A turbine engine for an aircraft which includes, in general, at least one assembly made up of a first part wherein a second part is attached with an attachment device including a milled head applied to the first part and a body engaging with the second part in order to clamp the parts. The recess of the head of such an attachment device requires a boss on the first part, which is complex and expensive to produce using conventional techniques. Such a boss can be replaced with a removable seat having an opening through which the body passes and forming a recess for the head, a bearing surface for the head, and abutment device applied to the first part in order to prevent a movement of the seat towards the second part.

A fixing washer comprising: an outer portion and an inner portion, the outer portion is radially outward of the inner portion and the inner portion defines a recessed region which is arranged, in use, to receive a head of a fastener, and the washer also comprises a number of channels, each of said channels extends though the inner portion and the outer portion.

The invention relates to a protection dish (32) for a counterbore formed in an aircraft mechanical part, said protection dish (32) having an axial cross-section about an axis (A) having substantially the shape of a U, and comprising a substantially annular wall (34) of axis (A) and a substantially cylindrical rim (36) of axis (A) connected to an outer periphery of said substantially annular wall (34). The invention is characterised in that said dish (32) is configured to be deformed in response to an axial stress (F) of a determined intensity applied on the substantially annular wall (34) thereof from a first state, wherein the substantially cylindrical rim (36) has a first transverse dimension (E) relative to axis (A), to a second state, wherein the substantially annular wall (34) being deformed, the cylindrical rim (36) has a second transverse dimension (E′) relative to the axis (A) that is greater than the first transverse dimension (E) along a transverse direction (T) determined relative to axis (A).

A fastening system to couple a first aircraft structure and a second aircraft structure is disclosed. The fastening system includes a fastener, a nutplate having a body defining an opening to receive the fastener, a flange extending from the body to engage an outer surface of the first structure, and a first sleeve protruding from the flange in a direction away from the body, the first sleeve to couple to a first bore formed in the first structure and prevents rotation of the nutplate relative to the first structure.

A fastener to fasten a member to be fastened includes a shaft portion, a tool working surface, and an external operation restricting portion. The shaft portion is provided with a male thread configured to be rotated about an axis line to work so as to fasten the member to be fastened. The tool working surface is formed to a tool working portion integrated with the shaft portion. A tool to rotate the shaft portion works to the tool working surface. The external operation restricting portion is configured to restrict the rotation of the shaft portion through an operation from outside the fastener. In this fastener, the tool working surface to which the tool works is formed in an approximately cylindrical inner surface shape.

A fastener is provided and is configured for securing magnetized items to a wallboard panel. Included on the fastener is a fastener body having a first side and an opposite second side, and a counter-sunk throughbore extends from the first side to the second side. The body has a tapered peripheral edge. In addition, the first side is covered with wallboard joint tape.

A wall mounting system is provided including a fastening member including one or more mounting studs and one or more anchor apertures. The fastening member is configured to be anchored to a support structure by one or more fasteners disposed through the one or more anchor apertures. The wall mounting system also includes a bushing assembly including an inner portion including a through hole configured to receive a mounting stud and an outer portion configured to rotate about the inner portion and including at least one set screw aperture configured to align with a set screw aperture of an accessory sleeve and receive a set screw. Rotation of the outer portion about the inner portion enables indexing of the set screw aperture about a longitudinal axis of the bushing assembly.

A bicycle adapter is configured to couple a bicycle operating device to a handlebar clamp is coupled to a handlebar. The bicycle adapter includes a first attachment surface and a second attachment surface. The first attachment surface is configured to be attached to an outer surface of the clamp. The second attachment surface is configured to be attached to the bicycle operating device. The first attachment surface has a first curved section. The second attachment surface has a second curved section that is different from the first curved section.

Disclosed is a bilateral anti-loosening and sealing nut, comprising a nut body having a tapped hole with a tapped-hole thread and being surrounded by a central-wall-surrounding portion, a flange portion, a front-protruding-annular edge, a rear-recess portion, and a front-engaging portion, the front-engaging portion having an inwardly-recessed-receiving portion and an engaging-protruding edge, the inwardly-recessed-receiving portion being formed between a front surface of the central-wall-surrounding portion and a rear surface of the engaging-protruding edge; an annular washer being arranged within the inwardly-recessed-receiving portion; and a sealing washer being arranged within the rear-recess portion.

A bicycle operating device includes a base member coupled to a handlebar clamp and a user operated member movably coupled to the base member to move a mechanical control cable with respect to the base member. The base member includes a coupling portion coupled to the handlebar clamp. The coupling portion includes an elongated hole having a long direction extending parallel to a center axis of the handlebar clamp. The coupling portion is coupled to the handlebar clamp via a fastener extending into the elongated hole. The user operated member is movable with respect to the base member between a rest position and an operated position. The bicycle operating device does not mechanically fix a position of the mechanical control cable with respect to the base member in accordance with movement of the user operated member between the rest position and the operated position.