U.S. patent number 3,596,703 [Application Number 04/764,208] was granted by the patent office on 1971-08-03 for method of preventing core shift in casting articles.
This patent grant is currently assigned to TRW Inc.. Invention is credited to Thomas H. Bishop, Kenneth K. Young, Jr..
United States Patent |
3,596,703 |
Bishop , et al. |
August 3, 1971 |
METHOD OF PREVENTING CORE SHIFT IN CASTING ARTICLES
Abstract
Shell-type casting molds for producing hollow cast articles, the
mold being built up by forming a low melting pattern about a
ceramic core, inserting thin metal pins through the pattern and
into engagement with the core, forming a shell mold about the
resulting pattern so that the ends of the pins are anchored in the
resulting shell mold, removing the meltable pattern, and casting
the molten metal into the cavity thus produced whereby the molten
metal dissolves the pins and no holes appear in the finished
article.
Inventors: |
Bishop; Thomas H. (Alliance,
OH), Young, Jr.; Kenneth K. (Paris, OH) |
Assignee: |
TRW Inc. (Cleveland,
OH)
|
Family
ID: |
25070001 |
Appl.
No.: |
04/764,208 |
Filed: |
October 1, 1968 |
Current U.S.
Class: |
164/132;
29/889.71; 164/30; 164/137; 164/340; 164/399 |
Current CPC
Class: |
B22C
9/10 (20130101); B22C 9/04 (20130101); B22C
21/14 (20130101); Y10T 29/49337 (20150115) |
Current International
Class: |
B22C
21/00 (20060101); B22C 9/10 (20060101); B22C
9/04 (20060101); B22C 21/14 (20060101); B22d
029/00 () |
Field of
Search: |
;164/23,24,25,26,30,31,32,34,35,36,132,137,340,351,366,370,397,398,399,361
;249/177 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
|
|
|
|
|
|
|
568,678 |
|
Jan 1959 |
|
CA |
|
470,283 |
|
Jan 1929 |
|
DT |
|
Primary Examiner: Overholser; J. Spencer
Assistant Examiner: Roethel; John E.
Claims
We claim as our invention:
1. The method of making a hollow casting which comprises forming a
low melting pattern about a ceramic core, inserting metal wires
through the resulting pattern into engagement with said ceramic
core while leaving exposed end portions on said wires, forming a
ceramic shell mold about said pattern thereby anchoring said
exposed end portions therein, melting out said pattern to leave
said metal wires providing lateral support for said core, casting
molten metal into the casting cavity provided by melting out said
pattern to thereby melt out the portions of the wires extending
through said casting cavity, and removing the ceramic core from the
casting.
2. The method of claim 1 in which said wires are composed of the
same metal as said molten metal.
3. The method of claim 1 in which said wires are inserted through
said pattern while hot.
4. The method of claim 1 in which said wires are less than about
0.050 inch in diameter.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention is in the field of precision investment casting
molds and, more specifically relates to a means for preventing core
movement or shifting of a core in a shell mold, such means
including a plurality of thin wire pins which are anchored in the
shell mold and extend into engagement with the surface of the core,
thereby spacing the core properly from the wall of the casting
cavity.
2. Description of the Prior Art
Modern investment casting procedures are frequently used to produce
castings which have complex hollow interiors. Some of the best
examples of such cast articles are turbine blades and vanes
containing a hollow interior for the purpose of providing cooling
to the blade or vane during use. In order to provide the hollow
interior in the cast article, of course, it is necessary to use a
core, usually ceramic in composition. A problem arises when there
is even a slight movement or shift of the core in the mold which
may occur during removal of the pattern material, during preheating
of the mold prior to pouring the metal therein, or during pouring
of the metal into the mold.
A prior practice which has attempted to solve this problem involved
drilling holes in the wax pattern until the core was reached. Then,
when the shell mold was formed about the pattern, the holes would
be filled with the ceramic material of the shell mold making
composition. After removal of the wax, the portions of the ceramic
material which had found their way into the holes formed posts
which remained to hold the core in place. However, when the metal
was cast around these ceramic posts, holes were left in the casting
wall. These holes then had to be plugged with metal or otherwise
removed.
