摘要:
A method of connecting a hub component and a connection between a shaft and a hub component, in particular a pinion connected to a shaft. The hub component and the shaft are formed of different materials, that is of ceramics and metal. A connecting element of metal is connected both to the hub component and to the shaft. The hub component and the shaft are connected to the connecting element by a material bond.
摘要:
A joint assembly that includes first and second joint members is provided. The joint assembly includes a reinforcing member that has an outer surface that defines a plurality of cavities. Foam is located in the joint members and engages the reinforcing member such that the foam is located in the cavities of the reinforcing member. Additionally or alternatively, the joint assembly may be constructed so that the inner surface of the first joint member defines a plurality of cavities. Foam is located in the joint members and engages the inner surface of the first joint member so that it is located in the cavities of the first joint member. Various methods of manufacturing and treating the joint assembly are also provided.
摘要:
Coupling apparatuses and methods of forming coupling apparatuses are provided herein. In an embodiment, a coupling apparatus includes a first component that includes a first metal substrate and a second component that includes a second metal substrate. The first metal substrate includes a titanium-based material. The second component is adapted to contact the first component in shear engagement. A protective coating is disposed on at least one of the first metal substrate or the second metal substrate. The protective coating consists of a first contact layer and, optionally, a diffusion barrier layer disposed between the first contact layer and the corresponding metal substrate. The first contact layer has a thickness of less than or equal to about 5 microns and includes material that is inert to titanium. The first contact layer has a contact surface that is adapted to directly contact an opposing surface in shear engagement.
摘要:
A splice and an associated method are provided in order to efficiently join structures, such as adjacent fuselage sections. A splice for joining fuselage sections may include a strap configured to bridge the fuselage sections, a shear tie overlying the strap and a fitting positioned between the strap and the shear tie such that the strap and the shear tie are spaced apart. At least the strap and the fitting may be formed of a composite material. The fitting may have an H-shape and may have first and second longitudinally extending sections that extend beyond opposite sides of the strap. Each longitudinally extending section is configured to overlie at least two stringers of a respective fuselage section. The fitting may also have a medial portion upon which the shear tie is seated.
摘要:
A splined drive body for supporting a plurality of sprockets is disclosed. The drive body is provided with at least one composite drive body spline which consists of a first portion made up of the drive body material and a second portion made up of a different, harder material. The second portion of the composite drive body spline is an insert which includes a force receiving surface and a force transmitting surface and is operable to transmit force transmitted to it into the drive body through a force receiving surface provided on the first portion of the composite drive body spline.
摘要:
A joint assembly that includes first and second joint members is provided. The joint assembly includes a reinforcing member that has an outer surface that defines a plurality of cavities. Foam is located in the joint members and engages the reinforcing member such that the foam is located in the cavities of the reinforcing member. Additionally or alternatively, the joint assembly may be constructed so that the inner surface of the first joint member defines a plurality of cavities. Foam is located in the joint members and engages the inner surface of the first joint member so that it is located in the cavities of the first joint member. Various methods of manufacturing and treating the joint assembly are also provided.