US3288601A - High-strength aluminum casting alloy containing copper-magnesium-silconsilver - Google Patents
High-strength aluminum casting alloy containing copper-magnesium-silconsilver Download PDFInfo
- Publication number
- US3288601A US3288601A US534249A US53424966A US3288601A US 3288601 A US3288601 A US 3288601A US 534249 A US534249 A US 534249A US 53424966 A US53424966 A US 53424966A US 3288601 A US3288601 A US 3288601A
- Authority
- US
- United States
- Prior art keywords
- alloy
- magnesium
- aluminum casting
- strength
- casting alloy
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
Definitions
- the present invention relates to aluminum casting alloys.
- the nominal mechanical properties of many aluminum casting alloys are in the range l5,000-20,000 p.s.i. tensile strength for as-cast or annealed alloys, and 30,000-40,000 p.s.i. tensile strength for alloys in the so-called T (solution plus age) condition. Recently, this limit has been raised to 50,000 p.s.i. in castings made with special techniques which require heavy chilling, as described in the paper of applicant Merton C. Flemings, entitled PremiumQuality Light Alloy Castings, appearing at pages 10-15 of Aerospace Engineering, July 1962.
- An object of the present invention accordingly, is to provide a new and improved aluminum casting alloy 7 that is of significantly higher strength than prior-art alloys of this character.
- Table II shows mechanical properties obtainable from the novel composition of the invention.
- High-strength aluminum casting alloy having the properties of minimum tensile strength of essentially 60,000 pounds per square inch and minimum yield strength of essentially 50,000 pounds per square inch and having high ductility, said alloy consisting essentially of v 4 2.75 to 3.75% copper, 0.4 to 0.6% magnesium, 0.7 to 1.2% silicon, and 0.35 to 0.45 silver with the balance aluminum.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
Nov. 29, 1966 ELONGATION (91,)
HARDNESS (R I M. C. FLEMINGS ETAL HIGH-STRENGTH ALUMINUM CASTING ALLOY CONTAINING COPPER-MAGNESIUM-SILIGONSILVER Original Filed June 10, 1963 INVENTOI5 I MINIMUM TENSILE 6O TENSILE E STRENGTH MINIMUM YIELD 5O YIELD STRENGTH MINIMUM ELONGATION 2 COPPER 6O- COMPOS-V ITION ss- LIMITS so I I I PERCENT COPPER MERTON C. FLEMINGS RICHARD F. POLICI-I ATTORNEYS United States Patent HIGH-STRENGTH ALUMINUM CASTING ALLOY CONTAINING COPPER-MAGNESIUM-SILICON- SILVER Merton C. Flemings, Percy Road, Lexington, Mass., and Richard F. Policli, 261 Marlboro St., Boston, Mass.
Continuation of application Ser. No. 286,630, June 10, 1963. This application Mar. 14, 1966, Ser. No. 534,249
2 Claims. (Cl. 75-142) This is a continuation of application Ser. No. 286,630, filed June 10, 1963, now abandoned.
The present invention relates to aluminum casting alloys.
The nominal mechanical properties of many aluminum casting alloys are in the range l5,000-20,000 p.s.i. tensile strength for as-cast or annealed alloys, and 30,000-40,000 p.s.i. tensile strength for alloys in the so-called T (solution plus age) condition. Recently, this limit has been raised to 50,000 p.s.i. in castings made with special techniques which require heavy chilling, as described in the paper of applicant Merton C. Flemings, entitled PremiumQuality Light Alloy Castings, appearing at pages 10-15 of Aerospace Engineering, July 1962.
It is to the problem of further increasing the tensile and yield strengths of such alloys consistent with minimum elongation, that the present invention is primarily directed. The difficulties which present themselves in the development of a new casting alloy, however, are not simply those of selecting compositions which have inherently high mechanical properties; for example, nearly all wrought alloys are stronger than any casting alloy and several wrought alloys are stronger than that disclosed herein.
The problem is, rather, to attain these high properties in cast materials where the mechanism by which alloys solidify plays a controlling part. When an alloy solidifies, the initial solid has a composition with solute lower "ice A further object is to provide a novel alloy of more general utility, also.
Other and further objects will be explained hereinafter and will be more particularly pointed out in the appended claims.
The invention will now be described in connection with the accompanying drawing the single figure of which is a composite experimentally obtained graph illustrating the mechanical properties of the novel alloy of the invention. several highly desirable and optimal mechanical properties can be attained simultaneously by rather critical percentages of additive elements in the aluminum alloy. Referring to the drawing, the percentage of copper is plotted along the abscissa and pounds per square inch (tensile and yield strengthcurves I and II, respectively), elongation (percent-curve III), and hardness (curve IV) are plotted at successively lower regions along the ordinate.
