Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberUS3401738 A
Publication typeGrant
Publication dateSep 17, 1968
Filing dateFeb 10, 1966
Priority dateFeb 10, 1966
Publication numberUS 3401738 A, US 3401738A, US-A-3401738, US3401738 A, US3401738A
InventorsParille Donald R
Original AssigneeUnited Aircraft Corp
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Core location in precision casting
US 3401738 A
Abstract  available in
Images(2)
Previous page
Next page
Claims  available in
Description  (OCR text may contain errors)

Sept. 17, 1968 D. R. PARILL CORE LOCATION IN FRECISION CASTING 2 Sheets-Sheet 1 Filed Feb. lO, 1966 &401338 Sept. 17, '1968 D. R. PARILLE CORE LOCATION IN PRECISION CASTING 2 Sheets-Sheet 2 Filed Feb. 10. 1966 F/G. a

United States Patent O" 3,401,738 CORE LOCATION IN PRECISION CASTING Donald R. Parille, Wapping, Conn., assignor to United Aircraft Corporation, East Hartford, Conn., a corporation of Delaware Filed Feb. 10, 1966, Ser. No. 526,432 6 Claims. (Cl. 164-353) ABSTRACT OF THE DISCLOSURE An improved mold for investment casting hollow articles, wherein the core is supported, at the end adjacent to the chill plate, by lateral projections located in a growth zone separate from the finished article and where the core support is out of contact with the chill plate.

This invention relates to a mold for investment casting of hollow articles and more particularly to elongated articles having one or more passages extending longitudinally therethrough from end-to-end of the article.

One feature of the invention is an arrangement for supporting the core which forms the passages in the finished article in such a :manner within the mold that the cast article will have the desired gran structure within the portion of the cast article that becomes the finished part.

Cast parts -are being produced which use, for example, turbine vanes and blades in which by directional solidification the grains within the finished part extend in a particular direction. In a turbine blade or vane it is desirable for certain purposes to have the grains running in a direction longitudinally of the -portion of the blade over which the gas flow is directed. This 'may be accornplished by casting the article in a heated mold, one end of which is in engagement with a chill plate with the mold cavity opening directly into the plate. One feature of the invention is the support of the core adjacent to the chill plate such that the grain structure of the part is not afiected and such that the passages formed by the core will be precisely located within the article.

Such cast articles when produced in this manner have a growth portion formed adjacent to the chill plate that is subsequently removed in forming the finished article ready for use. A feature of the invention is the location of the core supporting structure within this growth zone and outside of the finished article with the support so arranged as not to afiect the desired grain growth.

Other features and advantages will be apparent from the specification and claims, and from the accompanying drawings which illustrate an embodiment of the invention.

FIG. 1 is a sectional view through a mold and the surrounding heating structure for casting a turbine blade.

FIG. 2 is a fragmentary sectional view along the line 2-2 of FIG. 1.

FIG. 3 is a transverse section along the line 3-3 of FIG. 2.

FIG. 4 is a View similar to FIG. 3 showing a modification.

FIG. 5 is a fragmertary sectional view of a modified mold for use in casting a turbine vane.

FIG. 6 is a sectional view along the line 6-6 of FIG 5.

FIG. 7 is a transverse sectional view along the line 7-7 of FIG. 6.

Referring first to FIG. 1, the mold 10 is shown as made up of a plurality of individual mold elements 1011, 10b and 10c which in the particular arrangement shown are used for producing turbine blades. The mold is formed by the investment casting process and to accomplish this a pattern is provided in the usual way around which the 3,40l,738 Patented Sept. 17, 1968 "ice mold material is formed as by successively dipping and drying the pattern with coatings of suitable slurries in a well-known manner for making shell molds.

