Abstract: A metal/composite joint. An illustrative embodiment of the metal/composite joint includes a metallic component, a composite component provided in engagement with the metallic component, an engagement region defining contact between the metallic component and the composite component and a plurality of attachment projections joining the metallic component and the composite component. The attachment projections may be non-uniformly distributed along the engagement region. A method of joining a metallic component and a composite component is also included.

Abstract: A torque tube includes a composite body and an end fitting. The composite tube includes a body having a body interior diameter, a wall thickness, an end having an edge, and a set of helically-shaped grooves. Each helically-shaped groove may pass through the wall thickness. Each helically-shaped groove may begin at the edge and end in the body. The end fitting may include a sleeve configured to mate with the body interior diameter and a set of ribs configured to mate with the set of helically-shaped groove.

Abstract: A torque tube includes a composite body and an end fitting. The composite tube includes a body having a body interior diameter, a wall thickness, an end having an edge, and a set of helically-shaped grooves. Each helically-shaped groove may pass through the wall thickness. Each helically-shaped groove may begin at the edge and end in the body. The end fitting may include a sleeve configured to mate with the body interior diameter and a set of ribs configured to mate with the set of helically-shaped groove.

Abstract: A torque tube includes a composite body and an end fitting. The composite tube includes a body having a body interior diameter, wall thickness, an end having an edge, and a set of grooves. Each groove of the set of grooves passes through the wall thickness. Each groove of the set of grooves begins at the edge and ends in the body. The end fitting includes a sleeve configured to mate with the body interior diameter and a set of ribs configured to mate with the set of grooves.

Abstract: A joint is formed by joining two structures using a joint element. The joint element has a base and at least two legs extending from the base, the legs defining a slot having opposing sides and a bottom. The joint element is attached to the first structure. A second structure is positioned in the slot. An adhesive is disposed in the slot joining the second structure to the joint element. A cavity is formed between the bottom of the slot and the second structure. The cavity being substantially free of adhesive.

Abstract: A joint is formed by joining two structures using a joint element. The joint element has a base and at least two legs extending from the base, the legs defining a slot having opposing sides and a bottom. The joint element is attached to the first structure. A second structure is positioned in the slot. An adhesive is disposed in the slot joining the second structure to the joint element. A cavity is formed between the bottom of the slot and the second structure. The cavity being substantially free of adhesive.

Abstract: A metal/composite joint. An illustrative embodiment of the metal/composite joint includes a metallic component, a composite component provided in engagement with the metallic component, an engagement region defining contact between the metallic component and the composite component and a plurality of attachment projections joining the metallic component and the composite component. The attachment projections may be non-uniformly distributed along the engagement region. A method of joining a metallic component and a composite component is also disclosed.

Abstract: A product including a first structure. A joint element is attached to the first structure. The joint element has a base and at least two legs extending from the base, the legs defining a slot having opposing sides and a bottom. A second structure is positioned in the slot. An adhesive is disposed in the slot joining the second structure to the joint element. A cavity is formed between the bottom of the slot and the second structure. The cavity being substantially free of adhesive.

Abstract: A torque tube includes a composite body and an end fitting. The composite tube includes a body having a body interior diameter, wall thickness, an end having an edge, and a set of grooves. Each groove of the set of grooves passes through the wall thickness. Each groove of the set of grooves begins at the edge and ends in the body. The end fitting includes a sleeve configured to mate with the body interior diameter and a set of ribs configured to mate with the set of grooves.

Abstract: A product including a first structure. A joint element is attached to the first structure. The joint element has a base and at least two legs extending from the base, the legs defining a slot having opposing sides and a bottom. A second structure is positioned in the slot. An adhesive is disposed in the slot joining the second structure to the joint element. A cavity is formed between the bottom of the slot and the second structure. The cavity being substantially free of adhesive.

Abstract: A method of joining a first structure to a second structure using a joint element. The joint element has a base and at least two legs extending from the base and the legs define a slot having opposing sides and a bottom. The method comprises attaching the joint element to the first structure and inserting the second structure into the slot. The method further includes injecting an adhesive into the slot. The method also includes ensuring a cavity is formed between the bottom of the slot and the second structure and the cavity is substantially free of adhesive.

Abstract: A method of joining a first structure to a second structure using a joint element. The joint element has a base and at least two legs extending from the base and the legs define a slot having opposing sides and a bottom. The method comprises attaching the joint element to the first structure and inserting the second structure into the slot. The method further includes injecting an adhesive into the slot. The method also includes ensuring a cavity is formed between the bottom of the slot and the second structure and the cavity is substantially free of adhesive.

Abstract: A method for vacuum assisted resin transfer molding a composite structure including fibers at least partially surrounded by resin using a mold including a tool having a surface shaped to correspond to the composite structure and an inflatable bladder for forcing the composite structure against the tool. A resin inlet is connected to a resin source for introducing resin into a mold cavity at least partially defined by the tool surface and the bladder and a vacuum port spaced from the resin inlet. The method includes the steps of opening the mold cavity, loading fibers into the open mold cavity, closing the loaded mold cavity, introducing resin through the resin inlet into the closed mold cavity loaded with fibers, and pulling a vacuum at the resin inlet and the vacuum port to draw excess resin from the structure prior to curing thereof.

Abstract: A three dimensional textile joint reinforcement joins and reinforces a composite panel and a support structure. The composite panel includes lamina of textile fibers in the plane of the panel. The joint reinforcement is attached to the composite panel by staples. The support structure, which is typically perpendicular to the plane of the composite panel, is also attached to the joint reinforcement. Out of plane forces act upon the assembled structure and the joint reinforcement transfers out of plane loads between the support structure and the composite panel. The staples provide transfer of load to the plane of the textile fibers in the composite panel, where the composite panel is strongest.

Abstract: A three dimensional textile joint reinforcement joins and reinforces a composite panel and a support structure. The composite panel includes lamina of textile fibers in the plane of the panel. The joint reinforcement is attached to the composite panel by staples. The support structure, which is typically perpendicular to the plane of the composite panel, is also attached to the joint reinforcement. Out of plane forces act upon the assembled structure and the joint reinforcement transfers out of plane loads between the support structure and the composite panel. The staples provide transfer of load to the plane of the textile fibers in the composite panel, where the composite panel is strongest.