study of functional coating preparation on ceramic materials
TRANSCRIPT
STUDY OF FUNCTIONAL COATING PREPARATION
ON CERAMIC MATERIALS
E. I. Suzdal’tsev,1 D. V. Kharitonov,1 and A. A. Anashkina1
Translated from Novye Ogneupory, No. 10, pp. 38 – 47, October 2011.
Original article submitted August 8, 2011.
Results are presented for a study of functional coating application, for example with increased blackness coef-
ficient, on ceramic and glass ceramic materials. Various methods for coating application used currently are
considered. A coating is proposed based on methyl phenyl spirocyloxane polymer (product MFSS-8).
Keywords: quartz ceramic, glass ceramic, coating, blackness coefficient, modified material surface, product
MFSS-8.
In the construction of objects experiencing the action of
high-temperature gas streams there has been extensive use of
composite, ceramic, and glass ceramic materials. Particular
interest in this case are rocket nose cones, which during oper-
ation experience action of high-temperature (above 1000°C)
and pressure, which cause significant destruction of a struc-
ture, including simultaneous evaporation, sublimation, com-
bustion, and movement of cracked and melted material parti-
cles. In view of this a basic requirement which is laid down
for the materials indicated above is absorption by a compara-
tively small volume of removed mass of a considerable part
of the heat, entering a structure due to aerodynamic heating.
This requirement may be fulfilled with use of materials ex-
hibiting:
– good heat insulation properties, a capacity to localize
heat in a thin surface layer and thereby retain the main
physicotechnical properties of the whole thickness without
change. In this connection favorable material properties are
porosity, property anisotropy, opaqueness for thermal beams;
the most promising materials are based on SiO2, ZrO2, Si3N4,
SiC, etc.;
– the possibility of a change-over from a solid or vis-
cous liquid condition into a gaseous condition, when the
gases formed increase the thickness of a boundary layer and
are capable of shifting the thermal fluxes applied. The best
ablation materials are those with considerable heat of evapo-
ration: graphite, boron nitride, silicon oxide;
– a capacity for formation at a heated surface of a liquid
film with high viscosity, preventing blowing away (removal)
of a liquid phase by a thermal flux; the most promising mate-
rial is silicon oxide, whose viscosity above 2000°C is at the
level of 106 Pa·sec;
– good radiating capacity. Secondary radiation from a
surface leads to a reduction in the overall amount of heat en-
tering a structure. Even a small increase in material radiation
capacity (~0.1) is capable of reducing the rate of mass re-
moval in the entry path of a satellite into the dense atmo-
sphere by about 20% [1, 2].
It should be noted in considering the question of using
ceramic materials in structures for nose cones that quartz ce-
ramic and glass ceramic, having a series of favorable proper-
ties (high mechanical strength, low level of thermophysical
property indices, high heat resistance), exhibit a low degree
of blackness (the blackness coefficient for these material is
within the limits 0.15 – 0.17 un.). In view of this a require-
ment arises for increasing their radiating capacity in order to
increase their stability under the action of high-temperature
gas streams. In this case with quartz ceramic, having open
porosity of 8 – 10%, and additionally with an increase in
blackness coefficient, it is necessary to resolve questions
with respect to material water repellence.
Quartz ceramic has been used in production for quite a
long time (almost from the middle of the last century), and
therefore questions of increasing its operating capacity have
received much attention. One method used for increasing the
blackness coefficient was introduction into original quartz
glass of various alloying additions. In [3 – 10] there is a de-
tailed study of the possibility of alloying quartz glass with
additions of different oxides. The possibility has been dem-
onstrated of a marked change in its physicotechnical proper-
Refractories and Industrial Ceramics Vol. 52, No. 5, January, 2012
340
1083-4877�12�05205-0340 © 2012 Springer Science+Business Media, Inc.