In forming the mold there is a pouring spout 12 which communicates with a top filler 14 for each of the blade patterns. Below the filler 14 is the airfoil section 16 of the blade and at the bottom of the airtoil section is the root portion 18. Communicating and over substantially the same dimension as the root portion is a growth portion 20, described in detail later. The wax pattern used in forming the mold supports a core element 22 for each of the blades. As best shown in FIG. 2, the core element includes a plurality of parallel small diameter rods 24, FIG. 2, interconnected by a top crossbar 26 and a bottom crossbar 28. The top bar is embedded in the mold material in the portion of the mold above the filler 14 and the bottom crossbar 28 is supported by inwardly extending mold projections 30 which support opposite ends of the crossbar and which, as shown in FIG. 1, are spaced from opposite side walls of the growth zone 20. The bars 24 may be of any desired cross section but in the arrangement shown they are relatvely fiat with curved opposite edges, as best shown in FIG. 3.

After the -mold has been completed and the wax pattern has been melted out to produce a mold, as shown in FIG. 1, the latter is mounted on a chill plate 32 to which the growth portion of the mold cavity is directly open. The chill plate 32 is preferably water cooled for the rapid removal of heat from the material when the desired metallic alloy has been poured into the mold. The mold is surrounded by :a cylindrical graphite susceptor 34 and the latter is surrounded by a plurality of heating coils 36 in aXially spaced relation to the susceptor. By selectively energizng these coils the entire mold may be heated to the desired temperature before any alloy is poured therein and the rate of cooling of the mold may be adjusted by suitable de-energizing of the coils.

T o obtain the desired directional grain growth within the mold, the entire mold is heated by the coils to a temperature of above that of the melting of the alloy and the chill plate is kept at a temperature of preferably below that of the boilng point of water by the circulation of water therethrough. When a metallic alloy is poured into the mold cavity the alloy begins to solidify upwardly from the chill plate and because of the directional solidification a grain growth is obtained such that from :a point above the top edge of the growth zone, represented by the dotted line 38, the growth is in parallel grains vertically located within the mold. By selectively and successively de-energizing the coils beginning with the lowermost coil, the rate and thereby the directional growth of the grains is controlled to obtain the desired grain structure. A cap -40 may be placed on top of the mold after the alloy has been poured in order to retain heat at this end of the mold during the solidification process.

After the alloy is cooled within the mold the growth zone is removed by cutting the casting along the line 38 and the tip of the blade is cut off, for example, along the 'line 42 thereby removing the crossbars 26 and 28 and leaving a turbine blade element having passages extending longitudinally therethrough. Obviously, the core materal will have been removed in 'any desired way, as 'by leaching.

The core may be of different configurations dependent upon the shape of the passage desired. For example, as shown in FIG. 4, the airfoil section 16' of the blade has a hollow therein formed by a single core element 22' with grooves 23 on opposite side walls thereof to form a ridged inner wall surface on the blade, as will be apparent.

In the arrangement shown in FIGS. 5, 6 and 7, the mold is used to produce a turbine vane having an airfoil portion 44, an inner shroud 46 and an outer shroud 48. The dotted line 50 represents material removed from the cast article to produce the finished shroud 46 and a similar dotted line 52 represents the portion of the cast article removed to form the outer shroud 48. The growth zone between the chill plate 54 and the finished portion of the cast article is that portion of the casting below the dotted line 56 which represents the approximate upper edge of the so-called growth zone.

In this arrangement, a wax pattern is arranged so that when it is successively and repeatedly dip ped in 'a slurry of mold material and dred, it will `be producing a top filler 58 communicating with the space 60 within the mold which is above and substantially coextensive with the inner shroud 464 Below the airfoil section 44 is the outer shroud 48 and the growth zone 62 is coexistence laterally therewith. The pattern supports a core 641, the upper end of which extends beyond the pattern itself and is therefore embedded in a portion 66 of the mold located vertically above the portion 60. The lower portion of the core is supported 'by a transverse core plug 68 which extends laterally from the core and is embedded in the mold material forming a portion of the boundary of the growth zone. The plug 68 which may extend laterally in both directions if desired for more secure support serves to support the lower end of the core with which it is integral in precise position within the airfoil portion of the mold after the pattern material has been melted out. By locating the plug 68 below the upper limits of the growth zone, it will be clear that the lateral opening forming in the casting by the plug 68 is removed during the machining process that completes the vane.