Another method which has been tried involves the use of chaplets
consisting of two discs of metal connected by a cylinder. The
pattern material such as wax was injected around the chaplet, with
one head of the chaplet contacting the core and the other head
pressing against the mold wall. The chaplet was held in place by
the pressure exerted against the two heads. The disadvantage of
this method is that a relatively large mass of metal in the chaplet
prevents fusion with the poured metal.
SUMMARY OF THE INVENTION
The present invention provides a mold structure for producing
hollow castings. The mold is built up by first forming a low
melting pattern about a ceramic core, then inserting metal wires
through the resulting pattern into engagement with the ceramic core
while leaving exposed end portions on the wires. A ceramic shell
mold is then formed about the combination of core, pattern and
wires, thereby anchoring the exposed end portions of the wires in
the completed shell mold. When the pattern material is melted out,
the metal wires remain anchored in the shell mold and provide
lateral support for the core. Next, the molten metal is cast into
the casting cavity provided by the removal of the pattern, thereby
causing the portions of the wires which extended through the
casting cavity to be fused within the molten metal and disappear,
so that no imperfections remain in the body of the finished
casting.
BRIEF DESCRIPTION OF THE DRAWING
FIG. 1 is a view in elevation of a pattern having a core
therein;
FIG. 2 is a cross-sectional view taken substantially along the line
II-II of FIG. 1;
FIG. 3 is a view similar to FIG. 2 but illustrating the manner in
which the wire pins are positioned through the pattern and against
the core;
FIG. 4 is a view similar to FIG. 3 but illustrating the complete
assembly resulting after the shell mold has been formed around the
core and pattern;
FIG. 5 is a view similar to FIG. 4 but illustrating the elements of
the assembly after the pattern material has been removed; and
FIG. 6 is a view similar to FIG. 5 but showing the mold assembly
after casting and solidification of the metal, but prior to the
removal of the core.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
In FIG. 1, reference numeral 10 indicates generally a relatively
low melting pattern composed of wax, polystyrene or similar low
melting pattern making material. The particular pattern shown in
FIG. 1 is to be used for the manufacture of a turbine blade, the
blade having an arcuate vane section 11, an upper shroud 12 and a
relatively massive root portion 13. A gate forming portion 14 is
also included on the pattern to provide the cavity through which
molten metal may be introduced into the finished mold. While FIG. 1
is concerned, for purposes of simplicity, with a single pattern it
should be recognized that the present invention can be used and
usually will be used with clusters of patterns.
The pattern material has an internal core 15 composed of a ceramic
material such as fused silica. Typically, the material of the
pattern is injected about the ceramic core 15 in a conventional
pattern making mold. The core 15 may be provided with upper and
lower extensions 15a and 15b which serve to anchor the top and
bottom of the core when the ceramic mold is formed about the
core.
As illustrated in FIG. 3, a plurality of wire pins 16 is then
positioned at selected locations along the length and breadth of
the pattern, each of the pins 16 having an end portion 17 which
passes through the pattern material and engages the surface of the
ceramic core 15. In order to expedite insertion of the pin 16
through the pattern material, it is preferable to preheat the pin
16 slightly above the melting temperature of the wax or other
pattern material so that only a minimum diameter hole is provided
by the insertion of the pin 16 through the pattern material. In
order to facilitate removal of the pin, it is desirable that the
diameter of the pin 16 be kept very small, on the order of less
than 0.050 inch, although this value can be increased for larger
sizes of castings.
As also illustrated in FIG. 3, the opposed end portions 18 of the
pin 16 extend beyond the pattern material by a matter of one-eighth
or one-fourth inch or so to serve as anchoring means in the
completed shell mold.
In order to avoid contamination of the melt with the metal of the
pins 18 when they are fused therein, it is preferable that the pins
be composed of the same metal as will be used for forming the
ultimate casting.
