Corrosion resistant high strength brazing sheet
An apparatus, material and method for forming a brazing sheet has a high strength core bonded with corrosion protection layer on the coolant side and/or layers on both airside and coolant side. The material enables heat exchanger components, such as tube, header, plate, etc., for applications, such as automotive heat exchangers, that require high fatigue life as well as high service life in a corrosive environment.
1. A sheet material comprising:
an aluminum alloy core consisting of 0.1 to 1.2 wt % Si, up to 0.6 wt % Fe, 1.53 to 2.6 wt % Cu, 0.5 to 1.8 wt % Mn, up to 0.6 wt % Mg, 0.05 to 1.0 wt % Zn, up to 0.2 wt % Ti, up to 0.2 wt % Zr, Al, and impurities;
a 4XXX aluminum alloy braze liner comprising 6 to 13 wt % Si, up to 0.8 wt % Fe, up to 0.3 wt % Cu, up to 0.2 wt % Mn, up to 2.0 wt % Mg, and up to 4.0 wt % Zn; and
a waterside liner comprising 0.1 to 1.2 wt % Si, up to 1.0 wt % Fe, up to 0.3 wt % Cu, up to 1.5 wt % Mn, up to 0.6 wt % Mg, 0.5 to 12 wt % Zn, up to 0.16 wt % Ti, and up to 0.16 wt % Zr.
2. The sheet material of claim 1 , wherein the Zn of the core forms second phase particles which alter a corrosion potential difference between a matrix of the core and the second phase particles.
3. The sheet material of claim 2 , wherein the Zn of the core forms at least one of Cu 5 Zn 2 Al, Cu 3 ZnAl 3 or another Al—Cu—Zn/Al—Cu—Mg—Zn phase.
4. The sheet material of claim 2 , wherein the core consists of 0.1 to 1.0 wt % Si, up to 0.6 wt % Fe, 1.53 to 2.4 wt % Cu, 0.5 to 1.7 wt % Mn, up to 0.6 wt % Mg, 0.05 to 1.0 wt % Zn, up to 0.2 wt % Ti, up to 0.2 wt % Zr, Al, and impurities.
5. The sheet material of claim 2 , wherein the core consists of 0.1 to 0.8 wt % Si, up to 0.6 wt % Fe, 1.53 to 2.3 wt % Cu, 0.5 to 1.5 wt % Mn, up to 0.4 wt % Mg, 0.05 to 0.8 wt % Zn, up to 0.18 wt % Ti, up to 0.18 wt % Zr, Al, and impurities.
6. The sheet material of claim 1
wherein the core consists of 0.1 to 0.8 wt % Si, up to 0.6 wt % Fe, 1.53 to 2.3 wt % Cu, 0.5 to 1.5 wt % Mn, up to 0.4 wt % Mg, 0.1 to 0.8 wt % Zn, up to 0.18 wt % Ti, up to 0.18 wt % Zr, Al, and impurities.
7. The sheet material of claim 1 , wherein the waterside liner comprises 0.1 to 1.2 wt % Si, up to 1.0 wt % Fe, up to 0.2 wt % Cu, up to 1.5 wt % Mn, up to 0.6 wt % Mg, 0.5 to 12 wt % Zn, up to 0.16 wt Ti, and up to 0.16 wt % Zr; and
wherein the core consists of 0.1 to 0.8 wt % Si, up to 0.5 wt % Fe, 1.53 to 2.3 wt % Cu, 0.5 to 1.5 wt % Mn, up to 0.35 wt % Mg, 0.05 to 0.8 wt % Zn, up to 0.2 wt % Ti, up to 0.2 wt % Zr, Al, and impurities.
8. The sheet material of claim 1 , wherein the waterside liner comprises 0.1 to 1.2 wt % Si, up to 0.8 wt % Fe, up to 0.1 wt % Cu, up to 1.3 wt % Mn, up to 0.5 wt % Mg, 0.5 to 10 wt % Zn, up to 0.1 wt % Ti, and up to 0.1 wt % Zr; and
wherein the core consists of 0.1 to 0.8 wt % Si, up to 0.5 wt % Fe, 1.53 to 2.3 wt % Cu; 0.5 to 1.4 wt % Mn, up to 0.3 wt % Mg, 0.05 to 0.8 wt % Zn, up to 0.18 wt Ti, up to 0.18 wt % Zr, Al, and impurities.
