A friction damped insert for highly stressed engineering components is disclosed. The disclosed inventive concept provides a method and system for increasing the damping capacity of an engineering system by adding a non-flat solid, highly damped insert to a system component that contributes most to the system's dynamic response. The insert can either be embedded into a system component during casting or be fastened to the system component outer surface. The insert is made of the single layer of flexible material by forming it into a rigid elongated body. The layer of material can be turned over on itself without folding to create a cylinder or can be folded over a number of times to create a prismatic bar. The layer of material may be shaped into a corrugated panel. The layer of flexible material may have a number of relatively small openings or perforations with a uniform spatial distribution.

A friction damped insert for highly stressed engineering components is disclosed. The disclosed inventive concept provides a method and system for increasing the damping capacity of an engineering system by adding a non-flat solid, highly damped insert to a system component that contributes most to the system's dynamic response. The insert can either be embedded into a system component during casting or be fastened to the system component outer surface. The insert is made of the single layer of flexible material by forming it into a rigid elongated body. The layer of material can be turned over on itself without folding to create a cylinder or can be folded over a number of times to create a prismatic bar. The layer of material may be shaped into a corrugated panel. The layer of flexible material may have a number of relatively small openings or perforations with a uniform spatial distribution.

This shaping structure (1) comprises two shaping sheets (5, 7) facing each other at a distance from one another. According to the invention, the shaping structure (1) further comprises a macroporous spacer sheet (9), the spacer sheet (9) being arranged between the two shaping sheets (5, 7) and being corrugated in such a way as to form a series of alternating even peaks (18) and odd peaks (20) distributed in a first direction (D1) of the shaping structure, at least one of the even peaks (18) being attached to the first shaping sheet (5), at least one of the odd peaks (20) being attached to the second shaping sheet (7), each peak (18, 20) attached in this way defining an attachment surface (22, 26) for attachment to the shaping sheet (5, 7) to which this peak (18, 20) is attached.

A fiber reinforced energetic composite is provided. The fiber reinforced energetic composite includes reinforcing fiber embedded in a cured polymer matrix and energetic polymer nanocomposite disposed in the reinforcing fiber. The energetic polymer nanocomposite including core-shell nanoparticles entrained in a polymer matrix. The core-shell nanoparticles include a core made of a metal and at least one shell layer made of a metal oxide disposed on the core or a core made a metal oxide and at least one shell layer made of a metal disposed on the core. The method of making a fiber reinforced energetic composite is also provided. Further, a composite container made of fiber reinforced energetic composite is further provided.

A fiber reinforced energetic composite is provided. The fiber reinforced energetic composite includes reinforcing fiber embedded in a cured polymer matrix and energetic polymer nanocomposite disposed in the reinforcing fiber. The energetic polymer nanocomposite including core-shell nanoparticles entrained in a polymer matrix. The core-shell nanoparticles include a core made of a metal and at least one shell layer made of a metal oxide disposed on the core or a core made a metal oxide and at least one shell layer made of a metal disposed on the core. The method of making a fiber reinforced energetic composite is also provided. Further, a composite container made of fiber reinforced energetic composite is further provided.

A system and method for manufacturing composite parts has been developed which offers the ability to produce composite parts in an infusion resin process without the use of expensive preforms or tools. In addition, the methods of manufacturing composite parts described herein offer the ability to produce composite parts having complex structures without the need for complex tooling. The method of manufacturing and systems described herein typically include printing a part skeleton using an additive manufacturing process followed by infusing the part skeleton with resin and curing the resin infused part skeleton to form the composite part.

Patent of invention for automated process for manufacturing items of furniture in an integrated manufacturing cell and integrated cell for manufacturing items of furniture. There is described an automated process for manufacturing items of furniture in an integrated manufacturing cell, the process comprising the following steps: a) Initial machining of plate (P) according to a manufacturing program, generating channels and holes; b) Installing inserts in the holes generated in the initial machining and applying resin in at least one side hole of the insert; c) Applying edging resin inside the channels generated in the initial machining; d) Curing the edging resin and resin of the inserts in a heated environment; e) Final machining of plate (P) generating at least one item of furniture. There is also described an integrated cell for manufacturing items of furniture (100), comprising a machining station (200) and a curing station (50) associated with each other by way of a transfer module (30).

Patent of invention for automated process for manufacturing items of furniture in an integrated manufacturing cell and integrated cell for manufacturing items of furniture. There is described an automated process for manufacturing items of furniture in an integrated manufacturing cell, the process comprising the following steps: a) Initial machining of plate (P) according to a manufacturing program, generating channels and holes; b) Installing inserts in the holes generated in the initial machining and applying resin in at least one side hole of the insert; c) Applying edging resin inside the channels generated in the initial machining; d) Curing the edging resin and resin of the inserts in a heated environment; e) Final machining of plate (P) generating at least one item of furniture. There is also described an integrated cell for manufacturing items of furniture (100), comprising a machining station (200) and a curing station (50) associated with each other by way of a transfer module (30).

A method of manufacturing a gas tank comprises: a step (a) of preparing a liner having a hollow cylindrical shape; a step (b) of forming a first layer by winding a first fiber bundle impregnated with resin around the liner; a step (c) of forming a second layer by winding a second fiber bundle impregnated with resin around the liner with the wound first fiber bundle in such a manner that portions of the second fiber bundle overlap each other in a direction parallel to a center axis of the liner; a step (d) of causing a section where the portions of the second fiber bundle overlap each other to get into the first layer; and a step (e) of curing the resin.

A method of forming a cored composite laminate, the method including forming a first recess in a first coupling surface of a first layer of the cored composite laminate, forming a second recess in a second coupling surface of a second layer of the cored composite laminate so that when the first layer of the cored composite laminate and the second layer of the cored composite laminate are coupled, the first recess and the second recess form a cavity through the cored composite laminate, and disposing a shape memory alloy member in the cavity, so that the shape memory alloy member supports the cored composite laminate during curing of the cored composite laminate.