Systems, methods, and apparatus are disclosed for controlling a flow of a material through a vehicle component. In some embodiments, the methods include determining a first plurality of dimensions and a second plurality of dimensions associated with a flow medium based on one or more flow properties of the vehicle component, the flow medium including a plurality of baffle layers and a plurality of spacers. The methods may further include generating at least one baffle layer based on the first plurality of dimensions, and generating at least some of the plurality of spacers based on the second plurality of dimensions, the plurality of spacers being positioned on top of the at least one baffle layer.

Systems and methods are provided for vacuum handling of composite parts. One embodiment is a method for performing vacuum securement of an object. The method includes covering the object with an impermeable membrane, locating a vacuum port at the impermeable membrane, and applying a negative pressure to the vacuum port that offsets air leaks between the impermeable membrane and the object.

A method for manufacturing a wind turbine blade including: arranging an upper mold on a lower wherein a dry fiber lay-up is arranged in the upper mold or in the upper mold and the lower mold, applying vacuum to a space between the upper and lower molds, and infusing the dry fiber lay-up in the upper and/or lower molds with resin through at least one upper resin inlet arranged at an upper portion of the upper mold. Having the at least one upper resin inlet of the upper mold improves the vacuum-assisted resin infusion. Resin provided through the at least one upper resin inlet has to be raised by a smaller height to reach the top of the mold. A resin flow of the resin provided through the at least one upper resin inlet is supported in a downward direction by the gravitational force.

A manifold for resin application, infusion, and/or injection is provided. The manifold comprises at least one inlet and a plurality of outlets. At least one outlet of the manifold comprises a valve that is operable to selectively dispense or terminate a flow of a resin from the outlet, and wherein the resin is supplied through the at least one inlet.

This invention describes novel design and construction method for inflatable, pressure intensifier equipment that can be used for processing composites structures. The equipment can be used as a manufacturing and processing platform wherever low pressure and high temperature inputs are required in an enclosed volume.

A method for joining structural elements to a component made of at least one fiber-reinforced plastics material, includes providing at least two structural elements made of at least one fiber-reinforced plastics material having a particular matrix; providing at least one film element made of a thermoplastic heavy-duty material; arranging the at least one film element on a surface of one of the structural elements or between surfaces to be joined of the at least two structural elements to be joined; and producing the component to be joined in a curing process.

A method of manufacturing a thermoplastic panel may comprise: laying up a panel preform within a consolidation assembly, the panel preform comprising a plurality of plies of material comprising thermoplastic resin and fiber; generating, via a hot bond unit, a vacuum environment within the consolidation assembly; and heating, via the hot bond unit and through a heated blanket within the consolidation assembly, the panel preform.

Resin infusing a composite preform includes placing a first vacuum bagging film over a tool surface and the composite preform to define a sealed first chamber. A bridge structure has an underside defining a cavity above the first vacuum bagging film. A second vacuum bagging film is placed over the first vacuum bagging film and the bridge structure to define a sealed second chamber. At least partial vacuum pressure is applied to the first chamber to drive resin from a resin supply through the first chamber, infusing the composite preform with resin. Partial vacuum pressure is applied inside the second chamber and an exterior pressure is applied outside the second vacuum bagging film while. The exterior pressure exceeds the pressure applied to the first and second chambers, thereby compacting the composite preform outside of a region, with the bridge supporting the second vacuum bagging film against the exterior pressure.

The invention provides a method for preparing a fiber-reinforced part based on cyanate ester or a cyanate ester/epoxy blend, comprising the steps of (i) providing a liquid mixture comprising (a) from 15 to 99.9 wt. % of at least one di- or polyfunctional cyanate ester, (b) from 0 to 84.9 wt. % of at least one di- or polyfunctional epoxy resin, and (c) from 0.1 to 25 wt. % of a metal-free catalyst; (ii) providing a fiber structure (iii) placing said fiber structure in a mold or in a substrate, (iv) impregnating said fiber structure with said liquid mixture, (v) curing said liquid mixture by applying a temperature of 30 to 300° C. Using the method of the invention it is possible to produce in a short cycle time, using composite manufacturing processes such as resin transfer molding and infusing technology, fiber reinforced composite parts based on a cyanate ester or cyanate ester/epoxy resin formulation. The fiber-reinforced parts obtainable by the above method are also an object of the invention.

A pliable structure includes a first impermeable layer, a second impermeable layer opposed from the first impermeable layer to at least partially define an internal volume between the first impermeable layer and the second impermeable layer, and a flow media layer disposed in the internal volume.