NICKEL-BASED BRAZING FOIL, METHOD FOR PRODUCING A BRAZING FOIL, OBJECT WITH A BRAZING SEAM AND BRAZING METHOD
An amorphous ductile brazing foil is provided. The brazing foil has a composition consisting substantially of Ni Bal Cr a B b ,P c Si d Mo e X f Y g , with 21 atomic %≤a≤28 atomic %; 0.5 atomic %≤b≤7 atomic %; 4 atomic %≤c≤12 atomic %; 2 atomic %≤d≤10 atomic %; 0 atomic %<e≤5 atomic %; 0 atomic %≤f≤5 atomic %; 0 atomic %≤g≤20 atomic %; incidental impurities≤1.0 atomic %; balance Ni, wherein X is one or more of the elements Nb, Ta, W, Cu, C or Mn and Y is one or both of the elements Fe and Co and a/c≥2.
1 . An amorphous, ductile Ni-based brazing foil having a composition consisting essentially of
Ni Bal Cr a B b ,P c Si d Mo e X f Y g , wherein 21 atomic %≤a≤28 atomic %; 0.5 atomic %≤b≤7 atomic %; 4 atomic %≤c≤12 atomic %; 2 atomic %≤d≤10 atomic %; 0 atomic %<e≤5 atomic %; 0 atomic %≤f≤5 atomic %; 0 atomic %≤g≤20 atomic %; incidental impurities≤1.0% by weight; balance Ni, wherein X is one or more of the elements Nb, Ta, W, Cu, C or Mn and Y is one or both of the elements Fe and Co, and wherein a/c≥2.
2 . The amorphous, ductile brazing foil according to claim 1 , wherein the content of Cr is such that 22 atomic %≤a≤28 atomic %.
3 . The amorphous, ductile brazing foil according to claim 2 , wherein the content of Cr is such that 23 atomic %≤a≤27 atomic %.
4 . The amorphous, ductile brazing foil according to claim 1 , wherein c>b>c/15 and 14 atomic %≤(b+c+d)≤20 atomic %.
5 . The amorphous, ductile brazing foil according to claim 1 , wherein 0 atomic %≤f≤3 atomic %; 0 atomic %≤g≤15 atomic %.
6 . The amorphous, ductile brazing foil according to claim 1 , wherein 14 atomic %≤(b+c+d)≤18 atomic %.
7 . The amorphous, ductile brazing foil according to claim 1 , wherein the content of B is such that 1.5 atomic %≤b≤5.0 atomic %.
8 . The amorphous, ductile brazing foil according to claim 1 , wherein the content of P is such that 9 atomic %≤c≤11 atomic %.
9 . The amorphous, ductile brazing foil according to claim 1 , wherein the content of Si is such that 2.5 atomic %≤d≤4.5 atomic %.
10 . The amorphous, ductile brazing foil according to claim 1 , wherein the brazing foil is at least 80% amorphous.
11 . The amorphous, ductile brazing foil according to claim 1 , comprising an average thickness D of 15 μm≤D≤60 μm.
12 . The amorphous, ductile brazing foil according to claim 1 , comprising a width B of 0.5 mm≤B≤300 mm.
13 . The amorphous, ductile brazing foil according to claim 12 , wherein the width B is such that 30 mm≤B≤150 mm.
14 . The amorphous, ductile brazing foil according to claim 1 , comprising a thickness fluctuation relative to an average thickness of less than 25% over a length of 200 m and/or a thickness fluctuation relative to an average thickness of less than 20% over a length of 100 m and/or a thickness fluctuation relative to an average thickness of less than 20% over a length of 5000 m.
15 . The amorphous, ductile brazing foil according to claim 1 , comprising a thickness fluctuation relative to an average thickness of less than 15 μm over a length of 100 m.
16 . The amorphous, ductile brazing foil according to claim 1 , comprising a liquidus temperature between 980° C. and 1100° C.
17 . An object comprising a first component and a second component, wherein the first component is permanently joined to the second component by means of a brazing seam produced with an amorphous, ductile brazing foil according to claim 1 .
18 . A method for joining two or more components by adhesive force, the method comprising: introducing a brazing foil according to claim 1 between two or more components to be joined, the components to be joined having a higher melting temperature than the brazing foil, heating the brazing composite to a brazing temperature above the liquidus temperature of the brazing alloy, cooling the brazing composite accompanied by the forming of a brazed joint between the components to be joined.
19 . The method according to claim 18 , wherein the brazing composite is heated to a brazing temperature between 1050° C. and 1200° C.
20 . The method according to claim 18 , wherein the components to be joined are parts of a heat exchanger or of an exhaust gas recirculation cooler or components thereof.
21 . The method according to claim 18 , wherein the heating of the brazing composite to a brazing temperature above the liquidus temperature of the brazing foil is carried out in a protective gas atmosphere.
22 . The method according to claim 18 , wherein the heating of the brazing composite to a brazing temperature above the liquidus temperature of the brazing foil is carried out in a continuous furnace.
23 . A method of brazing two or more components of a heat exchanger or of an exhaust gas recirculation cooler comprising introducing a brazing foil according to claim 1 .
24 . A method for brazing two or more components made of an austenitic stainless steel or an Ni alloy or a Co alloy comprising introducing a brazing foil according to claim 1 .