The present invention relates to methods for repairing a structural weakness in an aircraft fuselage, or preventing the advancement of a structural weakness in an aircraft fuselage. Cold spray methods such as supersonic particle deposition have been shown to positively affect structural characteristics of sheet metal and lap joints as used in fuselage construction.

The present invention relates to methods for repairing a structural weakness in an aircraft fuselage, or preventing the advancement of a structural weakness in an aircraft fuselage. Cold spray methods such as supersonic particle deposition have been shown to positively affect structural characteristics of sheet metal and lap joints as used in fuselage construction.

A bearing cable structure while fabricating panel comprises a steel cable and two sets of fixing members. Each connection section of the steel cable is assembled to the corresponding antiskid ring and then assembled into the axial blind hole of each fixing member and further riveted to the screwing section of each fixing member by machine so that the fixing members are tightly connected to the outer layer of the steel cable and the steel cable and the fixing members are integrated with each other for preventing from falling off, and simultaneously the riveting of the axial blind hole may engage with the outer layer to perform double location so as to strengthen an axial pull strength of the bearing cable structure and increase service life.

A joined structure includes a first component, a second component, and an insert. The first component is formed of a fiber-reinforced material and has a hole defining an axis. The second component is adjacent the first component and has a hole aligned with the hole of the first component. The insert is positioned in the hole of the first component. The insert includes an inner layer having a tubular shape about the axis, a middle layer concentrically adjacent to the inner layer about the axis, and an outer layer concentrically adjacent to the middle layer about the axis. The layers are formed of fiber-reinforced materials. One of a boundary between the inner and middle layers and a boundary between the middle and outer layers has a nonlinear profile in a direction parallel to the axis.

A joined structure includes a first component, a second component, and an insert. The first component is formed of a fiber-reinforced material and has a hole defining an axis. The second component is adjacent the first component and has a hole aligned with the hole of the first component. The insert is positioned in the hole of the first component. The insert includes an inner layer having a tubular shape about the axis, a middle layer concentrically adjacent to the inner layer about the axis, and an outer layer concentrically adjacent to the middle layer about the axis. The layers are formed of fiber-reinforced materials. One of a boundary between the inner and middle layers and a boundary between the middle and outer layers has a nonlinear profile in a direction parallel to the axis.

A mechanical coupling assembly that includes a primary substrate having at least one aperture formed therein. A secondary substrate includes at least one mechanical interlock monolithically formed with the secondary substrate. The at least one mechanical interlock extends through the aperture. The mechanical interlock includes a main body and a head portion with a transition portion connecting the main body and head portions. The main body includes a bore formed longitudinally therein about a centerline of the aperture. The mechanical interlock joins the primary substrate and secondary substrate mechanically.

A mechanical coupling assembly that includes a primary substrate having at least one aperture formed therein. A secondary substrate includes at least one mechanical interlock monolithically formed with the secondary substrate. The at least one mechanical interlock extends through the aperture. The mechanical interlock includes a main body and a head portion with a transition portion connecting the main body and head portions. The main body includes a bore formed longitudinally therein about a centerline of the aperture. The mechanical interlock joins the primary substrate and secondary substrate mechanically.

A fastener for use in joining workpieces, for example automotive body parts such as a roof to a body frame member, is provided that includes a plastically deformable head portion, a platform disposed at a bottom of the head portion, and a distal end portion extending from the platform and defining at least one of elastically deformable locking member. The head portion is heat staked to one workpiece, and the elastically deformable locking member engages another workpiece to secure the workpieces together. The platform provides spacing, or a bond gap in one form, between the workpieces, and a material and geometry of the fastener are configured to compensate for a difference in thermal expansion of the workpieces.

A fastener for use in joining workpieces, for example automotive body parts such as a roof to a body frame member, is provided that includes a plastically deformable head portion, a platform disposed at a bottom of the head portion, and a distal end portion extending from the platform and defining at least one of elastically deformable locking member. The head portion is heat staked to one workpiece, and the elastically deformable locking member engages another workpiece to secure the workpieces together. The platform provides spacing, or a bond gap in one form, between the workpieces, and a material and geometry of the fastener are configured to compensate for a difference in thermal expansion of the workpieces.

Various embodiments relate to a method for closely connecting an organic optoelectronic component to a connection piece, including forming a first cavity in the organic optoelectronic component, wherein the first cavity has at least a first opening, introducing a connecting structure through the first opening into the first cavity, wherein the connecting structure has a first fixing area, wherein the first fixing area is configured partially complementarily to the form of the first cavity, forming a second cavity in a connection piece, wherein the second cavity has at least a second opening, wherein the second cavity is configured partially complementarily to the form of the second fixing area, and introducing a second fixing area through the second opening into the second cavity, and forming a friction-fitting connection of the organic optoelectronic component with the connecting piece once the connecting structure has been introduced into the first and the second cavity.