It will be observed from curve I that only in a critical region of from substantially 2.75 to 3.75 percent copper, can high tensile strengths of at least 60,000 p.s.i. be attained, with an optimum for substantially 3.25 percent copper. This highly desirable result has been found to be accompanied by yield strength well in excess of 50,000 p.s.i., curve II. Below substantially 2.75 percent copper, the tensile strength falls below 60,000 p.s.i. and the yield strength falls below 50,000 p.s.i. Above substantially 3.75 percent copper, the ultimate strength again falls below 60,000 p.s.i.; but, even more dangerous from the viewpoint of the designer is the drop in ductility. A minimum elongation of about 2 percent, moreover, as shown in curve III, can be simultaneously guaranteed in all areas of the sand casting, with highly desirable hardness properties, curve IV.
The composition of the novel aluminum casting alloy of the invention that attains these results is presented in the following Table I:
than the average composition. As solidification proceeds, the composition of both liquid and solid increase in solute until finally the liquid reaches eutectic composition and solidifies isothermally. The result is microsegregation, or an uneven distribution of solute. In wrought alloy, redistribution of solute is greatly expedited by mechanical working, wherein large areas of eutectic are broken up and areas of high and low solute concentration are squeezed together. In cast alloys, however, since the part is already in the desired shape, the only mechanism for redistribution of solute is thermally, by diffusion. Thus, for a casting alloy to be commercially feasible, the alloy content must be such that at least most of the microsegregation can be eliminated by heat treatment, and within some reasonable length of time. In addition, the alloy must be reasonably castable; e.g., it must not be excessively susceptible to such foundry defects as microporosity, hot tearing, etc.
An object of the present invention, accordingly, is to provide a new and improved aluminum casting alloy 7 that is of significantly higher strength than prior-art alloys of this character.
Table II shows mechanical properties obtainable from the novel composition of the invention.
TABLE II Mechanical properties of the new alloy 1 Ultimate Yield Tensile Strength Elongation Strength (p.s.i.)
(p.s.i.)
64, 900 55, 000 16% Chill Cast Test Bar.
61, 500 557 000 }Sand Cast Test Bars.
1 Heat Treatment:
1. Solution Treatment, 16 hrs. at 930 F. 2. Water Quench. 3. Age Treatment, 12 hrs. at 345 F. Of special importance in Table II are the sand cast test bar properties. While the chill bar properties are important in showing what optimum properties may be Underlying the invention is the discovery that 3 obtained from the alloy, the sand test bar properties are indicative of properties obtained in those parts of the casting which may be less rapidly cooled. The available elongation even for sand-cast bars is of real significance.
Further modifications will occur to those skilled in the art and all such are considered to fall within the spirit and scope of the invention as defined in the appended claims.
What is claimed is:
1. High-strength aluminum casting alloy having the properties of minimum tensile strength of essentially 60,000 pounds per square inch and minimum yield strength of essentially 50,000 pounds per square inch and having high ductility, said alloy consisting essentially of v 4 2.75 to 3.75% copper, 0.4 to 0.6% magnesium, 0.7 to 1.2% silicon, and 0.35 to 0.45 silver with the balance aluminum.
2. High-strength aluminum casting alloy as claimed in claim 1, and in which up to a maximum of 0.2% titanium is included in the alloy.
References Cited by the Examiner FOREIGN PATENTS 6/1940 Great Britain.
OTHER REFERENCES Light Metal Age, May 1944, p. 19.
DAVID L. RECK, Primary Examiner. I
D. L REISDORF, R. O. DEAN, Assistant Examiners;
Claims (1)
1. HIGH-STRENGTH ALUMINUM CASTING ALLOY HAVING THE PROPERTIES OF MINIMUM TENSILE STRENGTH OF ESSENTIALLY 60,000 POUNDS PER SQUARE INCH AND MINIMUM YIELD STRENGTH OF ESSENTIALLY 50,000 POUNDS PER SQUARE INCH AND HAVING HIGH DUCTILITY, SAID ALLOY CONSISTING ESSENTIALLY OF 2.75 TO 3.75% COPPER, 0.4 TO 0.6% MAGNESIUM, 0.7 TO 1.2% SILICON, AND 0.35 TO 0.45 SILVER WITH THE BALANCE ALUMINUM.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US534249A US3288601A (en) | 1966-03-14 | 1966-03-14 | High-strength aluminum casting alloy containing copper-magnesium-silconsilver |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US534249A US3288601A (en) | 1966-03-14 | 1966-03-14 | High-strength aluminum casting alloy containing copper-magnesium-silconsilver |
Publications (1)
Publication Number | Publication Date |
---|---|
US3288601A true US3288601A (en) | 1966-11-29 |
Family
ID=24129296
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US534249A Expired - Lifetime US3288601A (en) | 1966-03-14 | 1966-03-14 | High-strength aluminum casting alloy containing copper-magnesium-silconsilver |
