A joint structure (1) for a composite member made from a composite material. The joint structure includes a plate for increasing thickness (40a, 40b) adhered to at least one side of the composite member (10). The composite member (10) and a counterpart member (20) are fastened together by inserting and fixing a fastener member (30) into a through-hole (24, 26) formed through the composite member (10), the plate for increasing thickness (40a, 40b), and the counterpart member (20) to be joined to the composite member.

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 hybrid component is formed by a profiled component of a first material, which is materially bonded in certain sections to a component made of a second material, and is connected by a form-fit and/or force-fit connection outside the sections with a material bond. This creates sections that relieve the strains resulting from differing thermal expansion.

A vehicle glazing unit including a glazed element and at least one base for reversible attachment of an accessory to the glazed element, the base including an aperture for passage of the accessory, the base including a non-flat outer face which is fastened opposite a non-flat inner face of the glazed element. The outer face includes two adhesive strips each having an elongate shape and both positioned lengthwise along the transverse horizontal axis of the glazing unit.

An adhesively bonded frame section for an agricultural sprayer boom is provided. One agricultural sprayer boom section includes a first support member and a second support member disposed adjacent to the first support member. The boom section also includes a side plate adhesively bonded to a first lateral side of the first support member, and to a first lateral side of the second support member to couple the first support member to the second support member.

An assembly of a first and second constructional part is provided, wherein the first constructional part has a first end and an opposite second end connected by a central part extending substantially perpendicularly to a surface of the second constructional part. The first end of the first constructional part is connected to said surface of the second constructional part with an encapsulating material at least partly surrounding said first end and adhering to said surface of the second constructional part. The first constructional part between its first and second ends is provided with at least one protruding part. The first constructional part in contact the encapsulating material is provided with a flange of which the vertical projection on said surface of the second constructive part completely covers the vertical projection of the protruding part on said surface. A method for making the assembly is provided.

A load-bearing structure of a motor vehicle, having hollow profiles and junction elements to connect the hollow profiles. The hollow profiles may be fastened in receptacles of the junction elements, and the junction elements may have a plurality of areal webs in a vehicle vertical direction, at least some of the areal webs forming a framework structure which assists the load path in the respective junction element.

The described embodiments relate generally to methods for enhancing cosmetic surfaces of friction stir processed parts. More specifically a method for applying cold spray over a weld line generated by friction stir processing is disclosed. Methods are also disclosed for blending the cold spray applied over the weld line with a cosmetic surface portion of the friction stir processed parts. In some embodiments cold spray can be used to create a cosmetic joint between various parts. Structural joints between first and second substrates may also be formed via solid state deposition. Such joints may be strengthened through use of a hidden weld, mechanical interlocking between the substrates, and/or coupling via fasteners.

An aircraft storage bin that includes an upper housing and a bucket that cooperate to define a bin interior. The bucket is movable with respect to the upper housing between open and closed positions and includes a bottom and right and left side panels. The bottom includes lower and upper surfaces and right and left outer edges. The right and left side panels each include a first section having a first transverse width, a second section having a second transverse width, and a transition section that is located between the first and second sections. The second transverse width is less than the first transverse width. At least a portion of the second section of each of the side panels is received in a slot defined in the upper surface of the bottom of the bucket, such that the right and left side panels extend upwardly from the bottom.

Disclosed is a fixing module for fixing an optical system to an optical apparatus, including a coupling unit having a plate to couple to the apparatus, the coupling unit having a first penetrating space at a central portion thereof and a protruding portion protruded downwards from the plate; a first fixing unit combinable with the coupling unit and having a receiving space including a thermosetting resin such that the protruding portion is fixed into the thermosetting resin; and a second fixing unit combinable with the first fixing unit and having a second penetrating space communicating with the first penetrating space, such that the optical system can penetrate through the first and the second penetrating spaces and be fixed by the second fixing unit.