U.S. patent number 3,848,654 [Application Number 05/225,222] was granted by the patent office on 1974-11-19 for precision casting with variable angled vanes.
This patent grant is currently assigned to Howmet Corporation. Invention is credited to James H. Boyle, John E. Ingalls.
United States Patent |
3,848,654 |
Boyle , et al. |
November 19, 1974 |
PRECISION CASTING WITH VARIABLE ANGLED VANES
Abstract
The manufacture of a nozzle having optimum flow characteristics
by angular variation in the vanes in which such angular variation
between vanes is a function of mating angular surfaces and may be
achieved by ring segments having differently angled sockets for the
vane patterns and/or by vanes having angular rotation relative to
their locating studs adapted to be received within the sockets of
the segment members.
Inventors: |
Boyle; James H. (Muskegon,
MI), Ingalls; John E. (Pentwater, MI) |
Assignee: |
Howmet Corporation (Greenwich,
CT)
|
Family
ID: |
22844031 |
Appl.
No.: |
05/225,222 |
Filed: |
February 10, 1972 |
Current U.S.
Class: |
164/34; 164/45;
164/246; 164/137; 164/249 |
Current CPC
Class: |
B22C
9/04 (20130101) |
Current International
Class: |
B22C
9/04 (20060101); B22c 009/02 () |
Field of
Search: |
;164/34,249,245,235,246,238,247,35,36,248,236,45,59,333
;249/102,155,156,159,57,59,61,62 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
|
|
|
|
|
|
|
479,671 |
|
Dec 1951 |
|
CA |
|
589,496 |
|
Dec 1959 |
|
CA |
|
1,194,532 |
|
Jun 1965 |
|
DT |
|
Primary Examiner: Husar; Francis S.
Assistant Examiner: Rising; V. K.
Claims
We claim:
1. In the method of producing ring structures formed of a ring
member with a plurality of vanes of the same design extending
radially in circumferentially spaced apart relation from the ring
member, with some of the vanes extending at an angle of rotation
with reference to their radial axes normal to the ring axis which
differs from others of the vanes, in which an integral pattern of
the ring member and radially extending vanes is formed of heat
disposable material for use in producing an integral casting by
precision casting technique, the steps of providing separate heat
disposable patterns of the vanes with locating projections
extending from the ends thereof, providing separate ring forming
segments of heat disposable material having sockets shaped to
correspond with the locating projections on the ends of the vanes
for receiving the locating projections therein in fitting relation
for assembly of the vane patterns with the segments and in which
the segments are formed with end walls shaped to interfit one with
another for assembly into a composite ring structure, in which in
order to assemble the patterns with vanes extending at an angle of
rotation with reference to their radial axes which differ from
others of the vanes in the assembled ring structure, each of the
vanes are the same and each of the segments are the same except for
the sockets which form one segment to another different in their
angle of rotation with reference to the radial axis, assembling
said vanes with the segments having the sockets differing in angles
of rotation corresponding to the desired differences in angle of
rotation of the assembled vanes in the ring structure, and joining
the ring segments with the assembled vanes into the ring
structure.
2. In the method of producing ring structures formed of a ring
member with a plurality of vanes of the same design extending
radially in circumferentially spaced apart relation from the ring
member, with some of the vanes extending at an angle of rotation
with reference to their radial axes normal to the ring axis which
differs from others of the vanes, in which an integral pattern of
the ring member and radially extending vanes is formed of heat
disposable material for use in producing an integral casting by
precision casting technique, the steps of providing separate heat
disposable patterns of the vanes with locating projections
extending from the ends thereof, providing separate ring forming
segments of heat disposable material having sockets shaped to
correspond with the locating projections on the ends of the vanes
for receiving the locating projections therein in fitting relation
for assembly of the vane patterns with the segments, and in which
the segments are formed with end walls shaped to interfit one with
another for assembly into a composite ring structure, in which in
order to assemble the pattern with the vanes extending at angles of
rotation with reference to their radial axes which differ from
others of the vanes in the assembled ring structure, each of the
segments are the same with sockets having the same angle of
rotation and each of the vanes are the same except for the
projections which form one vane to another different in their angle
of rotation with respect to the radial axes, assembling the
segments with the vanes having the projections with differences in
angles of rotation corresponding to the desired differences in
angle of rotation of the assembled vanes in the ring structure, and
joining the ring segments with the assembled vanes into the ring
structure.
