An assembly to connect a panel to a support member. The assembly may include a saddle fitting configured to connect to the support member and including first and second plates. A back fitting may be positioned between the second plate of the saddle fitting and a second face of the panel. An index fitting includes a flange that may be positioned between the first plate of the saddle fitting and a first face of the panel, and a boss that extends outward from the flange and through the opening in the panel. The index fitting is wider than the panel and sized to fit within the gap of the saddle fitting with a first end of the index fitting contacting against the first plate and a second end of the index fitting contacting against the second plate. One or more fasteners may connect the saddle fitting to the index fitting.

There is disclosed a modular platform assembly including a plurality of legs (18), a plurality of floor beams (20a,b,c), and a plurality of connectors (24a,b,c,d) for connecting the legs (18) and the floor beams (20a,b,c). Each said connector (24a,b,c,d) comprises: a downwardly open blind recess (59) with a closed top end (60) and an open bottom end (62); and an upwardly open blind recess (64) with a closed bottom end (66) and an open top end (68). The legs (18) are mounted into the downwardly open blind recesses (59) of the connectors (24a,b,c,d) and the floor beams (20a,b,c) are mounted into the upwardly open blind recesses (64) of the connectors (24a,b,c,d) such that the legs (18) extend downwardly from the floor beams (20a,b,c).

A guide member 48 includes a cylindrical portion 52 fitted to a front end of a pinion shaft 19 and extending on the side of an opposite yoke and a slit engagement plate 54 extending on the side of the pinion shaft 19 from a portion, on the side of the pinion shaft 19, of the cylindrical portion 52 and engaging with a slit 42 of a yoke 22, the cylindrical portion 52 being inserted first in a clamp portion 36 of the yoke 22 upon the yoke 22 being fitted to the pinion shaft 19, the yoke 22 being rotatably guided by the cylindrical portion 52.

The present invention provides a crib rail structure that includes: at least one hollow horizontal tube member, a side portion of which is provided with a plurality of interspaced openings; and a plurality of hollow beam tube members, which are respectively inserted into the interspaced openings of the hollow horizontal tube members for assembly use. The sides of each of the hollow beam tube members are provided with a through opening, which are located in the tail end of the hollow beam tube member. Moreover, the positions of the through openings are adjacent to the sides of each of the interspaced openings of the hollow horizontal tube member. The crib rail structure further comprises the at least one fixing member, which passes through the plurality of hollow beam tube members and presses against the tube inner wall of the hollow horizontal tube member for fixing thereof.

A cardan joint spider comprising a body having four right-angled brackets, each bracket presenting two mutually perpendicular arms, the arm of one bracket being assembled to the arm of an adjacent bracket so as to form a cross-shaped spider having four branches.

A structural supporting bearing is comprised of a flange with a hole in the center and a cylindrical hollow tube. The cylindrical tube section is inserted through an appropriately sized hole in hollow fiberglass plastic tubing. The flange creates a stop for the cylinder against the outer wall of the tube. The length of the cylindrical tube is sized to approximately one-half the cross-section of the tube, so as to allow a similar bearing to be mounted to the other side of the tube. A plurality of other structural members is placed over the flanges as desired. The aforementioned assembly is configured to receive a suitably sized bolt through it and be secured in place with a receiving nut.

A joint for a composite frame includes a first composite rod, a first shell abutting the first composite rod, a second shell abutting the first composite rod and disposed opposite the first shell relative to the first composite rod. The first and second shells are joined together such that composite rod is fixed therebetween. A method of forming joints of composite frame includes forming a composite frame by interconnecting a plurality of composite rods formed by an Automated Fiber Placement (AFP) manufacturing method around a mandrel, applying a first shell to the plurality of composite rods at a first location where composite rods are interconnected, applying a second shell at the first location opposite the first shell relative to the composite rods, and joining the first and second shells together with the composite rods at the first location disposed between the first and second shells.

An assembly to connect a panel to a support member. The assembly may include a saddle fitting configured to connect to the support member and including first and second plates. A back fitting may be positioned between the second plate of the saddle fitting and a second face of the panel. An index fitting includes a flange that may be positioned between the first plate of the saddle fitting and a first face of the panel, and a boss that extends outward from the flange and through the opening in the panel. The index fitting is wider than the panel and sized to fit within the gap of the saddle fitting with a first end of the index fitting contacting against the first plate and a second end of the index fitting contacting against the second plate. One or more fasteners may connect the saddle fitting to the index fitting.

A cardan joint spider comprising a body having four right-angled brackets, each bracket presenting two mutually perpendicular arms, the arm of one bracket being assembled to the arm of an adjacent bracket so as to form a cross-shaped spider having four branches.

A joint for a composite frame includes a first composite rod, a first shell abutting the first composite rod, a second shell abutting the first composite rod and disposed opposite the first shell relative to the first composite rod. The first and second shells are joined together such that composite rod is fixed therebetween. A method of forming joints of composite frame includes forming a composite frame by interconnecting a plurality of composite rods formed by an Automated Fiber Placement (AFP) manufacturing method around a mandrel, applying a first shell to the plurality of composite rods at a first location where composite rods are interconnected, applying a second shell at the first location opposite the first shell relative to the composite rods, and joining the first and second shells together with the composite rods at the first location disposed between the first and second shells.