Process for producing an engine component, engine component and the use of an aluminum alloy

Abstract

The present disclosure describes a process for producing an engine component, e.g., a piston for an internal combustion engine, where an aluminum alloy is cast by gravity diecasting, and an engine component composed at least partly of an aluminum alloy. The aluminum alloy includes silicon 8% to 17% by wt., copper 2% to 10% by wt., nickel 1% to 6% by wt., iron 0.1% to 3.5% by wt., magnesium 0.1% to 2% by wt., manganese 0.1% to 4% by wt., barium up to 4% by wt., titanium up to 0.5% by wt., zirconium up to 0.4% by wt., vanadium up to 0.3% by wt., phosphorus up to 0.05% by wt., chromium up to 0.3% by wt., and a balance of aluminum and unavoidable impurities.

Claims

1. A process for producing an engine component, comprising: casting an aluminum alloy in a gravity diecasting method, wherein the aluminum alloy contains the following alloy elements: silicon 11% to 14% by wt., copper 2% to 10% by wt., nickel 1% to 6% by wt., iron 0.1% to 3.5% by wt., magnesium 0.1% to 2% by wt., manganese 0.1% to 4% by wt., barium up to 4% by wt., titanium up to 0.5% by wt., zirconium up to 0.4% by wt., vanadium up to 0.3% by wt., phosphorus up to 0.05% by wt., chromium up to 0.3% by wt., and a balance of aluminum and unavoidable impurities.

2. The process according to claim 1, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 13% by wt., copper 3% to 6% by wt., nickel 2% to 6% by wt., iron 0.7% to 2% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium up to 4% by wt., titanium up to 0.3% by wt., zirconium up to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., and the balance being aluminum and unavoidable impurities.

3. The process according to claim 1, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 14% by wt., copper 3% to 10% by wt., nickel 1.5% to 5% by wt., iron 0.7% to 2% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium 0% to 4% by wt., titanium 0.03% to 0.3% by wt., zirconium 0.03% to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

4. The process according to claim 1, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 13% by wt., copper 4% to 7% by wt., nickel 1% to 3% by wt., iron 0.15% to 1% by wt., magnesium 0.2% to 1% by wt., manganese ≥0.1% by wt., barium up to 1% by wt., titanium 0.03% to 0.3% by wt., zirconium 0.03% to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

5. The process according to claim 1, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 14% by wt., copper 5.2% to 9% by wt., nickel 1.5% to 4% by wt., iron 0.2% to 1.5% by wt., magnesium 0.2% to 1% by wt., manganese 0.2% to 1.5% by wt., barium up to 4% by wt., titanium up to 0.3% by wt., zirconium up to 0.3% by wt., vanadium up to 0.3% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

6. The process according to claim 5, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 14% by wt., copper 5.2% to 8% by wt., nickel 1.5% to 4% by wt., iron 0.2% to 1.5% by wt., magnesium 0.2% to 1% by wt., manganese 0.2% to 1.3% by wt., barium up to 1% titanium 0.05% to 0.2% by wt., zirconium 0.05% to 0.2% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., and the balance being aluminum and unavoidable impurities.

7. An engine component, comprising: an aluminum alloy, wherein the aluminum alloy contains the following alloy elements: silicon 11% to 14% by wt., copper 2% to 10% by wt., nickel 1% to 6% by wt., iron 0.1% to 3.5% by wt., magnesium 0.1% to 2% by wt., manganese 0.1% to 4% by wt., barium up to 4% by wt., titanium up to 0.5% by wt., zirconium up to 0.4% by wt., vanadium up to 0.3% by wt., phosphorus up to 0.05% by wt., chromium up to 0.3% by wt., and a balance of aluminum and unavoidable impurities.

8. An aluminum alloy for an engine component, comprising a composition including the following alloy elements: silicon 8% to 17% by wt., copper 2% to 10% by wt., nickel 1% to 6% by wt., iron 0.1% to 3.5% by wt., magnesium 0.1% to 3% by wt., manganese 0.7% to 2.5% by wt., barium up to 4% by wt., titanium up to 0.5% by wt., zirconium up to 0.4% by wt., vanadium up to 0.3% by wt., phosphorus up to 0.05% by wt., chromium up to 0.3% by wt., and a balance of aluminum and unavoidable impurities.

9. The aluminum alloy according to claim 8, wherein the composition consists of the alloy elements: silicon 8% to 13% by wt., copper 3% to 6% by wt., nickel 2% to 6% by wt., iron 0.7% to 2% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium up to 4% by wt., titanium up to 0.3% by wt., zirconium up to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., and the balance being aluminum and unavoidable impurities.

10. The aluminum alloy according to claim 8, wherein the composition consists of the alloy elements: silicon 8% to 15% by wt., copper 3% to 10% by wt., nickel 1.5% to 5% by wt., iron 0.7% to 2% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium 0% to 4% by wt., titanium 0.03% to 0.3% by wt., zirconium 0.03% to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

11. The aluminum alloy according to claim 8, wherein the composition consists of the alloy elements: silicon 11% to 13% by wt., copper 4% to 7% by wt., nickel 1% to 3% by wt., iron 0.15% to 1% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium up to 1% by wt., titanium 0.03% to 0.3% by wt., zirconium 0.03% to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

12. The aluminum alloy according to claim 8, wherein the composition consists of the alloy elements: silicon 10% to 15% by wt., copper 5.2% to 9% by wt., nickel 1.5% to 4% by wt., iron 0.2% to 1.5% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium up to 4% by wt., titanium up to 0.3% by wt., zirconium up to 0.3% by wt., vanadium up to 0.3% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

13. The aluminum alloy according to claim 12, wherein the composition consists of the alloy elements: silicon 11% to 14% by wt., copper 5.2% to 8% by wt., nickel 1.5% to 4% by wt., iron 0.2% to 1.5% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium up to 1% titanium 0.05% to 0.2% by wt., zirconium 0.05% to 0.2% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., and the balance being aluminum and unavoidable impurities.