3. The method as claimed in claim 1 which includes the step of
forming a mold shell about the pattern assembly, removing the heat
disposable material to leave a shell mold having an integral mold
cavity of a ring structure with radially extending vanes which
differ in angular rotation, and casting molten metal into the shell
mold to fill the mold cavity and then removing the metal casting
from the mold.
Description
This invention relates to the utilization of the lost wax process
in precision casting in the development of a turbine nozzle with
mixing vanes selectively adjusted at angles to provide an optimum
flow area and to the construction of disposable vane patterns into
a composite mold to enable the casting of the turbine nozzle as an
integral unit embodying the developed design features.
To the present, it has been necessary to re-tool for evaluation of
each of various gas flows through the nozzle, as effected by
angular arrangement of the nozzle vanes in the assembly. When
consideration is given to the number of vanes making up the nozzle,
evaluation for the various gas flows for the entire nozzle would be
very expensive, especially in the design development stage. Such
angular variations have been achieved usually by a machining
operation performed on selected vanes, which usually are fabricated
of hard to machine super-alloys.
It is an object of this invention to adapt the precision casting
process to the production of integral turbine nozzles with angular
arrangement of mixing vanes for optimum gas flow, and in which the
development of the particular nozzle design by angular adjustment
of the vanes can be conducted in a simple, efficient, and
relatively inexpensive manner.
These and other objects and advantages of this invention will
hereinafter appear and for purposes of illustration, but not of
limitation, embodiments of the invention are shown in the
accompanying drawings in which
FIG. 1 is an elevational view of a nozzle assembly formed of a
plurality of heat disposable plastic and/or wax patterns assembled
into a ring for use in casting an integral nozzle;
FIG. 2 is a sectional view taken along the line 2--2 of FIG. 1;
FIG. 3 is a sectional view taken along the line 3--3 of FIG. 1,
illustrating the vane patterns in an angular position, referred to
as a closed angle;
FIG. 4 is a sectional view similar to that of FIG. 3 in which the
vane patterns are arranged at an angle, referred to as an open
angle;
FIG. 5 is a sectional view similar to those of FIGS. 3 and 4, in
which some of the vane patterns are at an open angle while others
are arranged at closed angles;
FIG. 6 is a perspective view of a segment of the ceramic shell mold
formed about the assembled patterns to form the vaned nozzle;
FIG. 7 is an elevational view of the integral cast metal nozzle;
and
FIG. 8 is a side elevational view of a normal design for a single
nozzle vane pattern with the cross-sectional view being illustrated
in FIGS. 3 to 5.
FIG. 9 is an exploded view indicating a relationship between the
vanes, studs, and sockets.
Castings of complex shapes have been precision cast of metals and
super-alloys by providing patterns of heat disposable material,
such as of wax or plastics or combinations thereof, conforming to
the shape and dimension of the part or parts to be molded. One and
preferably a plurality of such patterns are assembled into a
cluster having the necessary sprues and runners which are also
formed of heat disposable material.
The cluster is then processed through a series of alternating dip
coats and stucco coats of ceramic materials as described in U.S.
Pat. No. 2,961,751, until a ceramic shell of sufficient thickness
and strength, when cured, has been built up about the exposed
surfaces of the cluster. After sufficient drying or setting of the
applied dip and stucco coats, the assembly is exposed to high
temperature sufficient to melt out as well as to burn out the heat
disposable components, leaving a ceramic shell having mold cavities
formerly occupied by the patterns and other heat disposable
material and conforming to the shape and dimensions thereof.
The ceramic shell is then further heated to cure and/or preheated
prior to metal pouring. The poured metal flows through the gates
and runners to fill the mold cavities formerly occupied by the heat
disposable patterns. After allowing the casting to cool for
solidification of the metal, the ceramic shell is broken away to
expose the metal casting which is separated into its elements and
cleaned.
The described casting process embodies the principles of the "lost
wax process," but with considerable improvement for precision
casting of complicated shapes of super-alloys and other metals,
such as titanium, which are difficult to machine or otherwise
process.
Referring now to the drawings for a description of the invention, a
nozzle vane 10 has the general shape of the body portion 12, shown
in FIG. 8 in side elevational view, with the front to back having
the shape shown in cross-sectional view in FIGS. 3 to 5 in the form
of an arcuate member in which the leading edge portion 14 is shown
as extending in the downward direction in FIGS. 3 to 5 and which
tapers gradually from the leading edge portion to a trailing edge
portion 16 of lesser dimension.