Country Status (1)
Country | Link |
---|---|
US (1) | US3288601A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3379518A (en) * | 1966-03-08 | 1968-04-23 | Alumalloy Company | Aluminum alloy |
EP0224016A1 (en) * | 1985-10-31 | 1987-06-03 | BBC Brown Boveri AG | Wrought aluminium alloy of the type Al-Cu-Mg having a high strength in the temperature range between 0 and 250o C |
US5032359A (en) * | 1987-08-10 | 1991-07-16 | Martin Marietta Corporation | Ultra high strength weldable aluminum-lithium alloys |
US5085830A (en) * | 1989-03-24 | 1992-02-04 | Comalco Aluminum Limited | Process for making aluminum-lithium alloys of high toughness |
US5122339A (en) * | 1987-08-10 | 1992-06-16 | Martin Marietta Corporation | Aluminum-lithium welding alloys |
US5630889A (en) * | 1995-03-22 | 1997-05-20 | Aluminum Company Of America | Vanadium-free aluminum alloy suitable for extruded aerospace products |
US6368427B1 (en) | 1999-09-10 | 2002-04-09 | Geoffrey K. Sigworth | Method for grain refinement of high strength aluminum casting alloys |
US6645321B2 (en) | 1999-09-10 | 2003-11-11 | Geoffrey K. Sigworth | Method for grain refinement of high strength aluminum casting alloys |
US20090142222A1 (en) * | 2007-12-04 | 2009-06-04 | Alcoa Inc. | Aluminum-copper-lithium alloys |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB522050A (en) * | 1938-12-02 | 1940-06-07 | Horace Campbell Hall | Aluminium alloy |
-
1966
- 1966-03-14 US US534249A patent/US3288601A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB522050A (en) * | 1938-12-02 | 1940-06-07 | Horace Campbell Hall | Aluminium alloy |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3379518A (en) * | 1966-03-08 | 1968-04-23 | Alumalloy Company | Aluminum alloy |
EP0224016A1 (en) * | 1985-10-31 | 1987-06-03 | BBC Brown Boveri AG | Wrought aluminium alloy of the type Al-Cu-Mg having a high strength in the temperature range between 0 and 250o C |
US4772342A (en) * | 1985-10-31 | 1988-09-20 | Bbc Brown, Boveri & Company, Limited | Wrought Al/Cu/Mg-type aluminum alloy of high strength in the temperature range between 0 and 250 degrees C. |
CH668269A5 (en) * | 1985-10-31 | 1988-12-15 | Bbc Brown Boveri & Cie | AL/CU/MG TYPE ALUMINUM ALLOY WITH HIGH STRENGTH IN THE TEMPERATURE RANGE BETWEEN 0 AND 250 C. |
US5122339A (en) * | 1987-08-10 | 1992-06-16 | Martin Marietta Corporation | Aluminum-lithium welding alloys |
US5032359A (en) * | 1987-08-10 | 1991-07-16 | Martin Marietta Corporation | Ultra high strength weldable aluminum-lithium alloys |
US5085830A (en) * | 1989-03-24 | 1992-02-04 | Comalco Aluminum Limited | Process for making aluminum-lithium alloys of high toughness |
US5630889A (en) * | 1995-03-22 | 1997-05-20 | Aluminum Company Of America | Vanadium-free aluminum alloy suitable for extruded aerospace products |
US6368427B1 (en) | 1999-09-10 | 2002-04-09 | Geoffrey K. Sigworth | Method for grain refinement of high strength aluminum casting alloys |
US6645321B2 (en) | 1999-09-10 | 2003-11-11 | Geoffrey K. Sigworth | Method for grain refinement of high strength aluminum casting alloys |
US20090142222A1 (en) * | 2007-12-04 | 2009-06-04 | Alcoa Inc. | Aluminum-copper-lithium alloys |
US8118950B2 (en) | 2007-12-04 | 2012-02-21 | Alcoa Inc. | Aluminum-copper-lithium alloys |
US9587294B2 (en) | 2007-12-04 | 2017-03-07 | Arconic Inc. | Aluminum-copper-lithium alloys |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4636357A (en) | Aluminum alloys | |
US5211910A (en) | Ultra high strength aluminum-base alloys | |
US4588553A (en) | Aluminium alloys | |
US5462712A (en) | High strength Al-Cu-Li-Zn-Mg alloys | |
CN109972003B (en) | High-elongation heat-resistant aluminum alloy suitable for gravity casting and preparation method thereof | |
JPS62112748A (en) | Aluminum forging alloy | |
US3288601A (en) | High-strength aluminum casting alloy containing copper-magnesium-silconsilver | |
US3475166A (en) | Aluminum base alloy | |
EP0273600A2 (en) | Aluminum-lithium alloys | |
US4555272A (en) | Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same | |
JPH0440418B2 (en) | ||
US4569702A (en) | Copper base alloy adapted to be formed as a semi-solid metal slurry | |
US20020155023A1 (en) | Foundry alloy | |
US4585494A (en) | Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same | |
US5023051A (en) | Hypoeutectic aluminum silicon magnesium nickel and phosphorus alloy | |
US3734785A (en) | Zinc forging alloy | |
Weiss | Composites and Alloys Based on the Al-Ce System | |
US1418303A (en) | Aluminum alloy | |
US3556872A (en) | Process for preparing aluminum base alloys | |
NO331275B1 (en) | Strontium aging composition with reduced solidus temperature, a method of preparing it, and use | |
US4067733A (en) | High strength aluminum alloy | |
US4661178A (en) | Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same | |
JPS6328978B2 (en) | ||
US3297435A (en) | Production of heat-treatable aluminum casting alloy | |
US2383026A (en) | Aluminum alloys |