Metal founding – Process – Shaping a forming surface
Reexamination Certificate
2003-05-30
2004-10-05
Elve, M. Alexandra (Department: 1725)
Metal founding
Process
Shaping a forming surface
C164S519000, C164S418000, C164S459000, C164S072000, C164S268000, C427S228000, C106S038200
Reexamination Certificate
active
06799627
ABSTRACT:
I. FIELD OF THE INVENTION
The invention relates to methods for making various metallic alloys such as nickel, cobalt and iron based superalloys, stainless steel alloys, nickel aluminides, titanium and titanium aluminide alloys, zirconium base alloys into engineering components by melting of the alloys in a vacuum or under a low partial pressure of inert gas and subsequent casting of the melt under vacuum or under a low pressure of inert gas in molds machined from fine grained high density, high strength isotropic graphite wherein the mold cavity is uniformly coated with titanium carbide.
II. BACKGROUND OF THE INVENTION
A. Investment Casting
If a small casting, from ½ oz to 20 lb (14 g to 9.1 kg (mass)) or today even over 100 lb (45 kg), with fine detail and accurate dimensions is needed, lost wax investment casting is considered. This process is used to make jet engine components, fuel pump parts, levers, nozzles, valves, cams, medical equipment, and many other machine and device parts. The investment casting is especially valuable for casting difficult-to-machine metals such as superalloys, stainless steel, high-nickel alloys and titanium alloys.
The process is slow and is one of the most expensive casting processes. If a design is changed, it may require expensive alterations to a metal die (as it would in die casting also).
Preparation of investment casting molds requires operation of several equipment involving many manual processing steps such as the following.
(a) Fabrication of wax patterns via injection molding equipment, (b) manual assembly of wax patterns, (c) dipping wax patterns in six to nine different alumina or zirconia ceramic slurries contained in large vats, (d) dewaxing the molds in autoclave, and (e) preheating the molds to 2000° F. in a furnace prior to vacuum casting.
Wax injection pattern dies are expensive depending on the intricacy of the part. Lead time of six to twelve months for the wax injection die is common in the industry. Defects often occur in wax patterns due to human errors during fabrication. These defects are frequently repaired manually, which is a time consuming process.
Ceramic molds are cracked frequently during dewaxing, that leaves a positive impression on the castings, which requires manual repair.
Ceramic facecoat applied after the first dip of the wax patterns in the ceramic slurry tends to spall or crack which often get trapped as undesirable inclusions in the final castings. Ceramic facecoat would react with rare earth elements in the superalloy, such as yttrium, cerium, hafnium, etc., which may cause a deviation of the final chemistry of the castings from the required specifications.
Investment castings are removed from the mold by breaking the molds and sometime by leaching the molds in hot caustic bath followed by grit blasting. These steps additionally increase the cost of production.
B. Ceramic-mold Processes
If long-wearing, accurate castings of tool steel, cobalt alloys, titanium, or stainless steel are desired, ceramic molds are often used instead of sand molds.
The processes use conventional patterns of ceramic, wood, plastic, or metal such as steel; aluminum and copper set in cope and drag flasks. Instead of sand, a refractory slurry is used. This is made of a carefully controlled mixture of ceramic powder with a liquid catalyst binder (an alkyl silicate). Various blends are used for specific metal castings. Ceramic molds are used only one time and are expensive.
There is a need for improving the molding of various metallic alloys such as nickel, cobalt and iron based superalloys, nickel aluminides, stainless steel alloys, titanium alloys, titanium aluminide alloys, zirconium and zirconium base alloys. Metallic superalloys of highly alloyed nickel, cobalt, and iron based superalloys are difficult to fabricate by forging or machining. Moreover, conventional investment molds and ceramic molds are used only one time for fabrication of castings of metallic alloys such as nickel, cobalt and iron based superalloys, stainless steel alloys, titanium alloys and titanium aluminide alloys. This increases the cost of production.
