A method of forming a monolithic aircraft structure having multiple aerodynamic surfaces includes forming a body component to have a body skin defining a body skin outer surface, and a body side wall integrally formed with the body skin and defining a body mating surface, the body skin outer surface providing a first aerodynamic surface. A cover component is formed to have a cover mating surface and a cover outer surface opposite the cover mating surface, the cover outer surface defining a second aerodynamic surface. The body component is positioned relative to the cover component so that the body mating surface engages the cover mating surface. At least portions of the cover mating surface are friction stir welded to the body mating surface to form friction stir welded joints between the body component and the cover component.

A stable bonding processing for metal, of which at least a part is plated, is provided. A plated metal bonding apparatus performs bonding of a first metal and a second metal. At least one from among the first metal and the second metal has a plated bonding portion where the bonding processing is to be performed. A bonding processing unit performs bonding of the first metal and the second metal using sound vibration and/or ultrasound vibration. The bonding processing unit performs the bonding processing using a plated material or otherwise using a metal portion in a state in which a plating material has been removed.

A method of assembling a first part made from a metal and a second part includes providing a first part comprising an assembly surface, and a second part comprising at least one through orifice. At least part of the second part is arranged on the assembly surface such that the orifice extends across from the assembly surface. A metal connecting part is positioned on the orifice to cover the orifice across from the assembly surface. The connecting part and/or the assembly surface are projected on one another to obtain high-speed plating and welding between the connecting part and the surface part.

The present invention includes: a preparation step in which a stepped portion including step bottom and step side surfaces is formed along an inner circumferential edge of a jacket body; a placing step in which a sealing body is placed on the jacket body forming first and second butted sections; and a main joining step in which friction stir welding is performed by moving a rotary tool along the first butted section, while only a stirring pin of the rotary tool is in contact with only the sealing body. During friction stir welding, a central axis of rotation of the rotary tool is tilted towards a central side of the jacket body so that the angle of tilt with respect to the step side surface is equal to the angle of inclination of an outer circumferential surface of the stirring pin with respect to the central axis of rotation.

To provide a pellicle frame for FPD (flat Panel display), which can maintain the rigidity required for a pellicle for a large FPD (flat Panel display) even if the cross-sectional area of the frame is reduced and can enlarge the inner dimensions of the frame by reducing the cross-sectional area, and has high dimensional accuracy and flatness, and an efficient manufacturing method thereof. The present invention provides a pellicle frame for FPD (flat panel display) composed of an extruded material of an aluminum alloy powder sintered body containing Si: 20 to 40% by mass, Mg: 0.2 to 1.2% by mass, Cu: 2% by mass or less, Fe: 2% by mass or less, Cr: 0.4% by mass or less, the balance being Al and unavoidable impurities to provide.

A primary joining rotary tool F comprises a stirring pin F2including a circumferential face tapers to become thinner toward a tip portion of the stirring pin, a flat face F3 at the tip portion of the stirring pin F2 and a projecting portion F4 projecting from the flat face F3. Friction-stirring is performed in the primary joining process by inserting the stirring pin F2 that is rotating into an abutted portion J1 in a manner that only the stirring pin F2 is in contact with the base member 2 and the lid plate 5 with the flat face F3 being in contact with the base member 2 and the lid plate 5 and with a tip face F5 of the projecting portion F4 being in contact only with the base member 2.

A welded blank assembly includes aluminum-based sheet metal blanks joined by a friction stir weld and an oxide removal zone on a surface of at least one of the blanks. The average thickness of an oxide layer in the oxide removal zone is less than elsewhere along the surface. The weld is at least partially located in the oxide removal zone and is substantially free from oxide remnants. A method of making a welded blank assembly includes removing at least a portion of an oxide layer on an aluminum-based sheet metal blank to form the oxide removal zone, then joining the blanks together at the oxide removal zone with a weld. Oxide regrowth in the oxide removal zone can be minimized and/or inhibited by welding within a pre-determined time after oxide removal, control of the local environment between oxide removal and welding, and/or use of an oxide inhibitor.

Shear assisted extrusion processes (ShAPE) for forming Metal-NCCF extrusions are provided. The processes can include: using a die tool, applying a rotational shearing force and an axial extrusion force to a feedstock material comprising a metal and NCCF (NanoCrystalline Carbon Films); and extruding a mixture comprising the metal and NCCF through an opening in the die tool to form the Metal-NCCF extrusion. ShAPE feedstock materials are provided that can include a metal and NCCF. Conductive solid material mixtures are provided that can include a metal and a NCCF. Portions of the metals and NCCF of the material mixtures can have an isotropic crystallographic orientation. Assemblies relying in part on conductivity can include: a conductive solid material mixture that includes: a metal; and a NCCF.

A foil stock comprising at least one AlFeSi-based layer. The foil stock according to the invention comprises an AlMg-based core layer and an AlFeSi-based cladding layer of not more than 0.05% by weight, in particular of not more than 0.03% by weight magnesium (Mg), thereby ensuring high strength and good deformation and coating properties of a carrier foil produced from said foil stock.

A battery module includes a plurality of battery cells each having a terminal, and a lead plate having a lead part each of which is joined to the terminal of each of the battery cells to electrically connect the battery cells to each other. The lead part includes an aluminum thin plate having aluminum purity higher than or equal to 99.0%. Surface roughness Ra of a joining surface of the lead part to the terminal is less than or equal to 10 μm. The lead part is electrically connected to the terminal by solid-phase bonding.