In this arrangement, as in FIGS. 1, 2 and 3, the mold having .been completed and the pattern material having been melted out, the mold is positioned on a chill plate 70 in the same manner that the mold is placed on the chill plate of FIG. 1. After this is completed the heating structure for the mold is placed therearound, as in FIG. 1, and the casting procedure is carried out in the same manner.

The growth zone, which has been referred to above, is described in greater detail in the copending application of Sink, Ser. No. 472,530, filed July 16, 1965, having the same assignee as the present application. A heating a-rrangement and chill plate by which the mold is heated and by which the cooling of the mold is controlled is described in the application of Barrow et al., Ser. No. 472,644, filed July 16, 1965, and also having the same assignee as the present application.

It is to be understood that the invention is not limited to the specific embodiment herein illustrated and described but may be used in other ways without departure from its spirit as defined by the following claims.

The embodirnents of the invention in which an exclusive property or privilege is claimed are defined as follows:

1. A mold for the production of cast hollow articles including, a shell having a main cavity corresponding substantially in shape to the article to be cast, and a core positioned within the cavity corresponding substantially in shape to the opening within the cast article, a filling space in the mold at one end of, and forming a Continuation of the main cavity, the end of the core extending beyond the filling space and being positioned in and supported by the mold, a cavity extension at the other end of the main cavity, and supporting elements extending laterally froni the mold into contact with the adjacent end portion of the core, the latter end portion being located within said cavity extension, the end of the cavity extension being open to be positioned on a chill plate, and the cavity extension providing a growth zone in the casting 'which is outside the dimensions of the finished article.

2. A mold as in claim 1 in which the supporting elements are located in the growth zone.

3. A mold for the production of cast hollow articles which are directionally solidified by casting in a heated mold with one end of the casting against a chill plate, said mold including a shell having a main cavity corresponding in shape to the article, a filling cavity forming an extension at one end of the main cavity, and a growth zone cavity extension at the opposite end of the main cavity, the growth zone cavity extension having an open end for contact with the chill plate, and a core positioned within the cavities and extending from the filling cavity through the main cavity and into the growth zone to dene a space within the cast article, said core extending into and being supported by the portion of the mold defining the filling cavity, the other end of the core terminating within the growth zone cavity extension (short of the open end to be out of contact with the chill plate), said mold in this growth zone extension having inwardly extending elements to engage and support the end of the core to locate it within the growth zone.

4. A mold as in claim 3 in which the elements are located externally of the part of the cast article that is used as a finished part.

5. A mold as in claim 3 in which the lateral dimension of the extensions is such as not to interfere with the desired grain growth in the cast article.

6. A mold as in claim 3 in which the temperature of the mold and the chill plate is so controlled as to produce directional grain growth from the growth zone to the filling cavity, and the core supporting elements are so positioned and 'have such a lateral dimension as not to afiect detrimentally the directional grain growth within the casting.

References Cited UNITED STATES PATENTS 239,609 4/1881 Hartman 164-399 404,187 5/1889 Fisher 164-399 1,952,500 3/1934 Huetteman 164-368 2,651,823 9/ 1953 Hohlfelder 164 398 2,985,930 5/1961 Hohlfelder 164-398 3,233,294 2/1966 Carpousis et al 164-353X J. SPENCER OVERHOLSER, P'ma'yExam'ner.

