U.S. patent number 3,903,341 [Application Number 05/399,774] was granted by the patent office on 1975-09-02 for ceramic honeycomb structure for accommodating compression and tension forces.
This patent grant is currently assigned to Universal Oil Products Company. Invention is credited to Clarence G. Gerhold.
United States Patent |
3,903,341 |
Gerhold |
September 2, 1975 |
Ceramic honeycomb structure for accommodating compression and
tension forces
Abstract
An improved ceramic honeycomb structure is provided by having a
configuration with thin curved walls between the multiplicity of
cells whereby both compression and tension forces can be better
accommodated when the structure is being subjected to non-uniform
temperature conditions. Two or more sets of opposing curved walls
can be used to define each cell of the multiplicity thereof and the
curvature for each set of walls is such as to permit elongative
deformation in one direction without causing a reduced width cell
or a closer spacing for juncture lines between adjacent cells in a
direction transverse to the expansion movement.
Inventors: |
Gerhold; Clarence G. (Palatine,
IL) |
Assignee: |
Universal Oil Products Company
(Des Plaines, IL)
|
Family
ID: |
23580908 |
Appl.
No.: |
05/399,774 |
Filed: |
September 20, 1973 |
Current U.S.
Class: |
428/116; 422/180;
428/118; 422/179; 422/240; 156/89.22 |
Current CPC
Class: |
B01J
35/04 (20130101); B01D 53/9454 (20130101); F01N
3/2828 (20130101); Y10T 428/24149 (20150115); Y02T
10/12 (20130101); F01N 2330/06 (20130101); Y10T
428/24165 (20150115) |
Current International
Class: |
B01D
53/94 (20060101); F01N 3/28 (20060101); B01J
35/00 (20060101); B01J 35/04 (20060101); B32B
003/12 () |
Field of
Search: |
;29/455LM ;161/68,69
;156/89,197 ;23/288F,288FC ;52/615,618 ;181/36C,71 ;252/477R |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Ansher; Harold
Assistant Examiner: Epstein; Henry F.
Attorney, Agent or Firm: Hoatson, Jr.; James R. Liggett;
Philip T. Page, II; William H.
Claims
I claim as my invention:
1. A ceramic composite with a multiplicity of parallel cells in a
honeycomb type of structure which can deform to accommodate
compression and tensile forces from non-uniform temperature
conditions, which comprises, having all interconnecting walls
between juncture lines of the walls and between adjacent cells
being curved and oriented one to another in a reoccurring
symmetrical pattern, each of said parallel cells being formed and
defined by two sets of opposing curved walls, and with one set of
walls generally normal to the other in the overall pattern and at
the junctures, said walls for any one cell being such that one set
of opposing walls will bow towards one another and the other set
will bow away from one another to form a necked-in and dumb-bell
form of cross-sectional configuration, and all cells having a
common wall with an adjacent cell will be of the same configuration
as such cell except that it will be in an orientation of 90.degree.
with respect thereto, whereby expansion movements in directions
transverse to the length of the longitudinal cells that are due to
differential temperature conditions can cause deformation and
straightening of one set of opposing curved walls without causing
juncture lines between cells to tend to move closer together in a
direction generally transverse to the walls being straightened and
to thereby provide a less fragile structure.
2. The ceramic composite structure claim 1 further characterized in
that said structure is provided with an active oxidizing catalyst
coating material suitable to provide for the conversion of a
noxious-gaseous stream.
3. A ceramic composite with a multiplicity of parallel cells in a
honeycomb type of structure which can deform to accommodate
compression and tensile forces from non-uniform temperature
conditions, which comprises, having all interconnecting walls
between juncture lines of the walls and between adjacent cells
being curved and oriented one to another in a reoccurring
symmetrical pattern, each of said parallel cells being formed and
defined by three sets of opposing curved walls, with each set of
walls being at approximately 120.degree. with respect to the next
adjacent set of walls to define any one cell, with next adjacent
walls around an individual cell alternately bowing inwardly and
outwardly, opposing curved partitioning walls between adjacent
cells in any one row thereof are bowed in the same direction, and
each cell in any given row of cells has the same cross-sectional
configuration as the other cells and is in the same orientation,
whereby to readily provide tension and deformation along any one of
three axis without causing any substantial reduced spacing between
juncture lines along either of the other 120.degree. transverse
axes.
4. The ceramic composite structure of claim 3 further characterized
in that said structure is provided with an active oxidizing
catalyst coating material suitable to provide for the conversion of
a noxious gaseous stream.