14. The engine component according to claim 7, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 13% by wt., copper 3% to 6% by wt., nickel 2% to 6% by wt., iron 0.7% to 2% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium up to 4% by wt., titanium up to 0.3% by wt., zirconium up to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., and the balance being aluminum and unavoidable impurities.

15. The engine component according to claim 7, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 14% by wt., copper 3% to 10% by wt., nickel 1.5% to 5% by wt., iron 0.7% to 2% by wt., magnesium 0.2% to 1% by wt., manganese 0.7% to 2.5% by wt., barium 0% to 4% by wt., titanium 0.03% to 0.3% by wt., zirconium 0.03% to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

16. The engine component according to claim 7, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 13% by wt., copper 4% to 7% by wt., nickel 1% to 3% by wt., iron 0.15% to 1% by wt., magnesium 0.2% to 1% by wt., manganese ≥0.1% by wt., barium up to 1% by wt., titanium 0.03% to 0.3% by wt., zirconium 0.03% to 0.3% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

17. The engine component according to claim 7, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 14% by wt., copper 5.2% to 9% by wt., nickel 1.5% to 4% by wt., iron 0.2% to 1.5% by wt., magnesium 0.2% to 1% by wt., manganese 0.2% to 1.5% by wt., barium up to 4% by wt., titanium up to 0.3% by wt., zirconium up to 0.3% by wt., vanadium up to 0.3% by wt., phosphorus 0.004% to 0.05% by wt., chromium up to 0.2% by wt., and the balance being aluminum and unavoidable impurities.

18. The engine component according to claim 17, wherein the aluminum alloy consists of the alloy elements: silicon 11% to 14% by wt., copper 5.2% to 8% by wt., nickel 1.5% to 4% by wt., iron 0.2% to 1.5% by wt., magnesium 0.2% to 1% by wt., manganese 0.2% to 1.3% by wt., barium up to 1% titanium 0.05% to 0.2% by wt., zirconium 0.05% to 0.2% by wt., vanadium up to 0.2% by wt., phosphorus 0.004% to 0.05% by wt., and the balance being aluminum and unavoidable impurities.

19. The engine component according to claim 7, in the form of a piston composed at least partly of the aluminum alloy.

20. The process according to claim 1, wherein the engine component is a piston for an internal combustion engine.

Description

EXAMPLES

Example 1

(1) silicon 14% to 17% by wt.,

(2) copper 3% to 5% by wt.,

(3) nickel 2% to 4% by wt.,

(4) iron 0.8% to 1.5% by wt.,

(5) magnesium 0.5% to 1% by wt.,

(6) manganese 1% to 2% by wt.,

(7) barium up to 2.5% by wt.,

(8) titanium 0.03% to 0.3% by wt.,

(9) zirconium 0.03% to 0.3% by wt.

(10) vanadium 0.03% to 0.2% by wt.,

(11) phosphorus 0.004% to 0.05% by wt.

(12) chromium up to 0.2% by wt.

Example 2

(13) silicon 9% to 12% by wt.,

(14) copper 3% to 5% by wt.,

(15) nickel 2.5% to 4% by wt.,

(16) iron 0.8% to 2% by wt.,

(17) magnesium 0.4% to 1% by wt.,

(18) manganese 0.8% to 2.3% by wt.,

(19) barium up to 1% by wt.,

(20) titanium 0.03% to 0.3% by wt.,

(21) zirconium 0.03% to 0.3% by wt.

(22) vanadium up to 0.2% by wt.,

(23) phosphorus 0.004% to 0.05% by wt.

(24) chromium up to 0.2% by wt.

Example 3

(25) silicon 11% to 13% by wt.,

(26) copper 5.5% to 8% by wt.,

(27) nickel 2% to 4% by wt.,

(28) iron 0.3% to 1.2% by wt.,

(29) magnesium 0.2% to 1% by wt.,

(30) manganese 0.3% to 1.2% by wt.,

(31) barium up to 1% by wt.,

(32) titanium 0.03% to 0.3% by wt.,

(33) zirconium 0.03% to 0.3% by wt.

(34) vanadium up to 0.2% by wt.,

(35) phosphorus 0.004% to 0.05% by wt.

(36) chromium up to 0.2% by wt.

Example 4

(37) silicon 11% to 13% by wt.,

(38) copper 4% to 7% by wt.,

(39) nickel 1% to 3% by wt.,

(40) iron 0.15% to 1% by wt.,

(41) magnesium 0.2% to 1% by wt.,

(42) manganese ≥0.1% by wt.,

(43) barium up to 1% by wt.,

(44) titanium 0.03% to 0.3% by wt.,

(45) zirconium 0.03% to 0.3% by wt.,

(46) vanadium up to 0.2% by wt.,

(47) phosphorus 0.004% to 0.05% by wt.,

(48) chromium up to 0.2% by wt.,

(49) and, as the balance, aluminum and unavoidable impurities.