9. The sheet material of claim 1 , further comprising an interliner positioned between the core and the braze liner.
10. The sheet material of claim 9 , wherein the interliner comprises up to 0.3 wt % Si, up to 0.5 wt % Fe, 0.1 to 1.0 wt % Cu, 0.5 to 1.8 wt % Mn, up to 0.3 wt % Mg, up to 0.25 wt % Zn, up to 0.25 wt % Ti, and up to 0.25 wt % Zr;
wherein the waterside liner comprises 0.1 to 1.2 wt % Si, up to 1.0 wt % Fe, up to 0.2 wt % Cu, up to 1.5 wt % Mn, up to 0.6 wt % Mg, 0.5 to 12 wt % Zn, up to 0.16 wt % Ti, and up to 0.16 wt % Zr; and
wherein the core consists of 0.1 to 1.0 wt % Si, up to 1.0 wt % Fe, 1.53 to 2.5 wt % Cu, 0.5 to 1.8 wt % Mn, up to 0.6 wt % Mg, 0.05 to 1.0 wt % Zn, up to 0.2 wt % Ti, up to 0.2 wt % Zr, Al, and impurities.
11. The sheet material of claim 9 , wherein the interliner comprises up to 0.2 wt % Si, up to 0.5 wt % Fe, 0.3 to 0.9 wt % Cu, 0.5 to 1.8 wt % Mn, up to 0.35 wt % Mg, up to 0.2 wt % Zn, up to 0.18 wt % Ti, and up to 0.18 wt % Zr;
wherein the waterside liner comprises 0.1 to 1.0 wt % Si, up to 1.0 wt % Fe, up to 0.2 wt % Cu, up to 1.2 wt % Mn, up to 0.5 wt % Mg, 0.5 to 10 wt % Zn, up to 0.1 wt % Ti, and up to 0.1 wt % Zr; and
wherein the core consists of 0.1 to 0.8 wt % Si, up to 0.5 wt % Fe, 1.53 to 2.5 wt % Cu, 0.5 to 1.6 wt % Mn, up to 0.3 wt % Mg, 0.05 to 0.8 wt % Zn, up to 0.18 wt % Ti, up to 0.18 wt % Zr, Al, and impurities.
12. The sheet material of claim 9 , wherein the interliner comprises up to 0.15 wt % Si, up to 0.4 wt % Fe, 0.2 to 0.9 wt % Cu, 0.5 to 1.7 wt % Mn, up to 0.3 wt % Mg, up to 0.15 wt % Zn, up to 0.16 wt % Ti, and 0.1 to 0.16 wt % Zr;
wherein the waterside liner comprises 0.1 to 1.0 wt % Si, up to 0.9 wt % Fe, up to 0.2 wt % Cu, up to 1.4 wt % Mn, up to 0.5 wt % Mg, 0.5 to 8 wt % Zn, up to 0.1 wt % Ti, and up to 0.1 wt Zr; and
wherein the core consists of 0.1 to 0.8 wt % Si, up to 0.5 wt % Fe, 1.53 to 2.3 wt % Cu, 0.5 to 1.5 wt % Mn, up to 0.3 wt % Mg, 0.05 to 0.8 wt % Zn, up to 0.18 wt % Ti, up to 0.18 wt % Zr, Al, and impurities.
13. A heat exchanger comprising:
at least one tube capable of conducting a fluid therethrough and at least one fin in heat conductive contact with the tube, the tube comprising the sheet material of claim 1 ;
wherein the fin comprising an aluminum alloy with a Zn addition; and
wherein the Zn of the core reduces the corrosion potential difference between the tube and the fin.
14. The heat exchanger of claim 13 , wherein the fin comprises a 3003+Zn/3003mod aluminum alloy comprising ≥0.5 wt % Zn addition.
15. A method for making the sheet material of claim 10 , the method comprising:
casting ingots for the interliner, the waterside liner, the core, and the braze liner;
subjecting the ingots for the interliner, the waterside liner, the core, and the braze liner to a preheat at a temperature in a range of 400-560° C. for a soak time of up to 6 hours;
rolling the ingots for the interliner, the waterside liner, the core, and the braze liner to form stackable laminae;
stacking the laminae into a composite; and
rolling the composite to form the sheet material.
16. The method of claim 15 , wherein the rolling the composite is conducted at a temperature in a range of 400-520° C.
17. The method of claim 15 , wherein the rolling the composite is conducted at room temperature.
18. The method of claim 15 , wherein the rolling the composite is conducted by cold rolling to an intermediate gauge followed by an intermediate anneal at a temperature in a range of 340-420° C. one or more times, followed by cold rolling to a final gauge.
19. The method of claim 15 , wherein the rolling the composite is conducted by cold rolling directly to a final gauge and then subjecting to a final anneal at a temperature in a range of 150-420° C.