Description
The present invention relates to an improved design and arrangement
for cells in a ceramic honeycomb structure such that there can be
greater ability to withstand the compression and tension forces
which can result from non-uniform high temperature conditions, as
for example, when a honeycomb section is being utilized as a
support for an oxidizing catalyst coating.
More particularly, there are herewith provided improved forms of
honeycomb structures by virtue of special cell configurations which
have all curved walls between common juncture lines forming the
multiplicity of cells such that tension conditions can be better
accommodated without causing breakage of the monolith walls.
One of the serious problems in connection with the use of ceramic
monoliths or "honeycomb" type of structures as supports for
catalyst coatings results from the fact that a catalyst structure,
or even a bed of catalyst particulates, does not operate at a
uniform temperature throughout its length or across its
cross-section. There are normally substantial temperature
differences between the inlet of the unit and the outlet end
thereof, as well as differences between the central section and the
areas adjacent to the catalyst chamber walls. As a result those
sections of the catalyst unit which are at a higher temperature
will undergo greater expansion than those at the lower temperatures
and there will also be various sections of the monolithic unit
undergoing either tension or compression. Typically, the ceramic
composites forming the conventional forms of monoliths are fairly
strong in compression, at least in comparison to tensile strength,
such that there can readily be cracks and failures in the tensioned
portions of a unit because of excessive stressing.
It is realized that various honeycomb configurations, with respect
to the cross-section of cells, have been made and used for
absorption elements and for catalyst supports in the air pollution
field. Individual cells of a particular honeycomb may be square,
rectangular, triangular, hexagonal, round, oval, etc., as well as
of different sizes and diameters. Typically, where a ceramic
honeycomb is used as a catalyst support member, it will be selected
to have as small cells as possible, without creating excessive
pressure drop for the fume stream, in order to provide a maximum of
catalytic surface area. However, the smaller the cells, the greater
is the rigidity and there is a lowering of flexibility for a given
structure.
While it is a feature of the present invention to provide for
curved interconnecting walls to extend between juncture lines and
to effect the partitioning between adjacent parallel cells in a
monolith, it must be realized that conventional circular or oval
patterns for cells will not provide the desired flexure and
deformation to help overcome tension breaks. Also, the curved wall
cell configurations resulting from node to node contact points with
the use of adjacent corrugated sheet manufacturing procedures, such
as taught in U.S. Pat. No. 3,444,925, do not seem to result in
suitable stress relieving patterns. For example, with a pattern
providing circles, or ovals, in the cross-section of a honeycomb,
there will be tensile forces without the available wall members to
readily give and lengthen. Stated another way, with the use of
curved wall patterns, from circular or oval cells, there will still
be a tendency for juncture lines to move closer together in a
direction transverse to a tension force and there is no real
elimination of breakage problems from non-uniform temperature
conditions.
On the other hand, it may be considered a principal feature of the
present invention to use curved members, rather than straight, to
provide cell walls and connect juncture lines between a plurality
of adjacent cells and, at the same time, have the curved walls form
special patterns which will not tend to cause juncture lines to
move closer together in a direction generally transverse to the
walls being subjected to lengthening and straightening from a
tensile condition.
The improved form of cell configuration can be accomplished, by way
of example, in a design where square cells would have the straight
walls replaced by arcs in which the curvature alternates between
concave inward and convex outward to result in "dumb-bell" shaped
cells. Also, where the walls of what would be a normal hexagonal
pattern are made to be arcuate and they alternate between being
concave inwardly and convex outwardly, then there is a resulting
"clover-leaf" shape for each cell.
In a broad embodiment, the present invention provides a ceramic
composite with a multiplicity of parallel cells in a honeycomb type
of structure which can deform to accommodate compression and
tensile forces from non-uniform temperature conditions, which
comprises, having all interconnecting walls between juncture lines
between adjacent cells being curved and oriented one to another in
a reoccurring symmetrical pattern, with next adjacent walls around
an individual cell alternately bowing inwardly and outwardly, and
there being at least two sets of opposing curved walls to form each
cell of said structure, whereby expansion movements in directions
transverse to the length of the longitudinal cells that are due to
differential temperature conditions can cause deformation and
straightening of one set of opposing curved walls without causing
juncture lines between cells to tend to move closer together in a
direction generally transverse to the walls being straightened and
to thereby provide a less fragile structure.
