ideally suited. It is to be
understood that the ceramic-containing material selected has to be
compatible with the metal components of the porous metal structure
so that detrimental reactions do not occur. Ceramic mixtures
containing SiO.sub.2, Cr.sub.2 O.sub.3, Al.sub.2 O.sub.3, and
TiO.sub.2 are admirably suited for this purpose.
For applying a thick oxidation preventive coating to a porous metal
structure, the above process can be repeated so in effect we have a
multiple layer build-up which upon being heated in the final stage
will form a substantially homogeneous coating.
The following examples will serve to illustrate the concept of this
invention and are not intended to restrict the invention in any
way.
EXAMPLE 1
A porous metal abradable seal, commercially available as Type AB-1,
measuring 2 inches by 6 inches and being 0.06 inch thick on an
Inconel 600 backing sheet (0.06 inch thick) was obtained from Union
Carbide Corporation. This commercial abradable seal, fabricated by
a diffusion-sintered bonding of Ni alloy (nominal 80% Ni-20% Cr) as
disclosed in U. S. copending application Ser. No. 128,182, had a
void fraction of 0.65 nominal, a bulk density of 3 grams per cubic
centimeter, a tensile strength of 500 pounds per square inch
nominal, and a hardness of 91 nominal based on a Rockwell B scale
of 3/4 inch diameter ball at a 15 kilogram load.
The abradable seal material was coated with a ceramic mix (cermet)
of the following composition:
100 grams of frit (commercially available as No. 6210 from the
Ferro Composition, Cleveland, Ohio).
40 grams of technical grade titanium dioxide
6 grams of green label clay
5 grams of chromium oxide
1/2 gram of potassium nitrate
Prior to coating the porous metal abradable seal, the dry powders
of the ceramic mix were loaded into a one quart Inconel 600 ball
mill jar containing 8 pounds (1/2 full) of nickel base alloy balls
(Type RA 103) along with sufficient liquid methanol to cover the
balls. This mixture was ball milled for three weeks to produce a
near colloidal suspension of the ground and blended powder with the
methanol. The colloidal-like suspension was thereafter separated
from the nickel alloy based balls, and then adjusted to 700 grams
(21.5 percent solids) to provide a stock solution. The viscosity of
this solution was 9 centipoises. The solution was then diluted with
additional methanol to 8 percent solids.
The abradable seal material was then impregnated with the solution
which was applied by a roller technique. The coated abradable seal
material was allowed to dry at room temperature for about 8 hours
after which it was furnaced in a continuous belt furnace at
1150.degree.C for a period of 30 minutes in a hydrogen atmosphere.
The coating material which was applied to the abradable seal
material amounted to 0.8 percent of the weight of the coated
material.
The coated abradable seal material was then subjected to an
oxidation environment within a furnace at a temperature of
1600.degree.F. The percent weight gained after various exposure
times is indicated as Curve 1' on the graph of the drawing. A
similar abradable seal material, except lacking the coating of this
invention, was also subjected to the same oxidation environment and
showed a substantial weight increase over that of the coated
abradable seal for similar time periods. Curve 1 on the graph
represents the uncoated abradable seal material. A comparison of
Curves 1 and 1' demonstratively reveals the increase in the
oxidation resistant characteristics of a porous metal structure
coated in accordance with this invention.
The coated and uncoated abradable seal materials specified above
were subjected to an abradability test utilizing a tester composed
of a 71/8 inch diameter rotating knife edge having a peripheral
speed of 100 revolutions per second and designed to plunge at a
depth of 0.001 inch per second until a scar of a 0.030 inch depth
was imparted in the material being tested. The horsepower required
to produce this 0.030 inch scar in both the coated and uncoated
materials was compared and found to be essentially the same, that
being about 0.1 of a horsepower. This abradability test was
conducted on the materials both before and after the materials were
subjected to the oxidation environment. Thus, the ceramic oxidation
coating on the abradable seal material produced no detrimental
effects to the abradability characteristics of the material.
EXAMPLE 2
Abradable seal material similar to that as in Example 1 except that
it had a hardness of 85 nominal as measured by a Rockwell B scale
with a 3/4 inch diameter ball under a 15 kilogram load. This
material was also fabricated as disclosed in U. S. copending
application Serial No. 128,182 and was commercially obtained from
Union Carbide Corporation as Type AB-2 abradable seal material. The
abradable seal material measured 2 inches by 6 inches and was 0.06
inch thick on an Inconel 600 backing sheet (0.06 inch thick).
A ceramic mix identical to that specified in Example 1 was applied
to the abradable seal material as also disclosed in Example 1. The
coated abradable seal material was then allowed to dry at room
temperature for about 8 hours after which it was subjected to a
hydrogen atmosphere in a heated environment of a continuous belt
furnace at a temperature of 1170.degree. C for a period of 30
minutes. The coating material which was added to the abradable seal
material amounted to 0.8 percent of the weight of the coated
material.
The coated abradable seal material was then subjected to an
oxidation environment within a furnace at a temperature of
1600.degree.F. The percent weight gained after various exposure
times is indicated as Curve 11' on the graph of the drawing. A
similar abradable seal material, except lacking the coating of this
invention, was also subjected to the same oxidation environment and
showed a substantial weight increase over that of the coated
abradable seal for similar time periods. Curve 11 on the graph of
the drawing represents the uncoated abradable seal material. A
comparison of Curves 11 and 11' demonstratively reveals the
increase in the oxidation resistant characteristics of a porous
metal structure coated in accordance with this invention.
The coated and uncoated abradable seal materials specified above
were subjected to an abradability test utilizing a tester composed
of a 71/8 inch diameter rotating knife edge having a peripheral
speed of 100 revolutions per second and designed to plunge at a
depth of 0.001 inch per second until a scar of a 0.030 inch depth
was imparted in the material being tested. The horsepower required
to produce this 0.030 inch scar in both the coated and uncoated
materials was compared and found to be essentially the same, that
being below 0.1 of a horsepower. This abradability test was
conducted on the materials both before and after the materials were
subjected to the oxidation environment. Thus, the ceramic oxidation
coating on the abradable seal material produced no detrimental
effects to the abradability characteristics of the material.
The oxidation resistant coating of this invention is also admirably
suited for use on porous metal structures having a bimodal pore
distribution, that is, a porous structure having two nominal pore
sizes. The colloidal-like suspension of ceramic-containing material
could be deposited on the structure in a state that would permit
the smaller pores to be filled with the coating by capillary
action. After drying, the bimodal porous structure would be heated
so that the ceramic-containing material would substantially fuse
and wet the walls of the larger pores while substantially filling
the cavities of the smaller pores. This would provide the porous
structure with a good oxidation resistant coating while not
substantially affecting the mechanical properties of the
structure.
* * * * *