Abstract: An eating appliance includes a swatch of a preformed carbon fiber resin of a predetermined size shaped and which is thermally permanently formed into an eating appliance shape to have a concave portion having a bottom and upwardly extending wall portion therefrom which terminates into a peripheral edge and wherein the peripheral wall has a reinforcing or decorative member connected to the peripheral edge. A method of forming the eating appliance is provided.

Abstract: A flexible abrasion resistant omnidirectionally reflective, preferably retractable, flat belt pet leash/pet collar exhibits omnidirectional reflectivity. The omnidirectionally reflective flat belt pet leash reflects an incoming light beam back in the direction from which it emanated. The reflected light beam provides accurate illumination of the pet leash and the location of the pet during dusk or nighttime hours. This reflective pet collar and/or leash is created by forming a substantially flat reflective woven band composed of narrow width reflective strips that comprise woven or knitted reflective threads. A raised, braided, dimensional band is optionally placed atop the substantially flat reflective woven band to further increase reflectivity and visibility thereof. The flexible reflective threads are composed of microsphere retroreflectors coated with water resistant compound and, optionally, a poly-phosphorus material.

Abstract: A filter element (100) according to the invention comprises a filter volume (150) having an inflow side and an outflow side defining an average flow direction. The filter volume (150) has an axis substantially parallel to the average flow direction and further comprising a casing (140) delimiting the outer boundary of the filter volume in the direction of the average flow path. The casing (140) is gas impermeable in radial direction. The filter volume (150) is filled with a filter material (111) comprising fibers, a majority of the fibers (102) at least partially encircle the axis.

Abstract: A method of making a filter is disclosed including providing a mandrel, positioning a filter form on the mandrel, the filter form including a dissolvable compound, disposing a filter basket over the filter form, dissolving the filter form, and removing the mandrel from the filter basket.

Abstract: To provide a seat having a three-dimensional complex undulated cushion body securing hardness in a stress direction and excelling in dispersibility of the stress and durability, and a method of manufacturing the same.

Abstract: A unified head for a staked fastener wherein the unified head is made from a first member in combination with a supplemental member, and the two members have at least one shared fiber. In a staking operation that forms the unified head, the operation is conducted in such a manner that a portion of a fiber, initially within the first member or the supplemental member, crosses the boundary therebetween creating the shared fiber, i.e., a segment of a single fiber is embedded in the first member and a segment is embedded in the supplemental member.

Abstract: A process for manufacturing a component with an insert made of a composite is disclosed. The composite includes a metal matrix, within which ceramic fibers extend. The insert is made of a composite which is obtained from a plurality of coated filaments, each filament includes a ceramic fiber coated with a metal sheath. The process includes winding a bundle or bonded sheet of coated filaments around a body of revolution perpendicular to the axis of rotation of said body. The insert is then subjected to a hot isostatic pressing step in a container. The process is applied to the manufacture of aeronautical turbomachine components.

Abstract: A biocomposite is produced from natural fiber fabrics embedded in a matrix of biosynthetic polyhydroxy-alkanoate (PHA) polymers. The PHA is synthesized using aerobic microbial biosynthesis using mixed bacterial cultures and a feedstock containing anaerobic degradation products such as methane and volatile fatty acids derived from microbial biodegradation of organic waste materials, which may include waste biocomposites. Monomers may be added to the synthesized PHA polymer to control mechanical properties of the resulting biocomposite. The natural fibers and/or PHA may be pretreated using various techniques to improve the bond between the fibers and the PHA resin matrix and water absorption resistance of the fibers. The composite may be a laminate of treated and untreated fabric layers, or differently treated layers, to achieve good in-service performance as well as rapid and/or optimal biogas production when taken out of service and put in an anaerobic environment to degrade.

Abstract: The invention relates to a process for manufacturing a metal part reinforced with ceramic fibres, in which: at least one housing (10A) for an insert is machined in a metal body (10) having an upper face (10B); at least one insert (11) formed from ceramic fibres in a metal matrix is placed in the housing; the insert is covered with a cover; a vacuum is created in the interstitial space around the insert and said space is hermetically sealed under vacuum; the assembly, namely the metal body with the cover, is treated by hot isostatic pressure; and said treated assembly is machined in order to obtain said part. The process is characterized in that the cover comprises an element (12) covering the insert (11) in the slot and projecting from the upper face, and a sheet (14) covering the upper face with said element (12). In particular, the insert (11) is straight and the housing for the insert in the metal body forms a straight slot.