In a specific embodiment, there may be a configuration which is a
modification of a conventional square pattern in that each cell
will have an opposing set of partitioning walls which are concave
toward one another and then at 90.degree. thereto there will be a
second set of partitioning walls which are curved outwardly, or
convexly away from one another, such that the resulting
configuration for each cell will be of a dumb-bell shape. Also,
where walls alternate between bending inwardly and outwardly, the
resulting overall pattern is such that any one cell will have
adjoining dumb-bell shaped cell configurations that are at right
angles thereto. This arrangement permits tensile stress elongation
in one direction by virtue of wall curvature permitting some
measure of desired elongation without breakage while, at the same
time, there should be substantially no narrowing of spacing with
respect to juncture points between cells in a direction transverse
to the elongation. Actually, there may be some local spreading of
juncture lines due to rotation thereof and to partial straightening
of the transverse walls.
In another embodiment, there may be provided a curved wall
modification for what might normally be considered a hexagonal cell
pattern, with three sets of opposing curved walls rather than three
sets of straight walls as provided in a conventional hexagon.
Opposing curved partitioning walls between adjacent cells in any
one row thereof will be bowed in the same direction and each cell
in any given row of cells will have the same cross-sectional
configuration and orientation. Also in this arrangement, the curved
walls for any one cell will alternate between being concave
inwardly and convex outwardly around the periphery of such cell
such that the result is a cell unit being generally of clover-leaf
shape. With respect to flexibility, this arrangement permits
tensile forces to, in effect, straighten or elongate two sets of
wall portions of a particular cell with little or no movement
between juncture lines in a direction transverse to the tensile
forces, whereby flexibility is in effect built into the honeycomb
structure to accommodate differential temperature conditions. The
deformation and flexibility aspects will be more clearly explained
and set forth in connection with the subsequent description of the
drawings.
The desired special cell configurations in a honeycomb type of
structure may be obtained during the manufacturing process by
extruding the ceramic material through suitably shaped die means;
however, other forms of manufacture may be utilized. For example,
specially shaped modifications of a corrugated type sheet may be
utilized to conform with and form a juncture with other specially
formed sheet members such that the desired clover-leaf pattern
could result in the final product. In other words, the procedure of
manufacturing honeycomb type of monolithic structures such as set
forth in U.S. Pat. Nos. 3,444,925 and 3,505,030 might well be
utilized in the present instance. Also, sheet-like members of
ceramic material in a curved or corrugated form may be slotted and
subsequently nested in the manner of making an egg-crate type of
carton to form the modified, curved wall square, configuration
where the result is the multiplicity of dumb-cell shaped cells.
Where sheets of corrugated films of green ceramic are nested with,
or made to contact adjacent sheets or panels, then during the
curing or firing stage there is a fusing and sintering of the
contacting sheets to form the desired shapes and juncture points
between longitudinal cells, such as is set forth and described in
the aforementioned patents.
In still another procedure, there can be the formation of a ceramic
mixture around suitably shaped burnable core members and a firing
and burning away of the core material from the ceramic material to
result in desired shaped cells for the honeycomb element. In other
words, it is not intended to limit the present invention to any one
method of making the honeycomb ceramic structure, nor is it
intended to limit the invention to any one type of material that
will form the resulting rigid cellular structure. For example, the
ceramic may comprise refractory crystalline materials such as
sillimanite, magnesium silicates, zircon, petalite, spodumene,
cordierite, alumino-silicates, mullite, etc. Such materials are of
advantage in having relatively high porosity over their surface
areas and being suitable for supporting catalyst coatings to, in
turn, provide catalytically active conversion elements.
The present honeycomb elements may be utilized to advantage,
without catalyst coatings, as absorption structures or heat
exchange elements; however, such types of coated structures are
finding wide usage in catalytic converters adapted to have auto
exhaust fumes passed therethrough to effect conversion and
elimination of undesired components such as carbon monoxide,
hydrocarbons and nitrogen oxides. While it is not intended to limit
the present invention to any one specific type of active catalyst
coating, such coating may comprise an oxidation catalyst and may
include the metals of Groups I, V, VI and VIII of the Periodic
Table, particularly copper, silver, vanadium, chromium, iron,
cobalt, nickel, platinum, palladium, with a component being used
singly or in combination with one or more other active component.
Also, typically, the ceramic honeycomb material will have been
coated with a suitable refractory inorganic oxide such as alumina
or alumina combined with one or more other refractory inorganic
oxide. Typically, the oxide supporting layer will be applied to the
wall surface prior to the coating of the active catalytic component
although there may be a mixture of refractory metal oxide support
material with the active catalytic component and the mixture
sprayed, dipped or otherwise coated onto the walls of the cellular
structure. Although not intended to be limiting, reference may be
made to U.S. Pat. No. 3,565,830, which sets forth various methods
for coating a refractory honeycomb type of member with an alumina
slip and an active catalytic coating.