1FGUP ONPP Tekhnologiya, Obninsk, Kaluga Region, Russia.
ties, including radiation capacity. However, as shown in [11],
the radiation intensity is determined not only by the degree
of material blackness, i.e., its transparency, but also surface
temperature. As applied to quartz glass the surface tempera-
ture determines melt viscosity. Here additions introduced,
with a capacity to effectively “darken” the quartz glass,
could not reduce its viscosity, and this is almost impossible
to achieve.
All of the above-mentioned effects, capable of leading to
an increase in the radiating capacity of quartz glass, may ade-
quately be extended to quartz ceramic. In [1] it is proposed to
introduce chromium oxide into a quartz glass slip. On intro-
ducing up to 2% Cr2O3 into a slip the rheological behavior of
the suspension and porosity of castings remains at the previ-
ous level. A subsequent increase in them due to bonding of
Cr2O3 particles with free water causes an increase in viscos-
ity, and therefore starting with an addition in an amount of
3% water was added at the rate of 20% of the weight of an
addition, and with 5% addition it was 50% water. A conse-
quence of introducing an additional amount of water is a re-
duction in slip solid phase consistency, increasing casting po-
rosity and reducing strength.
Based on results of work for increasing the radiating ca-
pacity of quartz glass, similar work was carried out for in-
creasing the blackness coefficient of glass ceramic. In [12]
modification of glass ceramic with addition of Cr2O3 is pro-
posed. The addition is made directly to a slip before molding
billets. Thereby there is a reduction in temperature and soak-
ing time [5]. In addition, as studies have shown, addition of
Cr2O3 does not effect the dielectric properties of glass ce-
ramic and increase the blackness coefficient. However, intro-
duction of an addition in an amount mote than 0.7 wt.%, the
same as in the case of quartz ceramic, has a marked effect on
the original porosity, significantly increasing it. In view of
this in order to resolve the problem of increasing blackness
coefficient for glass ceramic billets before firing it was pro-
posed to apply Cr2O3 to the surface of a molded billet with a
concentration of it in water from 40 to 60 wt.% [13]. This
method appears to be quite effective for reducing the firing
temperature (by about 100°C), although its use for increasing
the blackness coefficient for finished objects is problematic
due to lack of adhesion of Cr2O3 to shell material.
In view of this it is interesting to carry out work for mod-
ifying the surface of ceramic and glass ceramic objects.
Surface modification is a change in surface properties
and material surface zone with the aim of improving a broad
range of functional properties and material and object char-
acteristics (physical, chemical, optical, electrical, electronic,
magnetic, etc.) [14]. Available methods for surface differen-
tiation may be separated into two main groups: a change in
the surface layer and coating application.
In the first group there are also methods such as anodic
oxidation, diffusion impregnation, ion nitriding, ion implan-
tation, and ion atomization. This field of surface modifica-
tion is used during ion-volumetric strengthening of lithium
aluminosilicate glass ceramic in sodium nitrate salt [14, 16].
In view of existing limitations for the choice of materi-
als, suitable for use in technology of changing a surface, of
greatest interest are methods for coating application, i.e., ar-
tificially formed at the surface of an object, or a structure of
layers differing from the base material with respect to com-
position and physicochemical properties.
With respect to the position at a surface of a coating they
are separated into stratified, i.e., formed at the outer surface
of an object or structure having a sharp interface with the
base, and diffusion (or substitution), i.e., coatings formed
due to introduction into a material base without a marked
change in the initial object dimensions.
With respect to purpose coatings are divided into protec-
tive, production, and structural. Protective coatings provide
more prolonged component operation under working condi-
tions, production coatings protect the surface of an object
during production processing; by means of a structural coat-
ing the size and shape of an article is restored, the properties
are provided for its surface, and these coatings may fulfil the
role of structural materials. From most interest from the point
of view of use for coating application on ceramic materials
are the following methods: CVD. PVD, gasothermal deposi-
tion, application of paint and varnish materials.