Abstract: The invention relates to a method for tolerance compensation between two fibre composite component parts (1, 3) for aircraft. In order to compensate in simplified fashion tolerances between two fibre composite component parts being joined, the method according to the invention has the steps: a) manufacturing the first fibre composite component part (1) wherein an assembly surface (2) can have tolerance deviations, b) manufacturing a tooling insert (7) from a surface geometry of the assembly surface (2) c) manufacturing the second fibre composite component part (3) by means of the tooling insert (7) wherein a surface geometry of a contact surface (9) of the second fibre composite component part (3) corresponds substantially with the surface geometry of the assembly surface (2), and d) joining the first fibre composite component part (1) to the second fibre composite component part (3) in the area of the assembly surface (2) and contact surface (9).

Abstract: A curved composite aircraft frame comprises a multi-ply composite laminate having a generally Z-shaped cross section. At least certain of the laminate plies include unidirectional reinforcing fibers that are substantially tangent at substantially all points along the curvature of the frame.

Abstract: In a fiber there is provided a fiber matrix material having a fiber length; and an array of isolated in-fiber filaments that extend the fiber length. The in-fiber filaments are disposed at a radius in a cross section of the fiber that is a location of a continuous filament material layer in a drawing preform of the fiber. As a result, there is provided a fiber matrix material having a fiber length; and a plurality of isolated fiber elements that are disposed in the fiber matrix, extending the fiber length, where the plurality is of a number greater than a number of isolated domains in a drawing preform of the fiber.

Abstract: A method and a device for realizing a curved composite material profile made of composite material, and to the resulting profile (63), in which the profile is made from at least one composite strip (11) extending along a longitudinal axis. The strip is formed by stacking at least two tapes of unidirectional reinforcing fibers (4, 5, 6) arranged in orientations.

Abstract: A tampon applicator barrel including a cardboard tube having a first end and a second end and at least one gripping structure defined from the cardboard tube proximate the second end is provided. The cardboard tube has a wall thickness of between about 0.015 and about 0.020 inches, while the gripping structure has a height of up to about 0.035 inches.

Abstract: A tension-torque-transmission element (3; 3?; 4) for a rotor blade of a rotary wing aircraft (helicopter), in particular for a fenestron blade of a tail rotor, with a connecting section on the blade side and a connecting section (30; 30?; 40) on the axis side, with a connecting eye (32) on each connecting section, and with a torque-transmission section (34; 34?; 44) that connects the connecting sections (30; 30?; 40), is improved in that the tension-torque-transmission element (3; 3?; 4) is designed in a fibre-reinforced composite design including several layers (A to G) of a textile fabric. A method for producing such a tension-torque-transmission element (3; 3?; 4) is also described.

Abstract: A method of electrohydraulically trimming a blank involving positioning a blank on a trimming member having a cutting edge such that a portion to be trimmed extends over the cutting edge and is in fluid communication with a chamber. Immobilize the blank with respect to the trimming member. Position a pair of electrodes in the chamber proximate the portion of the blank to be trimmed such that the electrodes and the trimming member are on opposite sides of the blank. Electrically connect the electrodes to a capacitor. Charge the capacitor. Fill the chamber with fluid to submerge the electrodes and to contact the portion of the blank to be trimmed. Discharge the capacitor across the electrodes to generate a pressure pulse that pushes the portion of the blank to be trimmed against the cutting edge thus trimming it off the blank.

Abstract: Metal matrix composites having open or closed channels extending longitudinal through the length of the composite as well as methods and apparatus for forming the same are described. The shaped metal matrix composites are made of continuous fiber reinforced metal matrix composite materials. They have an integrally formed, non-cast, metal matrix composite body portion where the walls have a substantially uniform distribution of continuous fibers in a matrix metal throughout the volume of the walls and have at least one channel extending through the body of the shaped metal matrix composite.

Abstract: Methods and systems for manufacturing composite components, including asymmetric composite components, are disclosed. In one embodiment, a method of forming a composite component includes providing a forming tool having a base portion and at least one retaining portion; forming an uncured composite component on the forming tool; curing the composite component; performing a manufacturing operation on the cured composite component engaged with the forming tool; and after performing the manufacturing operation on the cured composite component, removing the cured composite component from the forming tool. In further embodiments, the forming tool may have a plurality of reference apertures disposed therethrough for performing drilling operations on the cured composite component.

Abstract: A force transmitting assembly comprises a composite fiber tie rod having a force transmitting element on the end thereof. The force transmitting element has at least a portion having a cross-section that tapers in a direction pointing away from the tie rod end. The load bearing fiber layer of the tie rod extends over and is wound about the tapered portion of the force transmitting element, thereby establishing a positive connection between the tie rod and the force transmitting element. The invention further relates to a method of manufacturing a force transmitting assembly comprising a composite fiber tie rod and a force transmitting element on an end thereof.

Abstract: A distal protection device captures debris during vascular procedures. In order to reduce the profile of the device, the thickness of the distal protection element is reduced in one or both of the end regions, either by reducing the thickness of filaments which form the distal protection element, or by removing portions of those filaments altogether. Various methods of reducing the thickness of the end regions and different profiles that can be created by the reduction are disclosed.