Reference to the accompanying drawing and the following description
thereof will serve to illustrate variations in the flexible cell
design being provided for a honeycomb type of ceramic structure and
the means for forming the special cell configurations, as well as
point out how differential temperature conditions provide failure
problems with conventional ceramic honeycomb elements.
FIG. 1 of the drawing indicates diagrammatically how differential
temperature conditions across a conventional honeycomb element can
create tensile forces leading to breakage in cell walls of a
honeycomb element.
FIGS. 2 and 3 of the drawing indicate diagrammatically two
different forms of cellular configurations which provide curved
wall portions that can better accommodate tensile stressing from
differential temperature conditions.
FIG. 2A indicates diagrammatically how an individual cell may be
deformed and elongated without leading to immediate breakage.
FIGS. 4 and 5 indicate diagrammatically how specially formed
ceramic sheet material may be joined with other specially formed
sheets to provide resulting curved wall cells.
Referring now particularly to FIG. 1 of the drawing, there is
indicated a portion of reactor unit 1 having a cylindrical form
wall or chamber portion 2 adapted to hold an internal honeycomb
element 3. Where the unit is serving as an exhaust fume reactor to
convert hydrocarbon containing exhaust gas fumes and the cellular
structure 3 is catalytically coated with an active oxidation
catalyst, there can be high temperature conditions through the
interior of the reactor of the order of 1200.degree. to
1600.degree. F. However, during certain stages of operation and
perhaps during most operating periods, there will be a
substantially higher temperature in the central core portion 3' as
compared to the peripheral portion of the honeycomb, being
indicated as 3". The hot interior will therefore tend to expand,
from the high temperature conditions, to a far greater degree than
the peripheral section 3" and, as indicated by the arrows, the
outward thrust from the expansion of the interior material will
necessarily cause resulting hoop stress or tension in the outer
ring of cells 3" and lead to wall breakage. As indicated
hereinbefore, typical ceramic materials can be relatively strong
under compression conditions but will have very little strength to
accommodate tensile forces and will readily shatter and break,
particularly where straight walls are being utilized for the
honeycomb cell configuration such as indicated in the present FIG.
1.
With reference to FIG. 2 of the drawing, there is indicated a
special cell configuration which provides curved wall portions that
can, in turn, provide flexure to a resulting honeycomb element.
Specifically, there is indicated a curved wall modification for
what might be considered a normally square pattern or layout such
as indicated by the dashed lines 4. In particular, the present
pattern is provided by having all arced or curved walls for each
and every cell of the entire honeycomb structure with the curved
walls alternating around a particular cell from being curved
inwardly to being curved outwardly. With reference to a particular
cell such as C, it will be noted that there are opposing walls 5
which are concave toward one another while at right angles thereto
there are opposing walls 6 that are convex outwardly to bow away
from one another. The net result is a dumb-bell type of shape for
the cell C by virtue of the necked-in portion in the central zone.
It will also be noted that the pattern for C is repeated at every
other location in any one row. It may also be noted that each next
adjacent, or touching, cell c' has the same dumb-bell configuration
but is at right angles to C in orientation.
In order to further illustrate the flexibility or deformation
characteristic for each cell, reference may be made to FIG. 2A of
the drawing, where an individual cell C is bounded by juncture
lines 7 and walls 5 and 6; however, when tensile forces T are
exerted with respect to the walls of the cell in the direction
indicated, there can be straightening of the walls 5 into the
partially flattened shapes 5' and the displacement of juncture
lines 7 into positionings 7' without causing juncture lines 7 to
move closer to one another. In other words, the curved or arcuate
walls 5 will tend to deform into a somewhat straighter
configuration without necessarily causing immediate breakage to
permit juncture lines to shift somewhat and give overall
flexibility to the unitary honeycomb structure. Actually, there is
probably some rotation of the immediate juncture lines at 7 and 7'
due to rigidity and moment forces that could cause some
straightening of walls 6 and a slight spreading apart of junctures
7 and 7'.
In FIG. 3 of the drawing, there is indicated what might be
considered a modified hexagonal cell pattern where hexagonal cells,
indicated by dash lines 8, are provided with alternating curved
wall portions to result in a modified clover-leaf pattern.