CVD-coating (chemical vapor deposition) is a chemical
coating applied by a vapor [17]. The coating application pro-
cess is carried out by supply of gaseous reagent in a treat-
ment chamber, where it is in contact with the surface of a bil-
let. The CVD method has almost no limitations with respect
to coating chemical composition. All particles present may
be deposited at a material surface. What coatings form de-
pends on a combination of material and process parameters.
If the process proceeds with filling of space with a reaction
gas (oxygen, nitrogen, or hydrocarbon), then there is forma-
tion of oxide, nitride, and carbide coatings. There is chemical
reaction between atoms of deposited metals and molecules of
reaction gas. The composition of a coating depends on the
partial pressure oft eh reaction gas and coating deposition
rate.
For occurrence of required chemical reactions a tempera-
ture is necessary up to 1100°C. This condition markedly lim-
its the number of materials to which it is possible to apply
coatings by the CVD method. Due to the high deposition
temperature, providing partial diffusion of coating material
into a material base, CVD coatings have the best adhesion to
the base material.
In addition, in order to obtain uniform coating properties
it is necessary to provide optimum gas flow throughout the
whole volume of a device. A special system is used in this
case for gas supply, a so-called shower, and in order to pre-
vent dangerous gas discharges into the atmosphere the device
is fitted with a filter system.
A PVD coating (physical vapor deposition) is deposited
by condensation from a gas phase or as it is still called, the
method of physical deposition [14, 17]. The coating material
is converted into a gas phase from a solid state as a result of
evaporation under the action of thermal energy or as a result
Study of Functional Coating Preparation on Ceramic Materials 341
of atomizing due to kinetic energy of material particle colli-
sion. Energy, and the distribution of density of a particle
stream, are determined by application and process parame-
ters, and the shape of a particle source. The process occurs in
three stages: creation of vapor phase particles, transfer of
particles to a surface, and growth of a film at a surface.
Coating by the PVD method is performed at low temper-
ature (up to 450°C), which does not lead to significant limita-
tions with respect to material, to which a coating is applied.
All of the processes occur in a vacuum or in a working gas
atmosphere at quite low pressure (about 10–2 mbar), which is
necessary in order to facilitate transfer of particle from a
source (target) to an object (substrate) with the minimum
amount of collisions with gas atoms or molecules. This con-
dition also determines the necessity of direct particle flow.
As a result of this a coating is only applied to that part of an
object that is aimed at the particle source. The deposition rate
(rate of coating application) depends in this case on the rela-
tive position of source material. For uniform coating applica-
tion it is necessary to move the material systematically or use
some specific way of positioning sources. At the same time a
coating is only applied at the surface “in direct view of a
source”, leaving an adjacent region of a surface without a
coating. This is absolutely impossible with use of a chemical
deposition method [17].
Coating quality, applied by physical deposition, is deter-
mined by the basic purity of the starting materials, required
level of vacuum, and reaction gas purity.
Gasothermal deposition (thermal spraying) is a process
of heating, dispersal, and transfer of condensed particles of
atomized material by a gas or plasma stream in order to from
at a substrate a layer of a specific material [18]. Under the
general term “gasothermal deposition” (GTD) the following
deposition methods are combined: gas flame, high-velocity
gas flame, detonation, plasma, deposition with facing, elec-
tric metallization, and activated electric arc metallization.
The essence of gasothermal deposition involves fusion of
coating material (wire or powder) followed by application
(deposition) of it on a base in a gas stream. In the microzone
of particle impact of a melt over a coated surface they de-
form and spread, subsequently adhering to each other; by so-
lidifying, the material forms a flat coating layer. The bond of
deposited particles with a base occurs due to thermal and ki-
netic energy, which are determined by the temperature and
movement velocity of the particles. A bond of coating with a
base is adhesive. It is accomplished due to intermolecular
forces and mechanical adhesion of a coating with roughness
of a developed surface. The same as in the PVD method,
coatings are only applied to that part of an object that is
aimed towards the particle source.
