EUTECTIC BRAZING COMPOSITIONS, AND RELATED PROCESSES AND DEVICES
An active braze alloy composition is described, including nickel; or a combination of nickel and cobalt; about 2% by weight to about 30% by weight germanium; and about 1% by weight to about 5% by weight boron and about 0.5% by weight to about 5% by weight of at least active element. The composition is free of silicon. Braze alloy joints formed of the braze alloy composition, and located in various devices, structures, and machines, are also described. A related method for repairing a crack or other cavity within a metal component, using the braze composition, is further described.
1 . A braze alloy composition, comprising:
nickel, or a combination of nickel and cobalt;
about 2% by weight to about 30% by weight germanium; and
about 1% by weight to about 5% by weight boron;
wherein the composition is free of silicon.
2 . The braze alloy composition of claim 1 , wherein the level of germanium is about 5% by weight to about 25% by weight.
3 . The braze alloy composition of claim 1 , wherein the level of boron is about 1.5% by weight to about 3.5% by weight.
4 . The composition of claim 1 , comprising at least about 20% by weight nickel.
5 . The composition of claim 4 , comprising about 60% to about 90% by weight nickel.
6 . The braze alloy composition of claim 1 , comprising about 0.5% to about 5% (total) of at least one active metal element, based on the total weight of the composition.
7 . The braze alloy composition of claim 1 , further comprising about 1% by weight to about 25% by weight chromium.
8 . The braze alloy composition of claim 7 , wherein the level of chromium is about 5% by weight to about 17% by weight.
9 . The braze alloy composition of claim 1 , further comprising at least one refractory element selected from molybdenum, tungsten, tantalum, and niobium.
10 . The braze alloy composition of claim 9 , containing about 1% by weight to about 10% by weight (total) of the refractory element.
11 . The braze alloy composition of claim 1 , substantially free of copper, manganese, silver, gold, platinum, palladium, gallium, tin, and lead.
12 . A braze joint formed of the composition of claim 1 , wherein the braze joint material has a microstructure that comprises
a full, single gamma nickel-phase, with at least germanium in solution, up to about 12% by weight;
a two-phase microstructure comprising gamma nickel and gamma prime (gamma′) Ni 3 Ge, wherein the Ni 3 Ge component is a precipitate present at levels between about 1% by volume and 75% by volume; and
metal boride phases of nickel, chromium, and at least one refractory element, wherein the metal boride phases comprise about 1% to 35% of the volume fraction of the braze joint material.
13 . A braze joint formed of the composition of claim 1 , joining a ceramic component and a metal component.
14 . The braze joint of claim 13 , wherein the ceramic component comprises zirconia or a zirconia-based material; alumina; aluminum nitride, silicon carbide, porcelain, titanium carbide, silica, glass, ceramic matrix composite (CMC), magnesium aluminate spinel, magnesium oxide, silicon nitride; an “MAX” phase material of the formula M n+1 AX n , where n is 1-3, M is an early transition metal, A is a Group A element, and X is carbon or nitrogen; an ultra-high temperature ceramic (UHTC) of the formula MX y , wherein M is a transition metal; and X is carbon, boron, or nitrogen; and alloys of any of the foregoing.
15 . The braze joint of claim 13 , wherein the metal comprises nickel, cobalt, niobium, molybdenum, tungsten, iron, nickel-cobalt ferrous alloys, mild steel, stainless steel, and alloys of any of the foregoing.
16 . The braze joint of claim 13 , wherein the ceramic and metal components are structures joined together in a medical device.
17 . The braze joint of claim 13 , wherein the ceramic and metal components are structures joined together in a turbine engine.
18 . The braze joint of claim 13 , wherein the ceramic and metal components each comprise at least one thermal battery structure selected from the group consisting of electrode compartments; sealing collar structures, sealing ring structures, and electrical current collectors.
19 . A method for repairing a crack or other cavity within a metal component, wherein the crack or cavity includes surfaces that contain oxide material, comprising the step of filling or partially filling the crack or cavity with a braze composition in its liquidus state, and then letting the braze material solidify, thereby sealing the crack or cavity, in part by bonding the metallic material of the component with the oxide material on the crack- or cavity-surfaces,
wherein the braze alloy composition comprises:
nickel or a combination of nickel and cobalt;
about 2% by weight to about 30% by weight germanium;
about 1% by weight to about 5% by weight boron; and
about 0.51% by weight to about 5% by weight of at least one active metal element;
wherein the braze composition is free of silicon.
20 . The method of claim 19 , wherein the metal component is a gas turbine engine blade.