Braze joints
A method of manufacturing includes depositing a first braze material to a first joint location between a first component having a first coefficient of thermal expansion and an intermediate component. The first component is fitted to the intermediate component at room temperature at the first joint location. A second braze material is deposited to a second joint location between the intermediate component and a second component having a second coefficient of thermal expansion. The second component is fitted to the intermediate component at room temperature at the second joint location. The intermediate component has a coefficient of thermal expansion between the first coefficient of thermal expansion and the second coefficient of thermal expansion.
1. A method of manufacturing an assembly for a turbine engine, comprising:
depositing a first braze material to a first joint location between a first component having a first coefficient of thermal expansion and an intermediate component;
fitting the first component to the intermediate component at room temperature at the first joint location;
depositing a second braze material to a second joint location between the intermediate component and a second component having a second coefficient of thermal expansion, wherein a melting temperature of the second braze material is equal to a melting temperature of the first braze material; and
fitting the second component to the intermediate component at room temperature at the second joint location,
wherein the intermediate component has a coefficient of thermal expansion between the first coefficient of thermal expansion and the second coefficient of thermal expansion,
wherein the first component and the second components are parts for the turbine engine, wherein the first component is a fitting and the second component is a housing, and
wherein the intermediate component is a sleeve formed from alloy 625, wherein alloy 625 includes a nickel-chromium-molybdenum superalloy comprising at least 58 wt % nickel, 20-23 wt % chromium, 8-10 wt % molybdenum, 3.15-4.15 wt % niobium, up to 5 wt % iron, and up to 1 wt % cobalt, up to 0.5 wt % manganese, up to 0.5 wt % silicon, up to 0.4 wt % aluminum, up to 0.4 wt % titanium, and rest as unavoidable impurities.
2. The method of claim 1 , further comprising heating the first, second and intermediate components to melt the first and second braze materials to form first and second braze joints.
3. The method of claim 1 , wherein at least one of the first braze material and the second braze material includes at least one material chosen from the group consisting of nickel based alloys containing boron, chromium, iron, nickel, cobalt, silicon, carbon and/or phosphorous, precious metal alloys containing gold, palladium, silver, nickel, copper, tin, and/or zinc, and copper based alloys containing copper, manganese, nickel, zinc, cobalt, and/or silicon.