A method for forming a vehicle reinforcing member (26, 28, 30). The method includes conforming a planar body of fibre reinforced material (CFRM) (504), such as a sheet or unidirectional tape, to a shape of a shape defining member (506, 900). In effect, the shape defining member (506, 900) is a core that defines an internal volume of a closed cross-section portion of the vehicle reinforcing member (26, 28, 30). The CFRM material (504) comprises continuous fibres in a synthetic matrix. The method further includes bonding a first edge portion (510) of the CFRM body (504) to a second edge portion (512) of the CFRM body (504) thereby to form the closed cross-section portion of the vehicle reinforcing member (26, 28, 30). An apparatus (800) for implementing the method, and components (e.g. vehicle reinforcing members (26, 28, 30), vehicle seats (10) and so forth) formed using the method are also described.

A replacement vibration absorbing device for replacing a wear wrap on a flexbeam includes a sleeve having a plurality of layers of vibration absorbing material, wherein an edge of the sleeve is cut so that the sleeve may be installed around a generally central portion of a flexbeam.

A replacement vibration absorbing device for replacing a wear wrap on a flexbeam includes a sleeve having a plurality of layers of vibration absorbing material, wherein an edge of the sleeve is cut so that the sleeve may be installed around a generally central portion of a flexbeam.

Provided herein is a method of manufacturing a product having a complex shape by using at least one jig and at least one mandrel. The method of manufacturing a product having a complex shape by using at least one jig and at least one mandrel is configured to include: a preparation step of preparing a prepreg sheet and a cylindrical first mandrel around which the prepreg sheet is wound; a first rolling step of forming a first stacking surface by winding the prepreg sheet around the first mandrel; a second mandrel preparation step of locating a second mandrel on the outer circumferential surface of the first stacking surface; a second rolling step of forming a second stacking surface by winding the first stacking surface and the second mandrel with the prepreg sheet; and a core removal step of removing the first mandrel and the second mandrel.

Provided herein is a method of manufacturing a product having a complex shape by using at least one jig and at least one mandrel. The method of manufacturing a product having a complex shape by using at least one jig and at least one mandrel is configured to include: a preparation step of preparing a prepreg sheet and a cylindrical first mandrel around which the prepreg sheet is wound; a first rolling step of forming a first stacking surface by winding the prepreg sheet around the first mandrel; a second mandrel preparation step of locating a second mandrel on the outer circumferential surface of the first stacking surface; a second rolling step of forming a second stacking surface by winding the first stacking surface and the second mandrel with the prepreg sheet; and a core removal step of removing the first mandrel and the second mandrel.

A method for manufacturing a waterproof felt duct may include (a) laminating a waterproof film on one side of a first nonwoven fabric and laminating a second nonwoven fabric on the waterproof film laminated on the first nonwoven fabric to form a laminated body; (b) forming a waterproof felt base material by thermally adhering the laminated body; (c) cutting the waterproof felt base material into a desired shape; (d) molding a duct while surrounding the waterproof felt base material cut into the desired shape around the external surface of a molding jig having a worm gear shape; (e) heat-treating the molded duct; (f) cooling the heat-treated duct; and (g) ejecting the cooled duct from the molding jig.

A method of constructing a mandrel generally complementary to a spar cavity of a spar includes connecting a first component and a second component to form a central space there between and inserting a center component within the central space such that the center component retains the first component and second component in a desired position forming an outer surface of the mandrel which corresponds to an inner surface of the spar cavity.

A method of forming a hollow spar for an aerofoil includes forming a sandwich structure having a first structural layer, a second structural layer and a cellular core layer located in between the first structural layer and the second structural layer. At least part of the sandwich structure is removed at intervals corresponding to one or more corner locations, and the sandwich structure is folded at the one or more corner locations to define a hollow space and form the spar. A chordwise extending rib section for an aerofoil has a substantially planar web with a chordwise length; and a reinforcement strip attached to an edge of the web over substantially the majority of the chordwise length.

A system for labeling a container includes a label forming section, a buffer section, and a bonding section. The label forming section includes a first rotatable turret having a plurality of forming mandrels. The buffer section includes a second rotatable turret having a plurality of buffer receptacles. The bonding section includes a third rotatable turret having a plurality of bonding stations. The label forming section forms a label in a frustoconical shape using one of the forming mandrels and transfers the label to one of the buffer receptacles of the buffer section. The buffer section receives, in a buffer receptacle, the label followed by a container blank, and transfers the label and the container blank together to one of the bonding stations of the bonding section. The bonding section bonds the label to the container blank in the bonding station.

A system for labeling a container includes a label forming section, a buffer section, and a bonding section. The label forming section includes a first rotatable turret having a plurality of forming mandrels. The buffer section includes a second rotatable turret having a plurality of buffer receptacles. The bonding section includes a third rotatable turret having a plurality of bonding stations. The label forming section forms a label in a frustoconical shape using one of the forming mandrels and transfers the label to one of the buffer receptacles of the buffer section. The buffer section receives, in a buffer receptacle, the label followed by a container blank, and transfers the label and the container blank together to one of the bonding stations of the bonding section. The bonding section bonds the label to the container blank in the bonding station.