Abstract: Herein provided is a sound-insulating laminated structure which is excellent in the ability of insulating low frequency sounds whose frequency falls within the range of from 200 to 1000 Hz. The sound-insulating laminated structure comprises a first glass wool layer, a metal foil layer free of any opening and a second glass wool layer. The first and second glass wool layers are ones each prepared by collecting and combining short glass fibers through the application of an uncured thermosetting phenol resin to the short glass fibers to thus give a web of glass wool prepreg and then molding, with heating, the web into a sound-insulating laminated structure having a desired shape.

Abstract: Embodiments of the present invention comprise a composite rim for used in spoked wheels, such as bicycle wheels, having molded-in spoke holes along with a method of fabricating the composite rim. Advantageously, the bearing and loading strength of the rim is improved over prior art composite rims wherein the spoke holes are drilled therein after fabrication of the rim hoop.

Abstract: A method for making a golf club head includes steps for processing upper and lower shells of the head. A metal- or non-metal-based composite material is provided which has a necessary thickness and whose area and total width are enough for making at least two unit shells, as determined by widths and surface curvatures of the upper and lower shells. A strip of excess material is reserved at a border between the unit shells. The two alternately or non-alternately arranged unit shells are integrally formed through a forming process, wherein an extension force generated while the unit shells are formed is constrained by the excess material to reduce deformation of the unit shells, so that the formed unit shells have flat cutting surfaces when the excess material is cut off, allowing the upper and lower shells thus made to have precise dimensions, improved ends of parts and close contact surfaces.

Abstract: An apparatus (1, 2, 20) and method are provided for separating a length of twisted pair cable (10) into its constituent individual insulated wire conductors (11, 12) for subsequent use in telecommunications networks or other electrical equipment. The apparatus (1, 2, 20) includes a separator (15, 66) adapted for insertion between the individual insulated wire conductors (11, 12) constituting the twisted pair cable (10). Cable drive means are provided to cause displacement of the length of twisted pair cable (10) relative to the inserted separator (15, 66) in a direction (a, b) co-incident with the axis of the twisted pair cable (10). In addition to separating the insulated wire conductors (11, 12), the driving (a, b) of the twisted wire cable (10) past the separator (15, 66) also causes plastic deformation of the individual insulated wire conductors (11, 12) thus preventing them from springing back into their initial wound state.

Abstract: A lacrosse stick mesh is disclosed in which each aperture of the mesh has the form of an extended diamond shape. The extended diamond shape of each aperture has a greater length in a vertical direction than in a horizontal direction. The vertical direction is the direction in which the lacrosse ball is thrown from the pocket of the lacrosse stick mesh. The lacrosse stick mesh has more surface area that is in contact with a lacrosse ball in the vertical direction when the lacrosse ball is in the mesh pocket. When a player swings the lacrosse stick to impart force to the lacrosse ball and throws the lacrosse ball from the mesh pocket, more of the force is imparted to the ball in the vertical direction by the lacrosse stick mesh than would be imparted if the lacrosse stick mesh were formed having prior art aperture shapes.

Abstract: A filter well suited for paint arrestor usage having a monolithic high loft manmade fiber body with a convoluted flow contact surface. The filter is preferably formed by a convoluter as in one with a roller set and blade cutter to form mirror image fiber filter sheets from a received fiber batt. Provided is a well mixed proper fiber blend, such as one having a set of fibers made of a majority of course fibers joined by way of thermal bonding fibers which facilitate, during convoluting, formation of a crisp cut and high integrity three dimensional surface, as in one of rows of peaks separated by valleys. The projection/recess arrangement over the flow contact surface as well as the thickness and relative projection-to-base dimensions are arranged to provide a high paint holding capacity without too fast a load up of, for example, paint particles and while avoiding too great of a pressure drop within that load up time.

Abstract: Nonwoven fibrous webs including amorphous polymeric fibers with improved and/or more convenient bondability are disclosed. The nonwoven fibrous webs may include only amorphous polymeric fibers or they may include additional components in addition to amorphous polymeric fibers. The amorphous polymeric fibers within the web may be autogeneously bonded or autogeneously bondable. The amorphous polymeric fibers may be characterized as varying in morphology over the length of continuous fibers so as to provide longitudinal segments that differ from one another in softening characteristics during a selected bonding operation.

Abstract: The present invention provides a system and a method for a portable attachment device. The portable attachment device includes a narrow attachment end, a wide wrap end, a fastening means on the narrow attachment end, a fastening means on the wide wrap end, and padding located within the wide wrap end. The portable attachment device is attachable to a first item by wrapping the narrow attachment end around a portion of the first item and attaching the narrow attachment end to a portion of the wide wrap end, securing the portable attachment device to the item. The first item is then attachable to a second item by wrapping the wide wrap end of the attachment device around the second item. In one embodiment the portable attachment device is used to secure the leg and calf of a wearer to a construction stilt, securely and comfortably holding the leg in place.