The pattern for the vane is pressure molded to the desired shape
and dimension of wax, thermoplastic or wax-plastic combinations, or
of other heat disposable material with a locating stud 18,
preferably of trapezoidal shape, extending beyond the opposite ends
thereof for interfitting into a similarly dimensioned socket 22 in
outer and inner rim segments 24 and 26, which are also molded of
heat disposable material, as previously defined.
Each segment 24 of the outer rim is formed with concentric
curvilinear inner and outer walls 28 and 30, spaced one from the
other by an amount corresponding to the radial thickness of the
outer rim 32 of the nozzle, with each segment 24 forming an equal
cord or segment of a circle with its center at the axis of the
nozzle whereby the outer walls 30 of each segment will have a
curvature having a radius corresponding to the distance between the
outer wall to the axis while the inner wall will have a curvature
having a radius corresponding to the distance between the inner
wall and the axis. Similarly, each segment of the inner rim 34 is
formed with concentric curvilinear inner and outer walls spaced
radially by an amount corresponding to the radial thickness of the
inner rim of the nozzle with each segment forming an inner cord of
equal dimension of a circle about the same axis as the outer rim
whereby the inner wall 36 of the inner segment will have a
curvature having a radius corresponding to the distance to the
center while the outer wall 38 will have a curvature with a radius
corresponding to the distance between the outer wall and the
axis.
The segments of the inner and outer rims are each formed with
leading and trailing walls 40 and 42 which are adapted to effect an
interfitting relationship therebetween so that the segments of the
outer rim can be interfitted to form a complete circular rim while
the segments of the inner rim can be interfitted to form a complete
circular member. This can be accomplished as shown in the drawing,
by designing the leading walls 44 and 46 to extend angularly from
an intermediate portion thereof with parallel trailing walls, or by
a type of tongue and groove arrangement in the form of grooved or
rectangular recessed portions on the leading edge and trailing
edges.
Each segment is formed with a socket 22 extending radially
outwardly from an intermediate portion of the inner wall and shaped
and dimensioned to receive the locating stud 18 in fitting
relationship therein to secure the vane pattern in position of use
between the rim members. Usually the segments are fitted onto the
opposite ends of the vane pattern to form a unit, a plurality of
which may thereafter be interfitted to form the nozzle assembly, as
a pattern of heat disposable material, as shown in FIG. 1, with the
vane pattern equally circumferentially spaced to extend radially
between the inner and outer rim members.
In accordance with one embodiment for the practice of this
invention, the vane patterns are all of the same construction to
define a single pattern design while the segments are formed with
sockets at varying angles, such as one set in which each socket is
rotated about its center to a -10% or -10.degree. angle with the
normal for an open angle position while in another set the sockets
are rotated about the center to a +10% or +10.degree. angle to a
closed angle.
Thus by the selection of pairs of segments with open or closed
angles, it becomes possible with only two segment designs to
achieve wide variation in the angles of each of the vanes of the
nozzle between open and closed positions to enable production of
nozzle castings of various designs of angular arrangement of vanes
throughout the entire nozzle. This enables development of nozzles
of various angle designs for testing to achieve an optimum gas flow
for the particular nozzle application.
Once the nozzle has been selected for the desired gas flow-through
properties, the designed nozzle with the determined variation in
the angles of the various vanes can be duplicated by duplication of
the segment arrangement of the designed unit to provide nozzles
having variable angled vanes in predetermined arrangement.
It will be apparent that instead of providing segments which differ
only between two angles in socket arrangements, additional sockets
can be provided with angular arrangements in between open and
closed angles to provide still greater flexibility in design and
finally in production.
By way of an alternative embodiment of this invention, instead of
providing vane patterns of identical construction and segments
having differently angled sockets, it will be apparent that the
elements can be reversed with the sockets in the segments all being
formed with a single angle to enable free interchange between
segments but in which variation in angular arrangement is
introduced into the body portion of the vanes relative to their
locating studs which are adapted to be received in fitting relation
in the sockets. In this instance, the angular relation of the vanes
relative to their locating studs can vary from normal between
closed and open angles and, as previously pointed out, at various
angles therebetween. Under these conditions, the segments are all
of the same design and flexibility in angular design of the vanes
for variation in gas flow-through characteristics is achieved only
by variation in vanes molded at the different angles.
The segments are joined together in the ring assembly in the usual
manner, such as by the application of adhesive or hot wax at the
adjacent surfaces to interbond one segment to the other in the
pattern assembly.
From this point on, the conventional processes and materials
employed in shell molding manufacture and metal casting are
followed.
