Cast aluminum alloy for structural components

US9771635B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9771635-B2
Application numberUS-201213545345-A
CountryUS
Kind codeB2
Filing dateJul 10, 2012
Priority dateJul 10, 2012
Publication dateSep 26, 2017
Grant dateSep 26, 2017

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  1. Title

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  2. Abstract

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  4. Key dates

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  5. First independent claim

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Abstract

Official abstract text for this publication.

An aluminum alloy that can be cast into structural components wherein the alloy has reduced casting porosity, improved combination of mechanical properties including tensile strength, fatigue, ductility in the cast condition and in the heat treated condition.

First claim

Opening claim text (preview).

What is claimed is: 1. An aluminum alloy consisting essentially of, by weight percentage, from about 11% to about 13.5% Silicon, up to about 0.2% Copper, from about 0.15% to about 0.55% Magnesium, from about 0.3% to about 0.4% Iron, about 0.4% Manganese, up to about 0.1% Titanium, about 0.5% Zinc, from about 0.015% to about 0.08% Strontium, from about 0.01% to about 0.05% Boron, and the balance aluminum. 2. The alloy of claim 1 wherein the ratio of Manganese to Iron is 0.6 to 1.0. 3. A cast cylinder head for an internal combustion engine formed of the alloy recited in claim 1 . 4. At least one of an engine block, wheel, suspension part, or airplane door formed of the alloy recited in claim 1 . 5. The aluminum alloy of claim 1 wherein the aluminum alloy consists essentially of, in weight percentage, from about 11.5% to about 13% Silicon, up to about 0.2% Copper, from about 0.3% to about 0.4% Magnesium, from about 0.3% to about 0.4% Iron, about 0.4% Manganese, up to about 0.1% Titanium, about 0.5% Zinc, from about 0.015% to about 0.08% Strontium, from about 0.01% to about 0.05% Boron, and the balance aluminum. 6. The aluminum alloy of claim 1 wherein the weight percentage of Silicon is from about 11.5% to about 12.5%, the weight percentage of Strontium is from about 0.03% to about 0.04%, and the weight percentage of Boron is from about 0.03% to about 0.04%. 7. The aluminum alloy of claim 1 wherein the weight percentage of Silicon is about 12.5%, the weight percentage of Strontium is from about 0.04% to about 0.05%, and the weight percentage of Boron is from about 0.025% to about 0.03%. 8. The aluminum alloy of claim 1 wherein the weight percentage of Silicon is 11.8%, the weight percentage of Magnesium is 0.33%, from about 0.3% to about 0.4% Iron, the weight percentage of Strontium is 0.034%, and the weight percentage of Boron is 0.032%. 9. The aluminum alloy of claim 1 wherein total impurity is less than 0.15% by weight. 10. The aluminum alloy of claim 1 wherein the weight percentage of Silicon is from about 13% to about 13.5%. 11. The aluminum alloy of claim 1 wherein the weight percentage of Strontium is from about 0.05% to about 0.08%. 12. An automotive cylinder head formed of the alloy consisting essentially of, by weight percentage, from about 11% to about 13.5% Silicon, up to about 0.2% Copper, from about 0.15% to about 0.55% Magnesium, from about 0.3% to about 0.4% Iron, about 0.4% Manganese, up to about 0.1% Titanium, about 0.5% Zinc, from about 0.015% to about 0.08% Strontium, from about 0.01% to about 0.05% Boron, and the balance aluminum. 13. The automotive cylinder head of claim 12 wherein the alloy is cast. 14. An aluminum alloy consisting essentially of, by weight percentage, from 11% to 13.5% Silicon, from 0.20% to 0.5% Copper, greater than 0.35% Magnesium, about 0.3% Iron, about 0.3% Manganese, up to 0.1% Titanium, from 0.1% to 0.4% Zinc, greater than 0.02% Strontium, greater than 0.032% Boron, and the balance aluminum. 15. The aluminum alloy according to claim 14 , wherein the weight percentage Magnesium is from 0.4 to 0.55% Magnesium, the weight percentage of Strontium is from 0.02% to 0.08%, and the weight percentage of Boron is from 0.03% to 0.05% Boron. 16. A cast cylinder head for an internal combustion engine formed of the alloy recited in claim 14 . 17. At least one of an engine block, wheel, suspension part, or airplane door formed of the alloy recited in claim 14 . 18. The composition according to claim 14 , wherein Titanium is not included. 19. The aluminum alloy of claim 14 wherein the weight percentage of Silicon is 12.6%, the weight percentage of Magnesium is 0.3%, from about 0.3% to about 0.4% Iron, the weight percentage of Strontium is 0.045%, and the weight percentage of Boron is 0.026%. 20. The aluminum alloy of claim 14 wherein the weight percentage of Silicon is 13.25%, the weight percentage of Magnesium is 0.25%, from about 0.3% to about 0.4% Iron, the weight percentage of Strontium is 0.048%, and the weight percentage of Boron is 0.022%.

Assignees

Inventors

Classifications

  • C22C21/02Primary

    with silicon as the next major constituent · CPC title

  • with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C · CPC title

  • Modified aluminium-silicon alloys · CPC title

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Frequently asked questions

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What does patent US9771635B2 cover?
An aluminum alloy that can be cast into structural components wherein the alloy has reduced casting porosity, improved combination of mechanical properties including tensile strength, fatigue, ductility in the cast condition and in the heat treated condition.
Who is the assignee on this patent?
Wang Qigui, Liao Hengcheng, Gm Global Tech Operations Llc
What technology area does this patent fall under?
Primary CPC classification C22C21/02. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Sep 26 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).