초록 ▼

A three-dimensional, woven metal fiber preform and metal braze matrix forms a high temperature metallic structural joint. The preform is used with a braze alloy matrix to join a structural skin to a flangeless frame. This same basic joint can be used to create large complex structures with very litt

A three-dimensional, woven metal fiber preform and metal braze matrix forms a high temperature metallic structural joint. The preform is used with a braze alloy matrix to join a structural skin to a flangeless frame. This same basic joint can be used to create large complex structures with very little tooling. The three-dimensional woven metal preform is a flexible element that conforms to match the skin and flangeless frame, thereby avoiding high costs associated with precision fixturing. A high temperature braze metal is used as a matrix for the wire and to join the woven preform to the skin and the frame. The edges of the preform are tapered to a feather edge to avoid stress concentrations and stiffness mismatch.

대표청구항 ▼

What is claimed is: 1. A structural joint, comprising: a preform formed from woven, flexible metal fibers to form a three-dimensional shape, the preform having a base and a pair of legs extending from the base to form a channel therebetween; a first component joined to the base of the preform with

What is claimed is: 1. A structural joint, comprising: a preform formed from woven, flexible metal fibers to form a three-dimensional shape, the preform having a base and a pair of legs extending from the base to form a channel therebetween; a first component joined to the base of the preform with a braze; a second component located in the channel of the preform and joined thereto with the braze to complete the structural joint; and wherein both the fibers of the preform and the braze completely diffuse to form a single homogenous material. 2. A structural joint according to claim 1, wherein the first component is a structural skin, the second component is a flangeless frame, the preform conforms to a shape of the structural skin and the flangeless frame, and edges of the preform are tapered to a feather edge. 3. A structural joint according to claim 1, wherein the fibers are formed from a material selected from the group consisting of stainless steel alloys, titanium alloys, and nickel-based alloys; and the fibers have a diameter in a range of approximately a few microns to 0.25 millimeters (0.010 inch). 4. A structural joint according to claim 1, wherein the braze is a braze alloy selected from the group consisting of powder, tape, and foil. 5. A structural joint in a condition for brazing, comprising: a preform formed from woven, flexible metal fibers to form a three-dimensional shape, the preform having a base and a pair of legs extending from the base to form a channel therebetween, the base having an interior side and two exterior side portions, each extending laterally from one of the legs, each of the legs having an interior side within the channel and an exterior side that joins one of the exterior side portions of the base; a first metallic component in abutment with the interior side of the base of the preform; a second metallic component having oppositely facing side surfaces that abut the interior sides of the legs; and brazing material overlying the exterior side portions of the base and the legs and positioned such that elevating the structural joint to a brazing temperature causes the braze material to melt and diffuse into the preform to join the first and second components to each other. 6. The structural joint according to claim 5, wherein the exterior side portions of the base and the exterior sides of the legs of the preform are free of contact with either of the metallic components. 7. The structural joint according to claim 5, wherein the first metallic component is a structural skin, the second metallic component is a frame having an edge that is joined to the structural skin by the preform, the preform conforms to a shape of the structural skin and the frame, and the exterior side portions of the preform are tapered to a feather edge. 8. The structural joint according to claim 5, wherein the fibers are formed from a material selected from the group consisting of stainless steel alloys, titanium alloys, and nickel-based alloys; and the fibers have a diameter in a range of approximately a few microns to 0.25 millimeters (0.010 inch). 9. The structural joint according to claim 5, wherein the brazing material is a braze alloy selected from the group consisting of powder, tape, and foil. 10. The structural joint according to claim 5, wherein the fibers of the preform and the brazing material remain substantially separate and distinct materials in the structural joint after being heated to the brazing temperature. 11. The structural joint according to claim 5, wherein both the fibers of the preform and the brazing material completely diffuse after being heated to the brazing temperature to form a single homogenous material. 12. The structural joint of claim 5, wherein: the brazing material comprises at least one tape overlying one of the exterior side portions of the base and the exterior side of one of the legs, and another tape overlying the other of the exterior side portions of the base and the exterior side of the other of the legs. 13. The structural joint of claim 5, wherein: the brazing material comprises a first tape overlying one of the exterior side portions of the base; a second tape overlying the exterior side of one of the legs; a third tape overlying the other of the exterior side portions of the base; and a fourth tape overlying the exterior side of the other of the legs.