In spite of the fact that by all of the methods in question
it is possible to apply different forms of coating on objects
and structures made of ceramics and glass ceramic materials,
they are not free from a marked disadvantage, i.e., the com-
plexity and expense of industrial equipment. This situation is
complicated by the fact that production of ceramic nose
cones is as a rule small scale with existence of a considerable
range of objects, and different standard sizes, which also
complicates the construction of the devices described above.
The simplest and cheapest in use and introduction into coat-
ing application technology on nose cones are paint and var-
nish coatings.
Paint and varnish materials (PVM) are multicomponent
compositions (liquid, paste, or powder), which on applica-
tion by a thin layer to a solid substrate provide formation of a
painted coating with prescribed properties. With respect to
composition and purpose PVM are separated into lacquers,
primers, putties, paints (including enamel). The main re-
quirements for a protective coating are high adhesion to a
substrate, absence of gas and water permeability, mechanical
strength, wear resistance and resistance under operating con-
ditions (atmospheric chemical resistance, etc.).
As film-forming organosilicon enamels lacquers are used
containing different substitutions for the silicon atom, i.e.,
methyl, ethyl, phenyl. It is possible to obtain polyorganosilo-
xanes from elastic to soluble with a different polyorgano-
siloxane structure in relation type and ratio of substitute. The
CH3 group in polyorganosiloxanes gives a coating atmo-
sphere resistance and hydrophobicity. With introduction of
C6H5 groups to polyorganosiloxane there is an increase in
heat resistance and hardness [19].
As protective LVM for rocket noses there is currently
widespread use of enamels FP-566 and KO-5189. In spite of
the fact that the blackness coefficient of these materials is
0.80 – 0.90 un., their operating temperatures do not exceed
250 – 450°C, and under the action of high temperature com-
bined with considerable aerodynamic loads, during operation
of objects these coatings are removed from a cone surface.
Monitoring of contemporary LVM has not revealed ma-
terials with a capacity to increase markedly the blackness co-
efficient of objects made of ceramic materials, to retain high
adhesion to a material substrate under conditions of action of
a high temperature, to provide their water repellence, and di-
electric property stability. A search for ways and methods for
obtaining coatings on ceramic and glass ceramic materials
with a set of functional properties remains important.
In choosing a film-forming component for a proposed
coating many years of operating experience with use of
quartz glass was considered, which requires sealing and
moisture repellence, since after firing this material it has
open porosity of 8 – 10%. For example, in [1; 20 – 24, pp.
302 – 307; 25 – 27] versions are presented for strengthening
and moisture repellence for quartz ceramic with different
organosilicon resin compositions. Most widespread is im-
pregnation of quartz ceramic with products TMFT (solution
of titanium organosilicon oligomer of phenolformaldehyde resin
and butyl ester of boric acid in acetaone, TU 6-02-933–79)
and MFSS-8 (solution of polymethyl spirocyloxane in ace-
tone, TU 6-02-1352–87 or TU 2229-001-64570284–2011).
Here strengthening and moisture repellence of ceramic
occurs due to forming within pores and at the surface of im-
pregnated material a thin polymer film, which covers the
342 E. I. Suzdal’tsev et al.
pore channels formed, and which also provides reliable pro-
tection of the ceramic from moisture. As a result of this
moisture repellence process due to surface impregnation
with products TMFT and MFSS-8 they are used extensively
in the production of cones made of glass ceramic [1].
In spite of the fact that both products are well recom-
mended as impregnating solutions for preparing sealed and
moisture repellent quartz ceramic, of greatest interest is
product MFSS-8, and this is due to the fact that during opera-
tion of objects in the range 250 – 700°C as a result of de-
struction TMFT with formation of carbon there is loss of ra-
dio transparency of an object, and at above 700°C the mate-
rial acquires its original values [1]. Destruction of product
TMFT at elevated operating temperature has led to the situa-
tion that impregnation of cones made of quartz ceramic is
only accomplished from the inner side, whose temperature is
markedly lower than that of the outer surface [21, 22].
