Composite braze liner for low temperature brazing and high strength materials
An apparatus, material and method for forming a brazing sheet has a composite braze liner layer of low melting point aluminum alloy and 4000 series braze liner. The low melting point layer of the composite braze liner facilitates low temperature brazing and decrease of the diffusion of magnesium from the core into the composite braze liner. The reduction of magnesium diffusion also lowers the formation of associated magnesium oxides at the braze joint interface that are resistant to removal by Nocolok flux, thereby facilitating the formation of good brazing joints through the use of low temperature controlled atmosphere brazing (CAB) and Nocolok flux. The apparatus also enables the production of brazing sheet materials with high strength and good corrosion property.
1. A brazing sheet, comprising:
a core of a 2XXX, 3XXX, 5XXX or 6XXX aluminum alloy;
a composite braze liner adjacent the core, wherein the composite braze liner comprises:
a 4XXX aluminum alloy layer; and
a first aluminum alloy layer connected to the 4XXX aluminum alloy layer;
wherein the first aluminum alloy layer has a melting point lower than that of the 4XXX aluminum alloy layer; and
wherein the first aluminum alloy comprises 4-12 wt. % Si, 0.1-1.0 wt. % Fe, 1.0-5 wt. % Cu and 5-20 wt. % Zn.
2. The brazing sheet of claim 1 , wherein the 4XXX aluminum alloy layer is disposed on the core, and wherein the first aluminum alloy layer is disposed on the 4XXX aluminum alloy layer.
3. The brazing sheet of claim 1 , wherein the first aluminum alloy layer is disposed on the core, and wherein the 4XXX aluminum alloy layer is disposed on the first aluminum alloy layer.
4. The brazing sheet of claim 1 , comprising a waterside liner.
5. The brazing sheet of claim 4 , wherein the waterside liner comprises 1.0-15 wt. % Zn.
6. The brazing sheet of claim 1 , wherein the first aluminum alloy layer has a solidus temperature of not greater than 560° C.
7. The brazing sheet of claim 1 , wherein the core has a solidus temperature of greater than 590° C., and wherein the core has a liquidus temperature of greater than 650° C.
8. The brazing sheet of claim 7 , wherein the core comprises 0.10-1.2 wt. % Si, 0.15-0.5 wt. % Fe, 0.40-3.5 wt. % Cu, 0.10-1.8 wt. % Mn, 0.20-1.85 wt. % Mg, <0.01 wt. % Cr, <0.20 wt. % Zn and <0.20 wt. % Ti.
9. A method comprising:
providing a first part formed from a brazing sheet, wherein the brazing sheet comprises:
a core of a 2XXX, 3XXX, 5XXX or 6XXX aluminum alloy;
a composite braze liner adjacent the core, wherein the composite braze liner comprises:
a 4XXX aluminum alloy layer; and
a first aluminum alloy layer connected to the 4XXX aluminum alloy layer;
wherein the first aluminum alloy layer has a melting point lower than that of the 4XXX aluminum alloy layer; and
wherein the first aluminum alloy comprises 4-12 wt. % Si, 0.1-1.0 wt. % Fe, 1.0-5 wt. % Cu and 5-20 wt. % Zn;
providing a second part formed from an aluminum alloy;
applying a Nocolok flux to at least one of the first part and the second part to remove oxides from a surface thereof;
placing the first part in contact with the second part;
heating the first part and the second part in a controlled atmosphere;
melting the first aluminum alloy layer before the 4XXX aluminum alloy melts;
melting the 4XXX aluminum alloy layer, thereby forming a mixed molten alloy of the first aluminum alloy and the 4XXX aluminum alloy;
forming a braze joint between the first part and the second part from the mixed molten alloy; and
allowing the mixed molten alloy to cool.