A procedure for repairing a polymer matrix composite component is provided. The procedure includes the steps of: providing a polymer matrix composite component having a site prepared for repair by removal of damaged or defective material; locating an uncured, polymer matrix composite repair patch at the site to re-build the component thereat; and curing the polymer matrix of the repair patch by heating the patch using eddy currents induced by one or more alternating current coils. The repair patch is without metallic additives, such that the repaired polymer matrix composite after the curing step is also without metallic additives in the vicinity of the repair patch.

A method for forming a composite material including reinforcing fibers includes connecting end portions of the reinforcing fibers with equipotential materials to form an electroconductive loop including the reinforcing fibers in the composite material before reaction; and applying a magnetic field in a direction intersecting a plane formed by the electroconductive loop.

An incremental forming machine and a process are disclosed that comprise selecting a blank and selecting a stylus tool that has a tip at one end. The stylus tool may be heated to a desired temperature before contacting the blank with the stylus tool to change a characteristic of the blank or part. The stylus tool apparatus may include a tip on an end of a shaft and a resistance heating element disposed inside the tip. Alternatively, the stylus tool apparatus may include an induction heating coil disposed around the tip. The tip of the stylus tool may have a rotatable ball that engages the blank or part.

The invention relates to a tool apparatus for producing a composite material component part, comprising a forming tool having a contact region for a workpiece, wherein the forming tool is made, in at least a portion thereof, of an electrically conductive material; and an induction heating apparatus having an inductive heating mat, wherein the heating mat is positioned in spaced relation to the forming tool, and wherein a positioning of the workpiece is provided between the heating mat and the forming tool, in contact with the forming tool, and wherein heating of the forming tool is provided, in at least a portion thereof, by the induction heating apparatus. The invention further relates to a method for producing a component part from a composite material by way of a forming tool.

A process for post curing a composite product made from a filament winding process comprises the steps of: surrounding the composite product, that is disposed about a rotatable mandrel, with an outer jacket; and simultaneously rotating and heating the mandrel resulting in post curing of the composite product according to a process that can be referred to as being a combo-semi-centrifugal post curing process.

The procedure (1) for obtaining raw materials resulting from waste material comprises: the supply (A) of harmonic steel resulting from waste material and prepared in a skein to be treated (3); a heat treatment (B) of the skein to be treated (3) for obtaining a treated skein (3a);—a post-treatment (E) of the treated skein (3a) for obtaining steel reusable as raw material; where the heat treatment (B) comprises an inductive exposure step (B1) of the skein to be treated (3) to at least an alternate magnetic field for the induction in the skein to be treated (3) of alternate eddy currents adapted to raise the temperature of same.

Provided a composite material forming method capable of easily using a composite material that is formed by causing a resin to react in a state where it is joined to another member; and a composite material. The composite material forming method includes a first material preparation step (magnetic field circuit forming material preparation step S11), a second material preparation step (magnetic field circuit non-forming material preparation step S12), a material assembly step S13, and a first heating step (magnetic field heating step S14). In the first material preparation step, a first material including a first resin is prepared. In the second material preparation step, a second material including a second resin is prepared. In the material assembly step S13, the first material and the second material are assembled to each other.

A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation. The plurality of smart susceptor heater blankets may be supported by a deployment system that lowers the plurality of smart susceptor heater blankets toward, and raises the plurality of smart susceptor heater blankets away from, a working surface.

A method of manufacturing a can lid composed of a composite material comprising at least one sheet metal part, in particular an aluminum part or a tin plate part, and at least one plastic part, in particular composed of polypropylene or polyethylene terephthalate, wherein the plastic material and the sheet metal part are joined together by pressing together and by inductive heating to effect a stable connection with an effort and a manufacturing time that are as small as possible.

A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.