The product MFSS-8 also burns at above 700°C, al-
though during its destruction there is no substance formed
perceptible for radio transparency, which makes it possible to
MFSS-8 for impregnating the outer surface of shells [23].
Similar impregnation of quartz ceramic by other impregna-
tion substances with product MFSS-8 provides sealing of
material only due to a thin surface film, whereas during poly-
merization there is “cross linking” of the polymer structure
with formation of a spatial siloxane skeleton [1].
In order to evaluate the possibility of using these coat-
ings for ceramic and glass ceramic materials, a mixture of
product MFSS-8 and an oxide, i.e., CoO, Cr2O3, TiO2, was
used. The mixture obtained was applied to specimens of
quartz ceramic and glass ceramic in order to determine the
ultimate strength in static bending �ben, and dielectric proper-
ties: dielectric permittivity � and the dielectric loss angle tg�.
Then polymerization was performed in order to fix the
layer on a specimen. Data for the change in basic material
properties before and after coating application are presented
in Table 1. Data are also given there for water absorption w
of an applied layer.
As seen from the data presented in Table 1, by applying
coatings of CoO and Cr2O3 it is possible to increase consid-
erably (up to 0.85 – 0.90) the blackness coefficient. Use of
TiO2 as a filler material does not lead to such a marked re-
sult, and the blackness coefficient obtained for a coating is
0.33 – 0.34. Here dielectric properties of both quartz ceramic
and glass ceramic in relation to form of coating are un-
changed. The ultimate strength in bending increases by about
10% of the original for glass ceramic and by 30 – 40% for
quartz ceramic.
Then the ceramic and glass ceramic specimens obtained
with coatings applied to them were subjected the action of
the temperature range 500 – 1250°C with soaking at the
maximum temperature for 60 sec. Property indices were de-
termined for specimens treated in this way (Table 2).
Analysis of data presented in Table 2 makes it possible to
conclude that all the coatings proposed are capable of operat-
ing up to 1250°C. Here neither strength nor dielectric proper-
ties of material undergo any marked changes (all of the
amount of deviations are within the limits of procedural er-
ror). Water absorption of the coating layer itself is also un-
changed. However, with visual examination of specimens of
glass ceramic with a coatings based CoO and TiO2 treated
from 900°C and above it is possible to observe breakdown of
coating integrity (swelling and crumbling), particularly for
cobalt oxide (Fig. 1). At the same time, a coating based on
Cr2O3 does not lose its high adhesion properties even with a
heat treatment temperature of 1250°C.
Worsening of adhesive capacity of the test coatings is
connected with the fact that at 900°C there is destruction of
product MFSS-8 and all of the organic phase evaporates.
This is indicated by data in Table 2, in which it may be seen
that there is an insignificant increase in tg� at 900°C. Up to
this temperature MFSS-8 is present within the system and
this unites coating particles into a single system. Above
Study of Functional Coating Preparation on Ceramic Materials 343
TABLE 1. Dependence of the Level of Change in Glass Ceramic OTM 357 and Quartz Ceramic NIASIT Properties and Coating Quality
Material Coating on baseBlackness
coefficient
Specimen properties
original* with coating
tg� � tg� � �ben
, MPa Wcoating
, 10–3 %
OTM 357 Uncoated 0.16 0.011 7.21 — — — —
MFSS-8 + CoO 0.90 0.011 7.08 0.011 7.10 136 4
MFSS-8 + TiO2 0.33 0.011 7.14 0.010 7.12 141 6
MFSS-8 + Cr2O3 0.85 0.012 6.94 115 6.94 140 2
NIASIT Uncoated 0.14 <0.0005 3.40 0.0003 3.41 64 5
MFSS-8 + CoO 0.91 <0.0005 3.41 0.0003 3.40 58 3
MFSS-8 + TiO2 0.34 <0.0005 3.42 0.0010 3.42 67 2
MFSS-8 + Cr2O3 0.84 <0.0005 3.41 0.0003 3.42 60 4
* Ultimate strength in bending for original OTM 357 material specimen is 130 MPa, and for original NIASIT material specimen it is 46 MPa.