Specifically, each cell H has an opposing set of walls 9 that curve
or bow in the same direction in any one line of cells, another
opposing set of walls 10 which also bow in the same direction in
their row, and a third set of opposing walls 11 which bow in the
same direction in their row. It will also be noted that there is
the alternate bowing outwardly and inwardly with respect to next
adjacent walls around the periphery of the cell H, with one wall 9
going outwardly and the next adjacent walls 10 and 11 bowing
inwardly or, conversely, where a wall 9 bows inwardly the next
adjacent walls 10 and 11 will bow outwardly. In this clover-leaf
pattern, each cell H in any one row along any one of the three rows
thereof, that are 120.degree. apart, will have the same pattern or
configuration.
It may be noted further with respect to FIG. 3 of the drawing, as
compared to the pattern in FIG. 2, that the three sets of opposing
walls for any one cell will permit tensile forces to act along more
than one direction at the same time and that normally four wall
sections will be tending to flatten or straighten out under tensile
forces and that four juncture lines may be displaced with respect
to any one cell along the direction of the tensile forces. Still
further, juncture lines in a transverse direction to the tensile
forces will not tend to move toward one another and will be
maintained separate by rotational effects at juncture lines and by
the compressive resistance of the opposing walls which are
extending generally transverse to the direction of the tensile
forces. Again, the net result is that the curved wall portions can
resist tensile forces by being deformed and flattened to some
degree while at the same time permit juncture lines to move and be
displaced within any one honeycomb structure in a manner so as to
eliminate breakage of individual wall members and a resulting
failure to the overall ceramic structure.
In FIG. 4 of the drawing there is indicated a manufacturing
procedure when corrugated shaped partitioning members of green
ceramic may be intermeshed at substantially right angles to one
another to form intersecting and adjacent wall portions of a cell,
and whereby a plurality of such members can result in a
configuration similar to that shown in FIG. 2 of the drawing.
Specifically, a plurality of corrugated form members, such as 12
with slots 13, can be made to fit "egg crate" fashion into a
plurality of corrugated members, such as 14 having slots 15, and at
90.degree. thereto to form a cellular type of structure. It is to
be realized that any number of wall members 12 at desired spaced
distances would be utilized in one direction to fit into the spaced
slots 15 and that another plurality of wall members 14 would be
utilized at desired parallel spaced distances from one another to
fit into the slots 13 such that there is the intermeshing of the
walls to result in the configuration of FIG. 2 with desired sized
cells. A heating and curing operation following the interlocking of
members will result in the desired sintering of the wall members to
form tightly fused juncture lines between resulting parallel cells
throughout the honeycomb structure.
In FIG. 5 of the drawing, there is indicated that a specially
formed green sheet of ceramic material, such as 16, can be brought
into contact with a next adjacent specially formed sheet 17 at the
arcuate zones 18 to result in cell patterns H' and that such system
might well be utilized to form a cellular structure with a
multiplicity of cells H'. The heating and fusing of the juncture
areas 18 will provide the sintering and "welding" of all of the
sheets into a resulting rigid structure.
Although the desired cell patterns and configurations may be
obtained in accordance with the procedures set forth in connection
with the descriptions of FIGS. 4 and 5, it is generally preferred
that the desired cell patterns be obtained by an extruding
procedure where accurate uniform, thin wall partitions can be
provided between the multiplicity of specially shaped cells in any
one structure.
The size of the cells in a particular honeycomb structure, as
hereinbefore noted, will typically be selected to be in accordance
with pressure drop limitations for a particular stream being passed
through a honeycomb element, or through a series of elements.
Typically, cell sizes may be from one thirty-second inch, or less,
nominal diameter to one-half inch or more. It may also be noted
that honeycomb elements may be of varying shapes for a particular
reactor chamber or housing and that special shapes may be cut from
larger honeycomb units produced under any one form of manufacturing
procedure.
The present forms or configurations of cellular structures may be
made to have varying coefficients of expansion depending upon the
type of ceramic material utilized in manufacturing the skeletal
honeycomb material. Typically, the coefficient of expansion for the
honeycomb structure will be small as compared to steel or other
metal housings and as a result a core element of the present
invention may well be utilized in metal housings without requiring
a resilient expansion absorbing medium between the external wall of
the honeycomb structure and the inside wall of the housing. In
other words, honeycomb materials utilizing the present forms of
configurations can have a certain degree of flexibility within the
housing without undergoing breakage problems when subjected to
non-uniform temperature conditions.
* * * * *