E. MAR, Assistant Exam'ner.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US239609 *Jan 21, 1881Apr 5, 1881 hartman
US404187 *Sep 28, 1888May 28, 1889 Chaplet for sand cores
US1952500 *Jul 14, 1931Mar 27, 1934Hammer Bray CompanyMold for casting gas burners
US2651823 *Feb 7, 1952Sep 15, 1953F Hohlfelder CompanyChaplet
US2985930 *Feb 4, 1959May 30, 1961F Hohlfelder CompanyChaplets
US3233294 *Feb 7, 1962Feb 8, 1966U S Magnet & Alloy CorpMethod and apparatus for casting vertically stacked magnet bodies
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3596703 *Oct 1, 1968Aug 3, 1971Trw IncMethod of preventing core shift in casting articles
US3620289 *Apr 1, 1970Nov 16, 1971United Aircraft CorpMethod for casting directionally solified articles
US3659645 *Aug 9, 1965May 2, 1972Trw IncMeans for supporting core in open ended shell mold
US3662816 *Apr 30, 1970May 16, 1972Trw IncMeans for preventing core shift in casting articles
US3668389 *Sep 19, 1969Jun 6, 1972United Aircraft CorpPhotosensitive device comprising photoconductive and photovoltaic layers
US3794100 *Jun 18, 1970Feb 26, 1974Cryomagnetics CorpMethod of making a billet suitable for manufacturing into a superconductor
US3795978 *Sep 24, 1971Mar 12, 1974J RaymondMethod of fabricating a composite superconductor
US3809147 *Sep 24, 1971May 7, 1974J RaymondMethod for making products suitable for use in forming composite superconductors
US3818578 *Sep 24, 1971Jun 25, 1974Cyromagnetics CorpMethod of casting and working a billet having a plurality of openings therein
US3957104 *Feb 27, 1974May 18, 1976The United States Of America As Represented By The Administrator Of The United States National Aeronautics And Space AdministrationMethod of making an apertured casting
US4093017 *Dec 29, 1975Jun 6, 1978Sherwood Refractories, Inc.Silica, mineralizer containing devitrifying metallic ions, cristobalite formation, heat resistance
US4180119 *Sep 18, 1978Dec 25, 1979Howmet Turbine Components CorporationMold for directionally solidified single crystal castings and method for preparing same
US4474224 *Jun 11, 1982Oct 2, 1984Rolls-Royce LimitedFoundry machinery
US4487246 *Apr 12, 1982Dec 11, 1984Howmet Turbine Components CorporationSystem for locating cores in casting molds
US4596281 *Sep 2, 1982Jun 24, 1986Trw Inc.Mold core and method of forming internal passages in an airfoil
US4811778 *Apr 4, 1988Mar 14, 1989Rolls-Royce PlcMethod of manufacturing a metal article by the lost wax casting process
US4913217 *Jan 23, 1989Apr 3, 1990Farley, Inc.Locators for expendable core in die casting die
US5505250 *Aug 19, 1994Apr 9, 1996Rolls-Royce PlcInvestment casting
US5718278 *Jun 18, 1997Feb 17, 1998Baum; RobertMethod for producing hollow ring having inner round radius design
US5916271 *Dec 5, 1997Jun 29, 1999Baum; RobertHollow jewelry ring having inner round design
US5979537 *Aug 26, 1998Nov 9, 1999Baum; RobertWax replica and soluble core insert used for producing hollow jewelry ring
US6032719 *Aug 26, 1998Mar 7, 2000Baum; RobertMethod for producing hollow jewelry ring
US6123141 *Jun 28, 1999Sep 26, 2000Baum; RobertMethod of forming a wax replica
US6467526Oct 23, 2000Oct 22, 2002I.B. Goodman Manufacturing Co., Inc.Method of making a jewelry ring in a vertical mold
US20100200189 *Feb 12, 2009Aug 12, 2010General Electric CompanyMethod of fabricating turbine airfoils and tip structures therefor
Classifications
U.S. Classification164/353, 164/399, 164/368, 164/359, 164/361
International ClassificationB22C9/04, B22D27/04
Cooperative ClassificationB22C9/04, B22D27/045
European ClassificationB22D27/04A, B22C9/04