900°C, when all of the acetone has evaporated, within the
system only SiO2 remains, being in a nanodispersed condi-
tion within the composition of the product MFSS-8. Due to
the high specific surface of SiO2 nanoparticles a considerable
number of siloxane bonds form with the surface of substrate
material and Cr2O3 particles.
Thus, most promising from the point of view of effective
increase in blackness coefficient (up to 0.85 un.) and high
adhesive capacity, is a coating based on product
MFSS-8 modified with Cr2O3 addition.
However, an attempt to apply a coating with chromium
oxide, showing good adhesion on glass ceramic specimens,
344 E. I. Suzdal’tsev et al.
TABLE 2. Dependence of the Level of Change in Glass Ceramic OTM 357 and Quartz Ceramic NIASIT with Coating Properties on Test Tem-
perature
Material
Specimen treatment
temperature, °C
(60 sec)
Specimen properties
original* with coating
tg� � tg� � �ben
, MPa Wcoating
, 10–3 %
Coating based on MFSS-8 + Cr2O3
OTM 357 500 105 7.05 105 7.02 140 5
700 102 7.14 109 7.08 146 0
900 104 7.09 112 7.13 138 0
1100 108 7.12 114 7.11 136 2
1250 103 7.13 111 7.07 99 2
NIASIT 500 <5 3.40 3 3.41 64 5
700 <5 3.42 9 3.43 57 1
900 <5 3.44 17 3.42 60 7
1100 <5 3.42 4 3.43 75 7
1250 <5 3.40 4 3.41 51 8
Coating based on MFSS-8 + CoO
OTM 357 500 105 6.99 117 6.91 134 7
700 110 7.00 114 6.99 123 7
900 110 7.18 118 7.13 123 11
1100 105 7.05 111 7.14 134 6
1250 104 7.16 109 7.12 100 11
NIASIT 500 <5 3.41 3 3.46 66 1
700 <5 3.43 7 3.41 58 4
900 <5 3.43 16 3.44 60 1
1100 <5 3.44 6 3.42 74 3
1250 <5 3.41 6 3.44 53 4
Coating based on MFSS-8 + TiO2
OTM 357 500 103 7.03 105 7.02 152 2
700 103 7.12 119 7.07 130 2
900 105 7.19 119 7.16 153 1
1100 106 7.21 101 7.15 99 1
1250 103 7.03 109 7.17 99 2
NIASIT 500 <5 3.44 10 3.44 57 1
700 <5 3.42 22 3.39 62 2
900 <5 3.45 19 3.45 48 1
1100 <5 3.42 11 3.45 57 2
1250 <5 3.39 16 3.40 45 5
* Ultimate strength in bending for original OTM 357 material specimen is 136 MPa, and for original NIASIT material specimen it is 60 MPa.
did not give a favorable result on quartz ceramic specimens
(Fig. 2). With an increase in heat treatment temperature there
was separation of all of the test coatings from a quartz ce-
ramic specimen surface. Whereas for coatings based on CoO
and TiO2, this effect was predictable, for a coating based on
Cr2O3, a lack of adhesion was entirely unexpected.
Analysis of the specimens obtained makes it possible to
propose that the reason for crumbling of a coating with
Cr2O3 from the surface of a quartz ceramic specimen is the
quite high porosity of ceramic specimens (8 – 10%). Pres-
ence of porosity in substrate material leads to a situation that
with application at its surface of a mixture of product
MFSS-8 and Cr2O3 there is impregnation of pores with
MFSS-8 material. Here Cr2O3 particles do not penetrate into
pores and remain at the surface. All of this leads to impover-
ishment of the mixture, which in total does not provide for-
mation of a sufficient number of siloxane bonds for joining
with the surface layers of substrate material.
