A method of manufacture of a carbon fiber article comprises providing a preform mold having a region that is shaped to compliment a shape of a preform part that is to be produced the surface being provided with at least one bore or groove that is connected to at least one conduit that passes through the mold to a manifold, laying a sheet of release material onto the surface covering at least some of the plurality of holes, applying reduced pressure to the manifold to cause the sheet to be sucked down onto the mold surface, laying carbon fiber material into the mold on top of the sheet of release material, applying an increase pressure to the manifold to push the preform free from the mold surface, and removing the preform from the mold.

The invention relates to a moulded part of a composite material comprising a main body (10) of polymer concrete or of reaction resin, which has at least one adhesion bonding surface (11) for adhesively bonding to an article, wherein the adhesive bonding surface (11) is detachably connected to a laminate layer (12) texturing the adhesive bonding surface (11).

Provided is a method of manufacturing a circuit board including preparing a board structural body (11) and covering a conductor circuit element (13) on an outermost layer of the board structural body (11) with a cover film (14), wherein a heat treatment is performed while having a release material (15) interposed between the cover film (14) and a heat-processing device. The release material (15) is a laminate at least including, sequentially from the cover film toward the heat-processing device, a low friction film (16) selected from an ultrahigh-molecular-weight polyethylene film and a polytetrafluoroethylene film, a first aluminum foil (17), a first high-density polyethylene film (18a), a second high-density polyethylene film (18b), and a second aluminum foil (19). The first high-density polyethylene film (18a) and the second high-density polyethylene film (18b) are positioned such that respective MD directions are perpendicular to each other.

Systems and methods for manufacturing unidirectional fiber prepreg tapes for CMC articles are provided. In one exemplary aspect, the method includes casting a matrix material on a carrier film to form a matrix film. The matrix material of the matrix film is then allowed to dry for a predetermined time. The matrix film is then wrapped on a drum and the matrix material is wet to a predetermined viscosity with a solvent. Thereafter, a fiber tow that includes of a plurality of fibers is wound about the drum so that the fiber tow penetrates into the matrix material and the matrix material impregnates the fiber tow to form the prepreg tape.

A layer-by layer method for additive manufacturing that includes: photocuring a first volume of resin to form a layer of a build at an upper surface of a separation membrane laminated over a build window; injecting a fluid into an interstitial region between the separation membrane and the build window; retracting the build from the build window; evacuating the fluid from the interstitial region; and photocuring a second volume of liquid resin to form a subsequent layer of the build between an upper surface of a separation membrane and the previous layer of the build.

A method and apparatus for reworking a structure. A compaction blanket comprising a number of magnets is placed on the structure. A heat source is applied on the compaction blanket, wherein the compaction blanket is between the heat source and a rework of the structure and heat is conducted from the heat source through the compaction blanket to heat the rework.

A method for the simultaneous production of two or more fiber composite components, to a fiber composite component, to a rotor blade of a wind power installation, as well as to a wind power installation. A method for the simultaneous production of two or more fiber composite components, in particular of two or more substantially identical fiber composite components which have a component contour, the method comprising providing at least one fibrous material, at least one planar separation element, and at least one matrix material, wherein the at least one planar separation element at least in portions is permeable to the matrix material; producing a semi-finished fibrous pack by disposing the fibrous material layer-by-layer so as to form semi-finished fibrous products stacked on top of one another, wherein at least one of the planar separation elements is in each case disposed between the semi-finish fibrous products; infusing the semi-finished fibrous pack with the matrix material; cutting the component contour into the infused semi-finished fibrous pack.

Example systems and methods are described including backing paper for use with uncured pre-impregnated material. An example system includes a backing paper having a first surface and a second surface. The system also includes a coating material positioned on the first surface of the backing paper. A blowing agent is encapsulated within the coating material.

A shaped object production method includes a first preparation step (S30) of preparing a molding sheet that includes a base, a thermally expansive layer laminated on a first main surface of the base, the thermally expansive layer including a thermally expandable material, and a brushed layer laminated on a surface of the thermally expansive layer on a side that is opposite to the base, the brushed layer including fiber; a first heat conversion layer laminating step (S40) of laminating a heat conversion layer that converts electromagnetic waves into heat onto a surface of the molding sheet on a side that is opposite to the brushed layer; and a first unevenness forming step (S50) of forming an unevenness on the surface of the thermally expansive layer on the side that is opposite to the base by irradiating the heat conversion layer with electromagnetic waves, thereby causing the thermally expandable material to expand.

A formable resin sheet includes a thermally expansive layer formed on a first side of a base and including a thermally expandable material. A breaking strength of the thermally expansive layer is greater than a peeling strength of the thermally expansive layer from the base, and the thermally expansive layer is peelable from the base. The formable resin sheet can easily be shaped by using a thermal conversion layer to cause the thermally expansive layer to distend and cause the base to deform as the thermally expansive layer distends. The thermally expansive layer can be removed after the shaping of the base.