Briefly described, the runners 50 and gates of heat disposable
material are joined to connect the segments of the outer and inner
rim portions of the nozzle pattern with a central pouring cup
54.
The assembly is then wet first with a conventional dip coat
composition, as described in U.S. Pat. No. 2,961,751, as by
immersion in a bath of the dip coat composition or by rotation of
the ring assembly while partially immersed in the fluid dip coat
composition, as described in the copending application Ser. No.
855,941, filed Sept. 8, 1969 now U.S. Pat. No. 3,668,177. After the
excess dip coat composition has been drained from the surfaces of
the assembled mold patterns, and while the surfaces of the assembly
are still wet, the stucco coat is applied as by sprinkling the
ceramic stucco materials onto the wet surfaces of the assembly, as
described in the aforementioned patent, whereby an amount of stucco
is retained by the dip coat to form a first layer on the pattern
surface.
The steps of wetting with the dip coat composition and stuccoing
are repeated, with intermediate drying, until a shell 56 of the
desired thickness and strength has been built up about the pattern
assembly, or cluster as it is referred to in the trade.
After the shell of ceramic material has been built up about the
pattern assembly, the heat disposable material is removed by
exposure of the assembly to elevated temperatures sufficient to
melt and/or burn out the wax and plastic materials. For this
purpose, it is sufficient to heat the assembly to an elevated
temperature, usually about 1,800.degree. F, but can be higher, for
from 3 to 30 minutes, depending somewhat upon the mass of material
requiring removal and the thickness of the ceramic shell mold. At
such temperatures, the small amount of organic material which does
not flow from the inverted assembly upon heating will be burned out
to leave a shell mold having mold cavities corresponding to the
patterns and connecting channels through which the molten metal may
flow from the pouring cup to the shell molds.
After removal of the pattern, gates and runners of heat disposable
material, the resulting shell mold can be fired to cure the ceramic
material. Such firing to cure can be achieved as a part of the
heating step for pattern removal or it can be carried out as a
separate pre-heating step prior to metal pouring. In any event, it
is desirable to heat the shell mold to an elevated temperature
which approximates the temperature of the molten metal to be
poured, such as to a temperature within the range of 1,600.degree.
F in the casting of super-alloys or other high melting point alloy
having a nickel or cobalt base. This temperature may be higher
depending upon the part to be cast and the alloy. After the mold is
pre-heated to the desired pouring temperature, the molten metal is
poured into the mold through the pouring cup to fill the mold
cavities and the mold with the motlen metal cast therein is set
aside to cool for gradual solidification of the molten metal.
When sufficiently cooled, the ceramic shell is broken away to
release the cast nozzle, illustrated by FIG. 7, with the vanes
integrally joined to the inner and outer rims as an integral
assembly in which the angular rotation of the vanes corresponds to
the angular rotation of the patterns originally assembled between
the rims of heat disposable material in making up the pattern
assembly.
It will be apparent that integral nozzles with various angular
rotations of the vanes can be produced in accordance with the
practice of this invention merely by making use of pre-selected
vane patterns and/or ring segments which vary either in the angular
relation of the vanes relative to their supports or in the angular
relation of the sockets in which the locating studs for the vanes
are received and that such angular rotation of the vanes can be
varied selectively throughout the entire ring in a simple and
efficient manner, with a minimum number of segments and vane
patterns.
It will be further understood that while the invention has been
described with reference to the manufacture of vaned nozzles with
variations in angular rotation of the vanes for development of
optimum flow patterns, the concepts of the invention will have
equal application to the development and construction of turbine
wheel assemblies embodying buckets or blades, wherein variation in
angular rotation is desirable for the development of optimum
performance characteristics and in other wheeled or circular rim
structures in which vanes, buckets or blades are mounted in a
preferred integral assembly.
While the invention has been described with reference to the
preparation of shell molds for casting nozzles, turbine wheels and
the like metal castings wherein the shell mold is formed of ceramic
material obtained from the dip coat composition and stucco, the
invention is not limited with respect to the compositions of the
dip coat or stucco but may include shell molds formed to include
carbon or graphite and the like materials such as employed in the
manufacture of shell molds for the casting of titanium and other
active metals, and as described in U.S. Pat. No. 3,296,666; No.
3,266,106; No. 3,257,692; No. 3,256,574; No. 3,248,763; No.
3,241,200, and others.
It will be understood that changes may be made in the details of
formulation, construction and operation, without departing from the
spirit of the invention, especially as defined in the following
claims.
* * * * *