Emerging from this complicated situation it appeared
preferable to impregnate porous substrate material with
MFSS-8 in order to seal its surface. Specimens of quartz ce-
ramic are shown in Fig. 3 with prior impregnation and with-
out it, coated with Cr2O3 and heat treated at 1250°C. It is evi-
dent that introduction of additional impregnation of porous
materials is capable of increasing markedly coating adhesion
to substrate material.
A result of these studies was preparation of a coating
based on product MFSS-8 and Cr2O3 capable of markedly in-
creasing the blackness coefficient for ceramic and glass ce-
ramic materials. Here a coating retains it properties, and also
with short-term action of high temperature. At the same time
operation of objects of ceramic materials for which the coat-
ings are being developed, occurs under the action of severe
climatic conditions: alternating temperature, increased mois-
ture content, rain, dust, etc. Therefore it is desirable to pro-
duce verification of retention of property stability for the
proposed coatings under these conditions, and also the stabil-
ity of a coating based on MFSS-8 and Cr2O3 compared with
materials used currently: enamels FP-566, KO-5189,
ÉP-140, and products MFSS-8 and TMFT, used for water
repellence of quartz ceramic. For complete information
about the protective properties of these products studies were
carried out for resistance to action of cyclic thermal loads
and prolonged action of sea water.
In order to determine the resistance of different coating
versions thermal cycling of specimens was performed at
temperatures from -60 to +300°C (50 cycles). After 25 cy-
cles specimens were selected for determination of water ab-
sorption, �, and tg�. Then specimens were returned for fur-
Study of Functional Coating Preparation on Ceramic Materials 345
Fig. 1. Specimens of glass ceramic OTM 357 with different coatings after heat treatment at 500 and 1250°C with soaking for 60 sec.
ther testing. The results of measurements are presented in Ta-
ble 3.
Practically all of the coatings applied to quartz ceramic,
did not withstand cyclic temperature drops, and after 25 cy-
cles there is a marked increase in water absorption, and cor-
respondingly the dielectric loss angle. Only a coating based
on MFSS-8 with Cr2O3 filler behaved well. It is interesting
that a coating of pure MFSS-8 was subject to surface failure
after 50 thermal cycles. A specimen is presented in Fig. 4 of
quartz ceramic impregnated with product MFSS-8 after ther-
mal cycling. In contrast to specimens with a coating of
346 E. I. Suzdal’tsev et al.
TABLE 3. Dependence of Change in Coated Quartz and Glass Ceramic Properties on Thermal Cycling*
Coating
Original uncoated specimen parameters
Coated specimen parameters after thermal cycling, cycles
with coating 25 50
�, g/cm3 W, % � tg�, 104� tg�, 104 W, % � tg�, 104 W, % � tg�, 104 W, %
NIASIT quartz ceramic
MFSS-8 1.972 5.372 3.43 <5 3.40 12 0.005 3.40 11 0.062 3.59 308 0.175
TMFT 1.959 5.777 3.39 <5 3.39 10 0.007 3.37 16 0.048 3.57 437 0.250
FP-566 1.974 5.380 3.39 <5 3.39 7 0.008 3.39 12 0.012 3.24 201 0.083
KO-5189 1.984 5.054 3.42 <5 3.48 10 0.000 3.48 10 0.019 3.47 95 0.208
MFSS-8 + Cr2O3 1.976 5.219 3.42 <5 3.40 10 0.003 3.44 9 0.008 3.42 9 0.007
OTM 357 glass ceramic
MFSS-8 + Cr2O3 2.50 0.003 7.02 110 7.02 115 0.002 7.03 109 0.003 7.02 116 0.005
* Cycle from –60 to +300°C, soaking at final temperature for 60 min.