As seen in FIG. 4, a shell mold 19 is then built up around the
combination of the core 15, the pattern 10 and the pin 16.
There are a number of ways in which to build up a ceramic shell
mold about a low melting pattern. Usually, the pattern assembly is
dipped in a series of ceramic slurries, with intermediate drying,
to form a mold which, after firing, provides a relatively gas
permeable ceramic structure of one-eighth to one-fourth inch or so
in thickness.
A particularly preferred method of building up the ceramic shell
mold involves dipping the pattern in an aqueous ceramic slurry
having a temperature about the same as that of the pattern material
to form a refractory layer of a few mils in thickness. A typical
slurry may contain ceramic material such as zirconium oxide, a
binder such as colloidal silica and a thickener and low temperature
binder such as methyl cellulose. The initial layer while still wet
is then dusted with small particles (40 to 200 mesh) of a
refractory glass composition such as that known as "Vycor" which is
a finely divided, high silicon oxide glass containing about 96
percent silica and a small amount of boric acid, together with
traces of aluminum, sodium, iron and arsenic. The pattern with the
dusted wet refractory layer on it is then suspended on a conveyor
and moved to a drying oven having a controlled humidity and
temperature, thereby drying the coated pattern adiabatically.
The steps of dipping, dusting and adiabatic drying are then
repeated using air at progressively lower humidities for succeeding
coats. For example, the first two coats can be dried with air
having a relative humidity of 45 to 55 percent. The third and
fourth coats can then be dried with a relative humidity of 35 to 45
percent, the fifth and sixth coats with a relative humidity of 25
to 30 percent, and the final coat with a relative humidity of 15 to
25 percent.
The first layer is preferably applied to a thickness of 0.005 to
0.020 inch, and the fine refractory particles are dusted onto the
wet layer with sufficient force to embed the particles therein. It
is preferred that the dusting procedure used provide a dense
uniform cloud of fine particles that strike the wet coating with
substantial impact force. The force should not be so great,
however, as to break or knock off the wet prime layer from the
pattern. This process is repeated until a plurality of integrated
layers is obtained, the thickness of the layers being about 0.005
to 0.020 inch.
After the mold is built up on the pattern material, the pattern can
be removed by heat, and then the green mold is ready for firing.
Generally, firing temperatures on the order of 1,500.degree. to
1,900.degree. F. are used. The resulting shell molds are hard,
smooth and relatively permeable.
The condition of the assembly after melt out of the pattern and
firing of the mold is illustrated in FIG. 5. It will be seen that
the core 15 remains laterally supported within the casting cavity
20 by virtue of the pins 16 which have become anchored in the
ceramic shell mold.
FIG. 6 illustrates the assembly after the molten metal has been
poured into the casting cavity 20 to provide a casting 21. The
molten metal which is usually superheated by a matter of several
hundred degrees above its liquidus temperature before pouring,
causes the portions of the pins 16 which had previously extended
into the casting cavity to become fused therein while the end
portions 18 of the pins remain anchored in the walls of the shell
mold 19.
After solidification of the metal, the shell mold 19 is broken off
and the silica core 15 is removed as by dissolution in strong
alkali solutions. The presence of the wires maintains the same
distance between the core surface and the mold wall surface during
wax removal, mold preheating, and during pouring of the metal into
the mold. This prevents core movement and the resulting undersize
wall thickness.
The process of the present invention was used to cast turbine
blades from a nickel base superalloy. The pins employed were about
0.020 inch in diameter and extended for about one-eighth to
one-fourth inch beyond the surface of the pattern. Consistently
good results were obtained with respect to preventing core movement
during the mold making and casting process as evidenced by the fact
that the method was used on a two hundred piece production run and
resulted in a better than 90 percent yield of good parts, whereas
the same number of blades produced without the supporting wires
yielded only about 10 percent good parts.
It should be evident that various modifications can be made to the
described embodiments without departing from the scope of the
present invention.
* * * * *