MECHANICAL FLOW JOINING OF HIGH MELTING TEMPERATURE MATERIALS
A system and method for securely joining a high melting temperature material and a backing substrate using a mechanical connection includes a backing substrate integrally formed with a material positioned inside a dovetail recess in the high melting temperature material, mechanically fixing the backing substrate to the high melting temperature material without fusion or bonding of the microstructure.
1 . A friction stir joined assembly, the assembly comprising:
a non-weldable work piece having an outer surface and an opposite attaching surface;
at least one dovetailed recess disposed in the attaching surface;
an insert disposed in the dovetailed recess; and
a weldable work piece disposed against the attaching surface and friction stir welded to the insert, the insert forming an interference fit inside the at least one dovetailed recess after friction stir welding.
2 . The friction-stir joined assembly as defined in claim 1 wherein the non-weldable work piece is selected from the group of materials consisting of tungsten carbide, alumina, silicon carbide, silicon nitride, polycrystalline diamond, polycrystalline cubic boron nitride, thermally stable polycrystalline diamond, synthetic sapphire, and aluminum oxynitride.
3 . The friction-stir joined assembly as defined in claim 1 wherein the at least one dovetailed recess is comprised of a plurality of dovetailed grooves that are linear.
4 . The friction-stir joined assembly as defined in claim 1 wherein the at least one dovetailed recess is comprised of a plurality of dovetailed recesses formed with an opening in the form of an ellipse.
5 . The friction-stir joined assembly as defined in claim 1 wherein the weldable work piece is selected from a group of materials consisting of steel, stainless steel, aluminum, and high nickel alloys such as Inconel.
6 . The friction-stir joined assembly as defined in claim 1 wherein the at least one dovetailed recess is further comprised of at least one dimple formed therein.
7 . The friction-stir joined assembly as defined in claim 1 wherein the at least one dovetailed recess is further comprised of at least one notch that extends into the non-weldable work piece.
8 . The friction-stir joined assembly as defined in claim 1 wherein the non-weldable work piece is cylindrical, wherein the weldable work piece is configured to be connected to an outer surface of the cylindrical non-weldable work piece.
9 . A friction-stir joined assembly comprising:
a non-weldable work piece having a outer surface and an opposite attaching surface;
at least one dovetailed recess disposed in the attaching surface; and
a weldable work piece disposed against the attaching surface and extruded into the at least one dovetailed recess by friction stir welding, an extrusion from the weldable work piece forming an interference fit inside the at least one dovetailed recess.
10 . The friction-stir joined assembly as defined in claim 9 wherein the attachment device is selected from the group of attachment devices consisting of threaded screws and rods with cotter pins.
11 . The friction-stir joined assembly as defined in claim 9 wherein the at least one dovetailed recess is comprised of a plurality of dovetailed grooves that are linear, and wherein at least one of the plurality of dovetailed grooves crosses at least another one of the plurality of dovetailed grooves.
12 . A method of manufacturing a friction-stir joined assembly, said method comprising:
forming a non-weldable work piece into a desired shape, selecting a outer surface and an opposite attaching surface;
forming a plurality of dovetailed recesses in the attaching surface;
disposing an insert into each of the plurality of dovetailed recesses; and
disposing a weldable work piece against the attaching surface and friction stir welding the weldable work piece to each of the inserts, the inserts forming an interference fit inside the plurality of dovetailed recesses after friction stir welding.
13 . The method as defined in claim 12 wherein the method further comprises selecting the non-weldable work piece from the group of high melting temperature materials consisting of tungsten carbide, aluminum oxide, silicon carbide, silicon nitride, polycrystalline diamond, polycrystalline cubic boron nitride, thermally stable polycrystalline diamond, synthetic sapphire, and aluminum oxynitride.
14 . The method as defined in claim 12 wherein the method further comprises forming the plurality of dovetailed recesses as a plurality of dovetailed grooves that are linear and parallel.
15 . The method as defined in claim 12 wherein the method further comprises forming the plurality of dovetailed recesses as a plurality of dovetailed grooves that are linear and wherein at least one of the plurality of dovetailed grooves crosses at least another one of the plurality of dovetailed grooves.
16 . The method as defined in claim 12 wherein the method further comprises forming the plurality of dovetailed recesses with an opening in the form of an ellipse.
17 . The method as defined in claim 12 wherein the method further comprises selecting the weldable work piece from a group of materials consisting of steel, stainless steel, aluminum, and high nickel alloys such as Inconel.
18 . The method as defined in claim 12 wherein the method further comprises selecting the attachment device from the group of attachment devices consisting of threaded screws and rods with cotter pins.
19 . The method as defined in claim 12 wherein the method further comprises forming the non-weldable work piece and the weldable work piece as arcuate objects.
20 . The method as defined in claim 12 wherein the method further comprises mechanically coupling the weldable work piece to another device in order to provide an outer surface.