Fig. 2. Specimens of quartz ceramic with different coatings after heat treatment at 500 and 1250°C with soaking for 60 sec.
MFSS-8 and Cr2O3, which has a form similar to that pre-
sented in Fig. 3b, all of the specimens surface impregnated
only with MFSS-8 is a fine network of cracked structure.
Proceeding from the fact that MFSS-8 destruction occurred
at 700 – 900°C, it may be suggested that the action of low
temperature led to this unfavorable effect. In the case of test-
ing specimens impregnated with chromium oxide, apparently
a favorable result is connected with formation of a stronger
coating carcase.
Another batch of specimens was subjected for verifica-
tion of coating stability to the action of sea water. Specimens
impregnated with product MFSS-8 and TMFT, and also
painted with enamels FP-566 and KO-5169, were placed in
saline water. The change in dielectric properties and water
absorption under the action of sea water are presented in Ta-
ble 4. After 150 h for specimens in sea water there is a sharp
increase in tg� for specimens coated with enamels FP-566
and KO-5169, and also impregnated with TMFT solution. A
further increase in exposure to 550 h only aggravates this
change. Thus, only specimens of glass ceramic and quartz
ceramic with coatings of MFSS-8 and a composite based on
product MFSS-8 modified with chromium oxide withstood
testing.
Thus, as a result of these studies a new functional coating
has been prepared having as a film-forming component prod-
uct MFSS-8 and chromium oxide as a filler. The coating ob-
Study of Functional Coating Preparation on Ceramic Materials 347
Fig. 3. Specimens of quartz ceramic coated with
MFSS-8 + Cr2O3 heat treated at 1250°C for 60 sec: a)
substrate material without prior impregnation; b ) pre-
vious impregnation of substrate with product MFSS-8.
Fig. 4. Quartz ceramic specimen impregnated with MFSS-8 prod-
uct after 50 thermal cycles –60 to +300°C.
TABLE 4. Dependence of Change in Coated Quartz Ceramic NIASIT and Glass Ceramic OTM 357 Properties on Prolonged Exposure in Sea
Water
Coating
Original uncoated specimen parameters
Coated specimen parameters after exposure, h
coated 150 550
�, g/cm3 W, % � tg�, 104� tg�, 104 W, % � tg�, 104 W, % � tg�, 104 W, %
NIASIT quartz ceramic
MFSS-8 1.975 5.380 3.43 <5 3.40 7 0.004 3.43 8 0.004 3.44 10 0.005
TMFT 1.962 5.657 3.43 <5 3.43 6 0.005 3.46 78 0.170 3.46 121 0.370
FP-566 1.970 5.480 3.44 <5 3.43 5 0.009 3.71 613 0.750 No signal 3.020
KO-5189 1.981 5.244 3.42 <5 3.42 9 0.016 3.47 97 0.120 3.52 283 0.350
MFSS-8 + Cr2O3 1.980 5.283 3.43 <5 3.43 8 0.004 3.44 9 0.006 3.43 9 0.007
OTM 357 glass ceramic
MFSS-8 + Cr2O3 2.50 0.003 7.02 115 7.02 118 0.004 7.03 116 0.004 7.03 121 0.005
tained is capable of increasing markedly ceramic and glass
ceramic material blackness coefficient. A coating exhibits
good adhesion capacity, it may be operated under the action
of temperatures up to 1250°C, withstand thermal cycling in
the range from –60 to +300°C, and also maintain its proper-
ties with prolonged action of sea water.
The results of these studies may be used not only for im-
proving the blackness coefficient of objects made from ce-
ramic and glass ceramic materials, but also in order to re-
solve other important problems, for example a change in ma-
terial dielectric permittivity, an increase in object wall radio
transparency, etc. All of these problems are resolved by
choice of the required component for introduction of product
MFSS-8.
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