The term superalloy is used in this specification in its conventional sense and describes the class of alloys developed for use in high temperature environments and typically having a yield strength in excess of 100 ksi at 1000° F. Nickel base superalloys are widely used in gas turbine engines and have evolved greatly over the last 50 years. As used herein the term superalloy will mean a nickel base superalloy containing a substantial amount of the &ggr;′ (gamma prime) (Ni
3
Al) strengthening phase, preferably from about 30 to about 50 volume percent of the gamma prime phase. Representative of such class of alloys include the nickel base superalloys, many of which contain aluminum in an amount of at least about 5 weight % as well as one or more of other alloying elements, such as titanium, chromium, tungsten, tantalum, etc. and which are strengthened by solution heat treatment. Such nickel base superalloys are described in U.S. Pat. No. 4,209,348 to Duhl et al. and U.S. Pat. No. 4,719,080 incorporated herein by reference in their entirety. Other nickel base superalloys are known to those skilled in the art and are described in the book entitled “Superalloys II” Sims et al., published by John Wiley & Sons, 1987, incorporated herein by reference in its entirety.
Other references incorporated herein by reference in their entirety and related to superalloys and their processing are cited below:
“Investment-cast superalloys challenge wrought materials” from Advanced Materials and Process, No. 4, pp. 107-108 (1990).
“Solidification Processing”, editors B. J. Clark and M. Gardner, pp. 154-157 and 172-174, McGraw-Hill (1974).
“Phase Transformations in Metals and Alloys”, D. A. Porter, p. 234, Van Nostrand Reinhold (1981).
Nazmy et al., The effect of advanced fine grain casting technology on the static and cyclic properties of IN713LC, Conf: High temperature materials for power engineering 1990, pp. 1397-1404, Kluwer Academic Publishers (1990).
Bouse & Behrendt, Mechanical properties of Microcast-X alloy 718 fine grain investment castings, Conf: Superalloy 718: Metallurgy and applications, Publ:TMS pp. 319-328 (1989).
Abstract of U.S.S.R. Inventor's Certificate 1306641, published Apr. 30, 1987.
WPI Accession No. 85-090592/85 & Abstract of JP 60-40644 (KAWASAKI), published Mar. 4, 1985.
WPI Accession No. 81-06485D/81 & Abstract of JP 55-149747 (SOGO), published Nov. 21, 1980.
Fang, J; Yu, B, Conference: High Temperature Alloys for Gas Turbines, 1982, Liege, Belgium, Oct. 4-6, 1982, pp. 987-997, Publ: D. Reidel Publishing Co., P.O. Box 17, 3300 AA Dordrecht, The Netherlands (1982).
Processing techniques for superalloys have also evolved as evident from the following references incorporated herein by reference in their entirety. Many of the newer processes are quite costly.
U.S. Pat. No. 3,519,503 describes an isothermal forging process for producing complex superalloy shapes. This process is currently widely used, and as currently practiced requires that the starting material be produced by powder metallurgy techniques.
The reliance on powder metallurgy techniques makes this process expensive.
U.S. Pat. No. 4,574,015 deals with a method for improving the forgeability of superalloys by producing overaged microstructures in such alloys. The gamma prime phase particle size is greatly increased over that which would normally be observed.
U.S. Pat. No. 4,579,602 deals with a superalloy forging sequence that involves an overage heat treatment.
U.S. Pat. No. 4,769,087 describes another forging sequence for superalloys.
U.S. Pat. No. 4,612,062 describes a forging sequence for producing a fine grained article from a nickel base superalloy.
U.S. Pat. No. 4,453,985 describes an isothermal forging process that produces a fine grain product.
U.S. Pat. No. 2,977,222 describes a class of superalloys.
Since, the introduction of titanium and titanium alloys in the early 1950's, these materials have found wides
Ray Ranjan
Scott Donald W.
Elve M. Alexandra
Lin Ing-Hour
Santoku America, Inc.
Stevens Davis Miller & Mosher LLP
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