Abstract: A method for fabrication of nanometer scale metal fibers, followed by optional further processing into cables, yarns and textiles composed of the primary nanofibers. A multicomponent composite is first formed by drilling a billet of matrix metal, and inserting rods of the metal desired as nanofibers. Hexed or round rods can also be inserted into a matrix metal can. The diameter of this composite is then reduced by mechanical deformation methods. This composite is then cut to shorter lengths and reinserted into another billet of matrix metal, and again the diameter is reduced by mechanical deformation. This process of large scale metal stacking followed by mechanical deformation is repeated until the desired fiber size scale is reached, the fibers being contained in the matrix metal. After size reduction, the composite metal wires may be further processed into built up configurations, depending on intended application, by stranding, cabling, braiding, weaving, knitting, felting, etc.

Abstract: A method and apparatus for forming a bend in composite panel. In one advantageous embodiment, a method is used to form a bend in a composite panel. An angle and a radius bend are identified for the bend. A location of the bend in the composite panel is identified. A slot is cut having a curved flange in the composite panel at the identified location in a single pass through the composite panel with a tool, wherein the curved flange has a shape with a bend allowance width and a bend slot width. The bend allowance width is BA=2?*A/360, wherein BA is the bend allowance width, R is a corner radius, and A is a bend angle. The bend slot width is BS=BA?2K(R?T), wherein K is Tan(A/2) and T is a thickness of the composite panel. The composite panel with the slot is bent to form the bend.

Abstract: A process for manufacturing a bonded sheet with a plurality of coated filaments, which include a ceramic fiber coated with a metal sheath, includes placing the filaments beside one another in one and the same plane, and welding the filaments together by laser spot welding.

Abstract: A process for manufacturing a tubular component with an insert made of a metal matrix composite, within which ceramic fibers extend, includes a draping step, in which a bonded sheet of coated filaments is draped around a metal mandrel. Each filament includes a ceramic fiber coated with a metal sheath, and the filaments are bonded by spot welds.

Abstract: A filtration medium includes a fine filter layer having a plurality of nanofibers and a coarse filter layer having a plurality of microfibers attached to the fine filter layer. The coarse filter layer is positioned proximal to a direction of fluid flow, and the fine filter layer is positioned distal to the direction of fluid flow.

Abstract: A method and device for handling an elongate strength member. In the method, an elongate strength member with a plurality of elongate composite rods, or metal wires or plastic fibers are bundled together with the composite rods, or metal wires, or plastic fibers in a generally parallel and untwisted and un-spiraled arrangement when the elongate strength member is extended along a generally straight path, wherein the composite rods are longitudinally and rotatably moveable relative to each other. It is then twisted relative to a longitudinal dimension of the elongate strength member and the path of the elongate strength member is curved, such as by coiling.

Abstract: A blade or a vane preferably used in a gas turbine engine, the blade or vane being formed of a metallic core or insert with a ceramic airfoil surface bonded to the metallic insert. The insert includes a series of concave and convex portions arranged along the outer surface, in which a plurality of hoop fibers are secured within a resin matrix to firmly secure the metallic insert to the ceramic airfoil body. Axial loads between the insert and the ceramic body are transferred to the hoop fibers. The hoop fibers are strong enough to resist extending in length that would permit the hoop fibers from sliding over the widest portion of the insert.

Abstract: An endoprosthesis that includes a composite having a metal matrix and a plurality of stiffening particles in the matrix. The metal of the metal matrix can include titanium, niobium, tantalum, or alloys thereof The stiffening particles can include a metal core and a thin surface layer. The thin surface layer can include oxides, carbides, nitrides, or combinations thereof.

Abstract: A method of making a hole in a composite material comprising the steps of providing an elongate cutting tool having a cutting portion in the form of a tubular cylinder; and advancing the cutting tool in a direction parallel to a longitudinal axis of the cutting tool whilst rotating the cutting tool about said axis and vibrating the cutting tool along said axis.

Abstract: A recreational surface such as an artificial turf playing field includes a pile fabric having a backing and a multiplicity of generally upstanding pile elements, and an infill overlying the backing and being interspersed between the upstanding pile elements. The infill advantageously includes resilient particles as well as particles of a rubber coated hard granular material such as rubber coated sand. The particles of rubber and the particles of rubber coated sand may be mixed together or they may be applied separately in different courses or layers in which the relative proportions of the two types of particles differ. Also disclosed is a method of designing and constructing such a recreational surface in which the properties of the recreational surface are specified according to the intended use of the recreational surface.

Abstract: A thermal conductor is made of copper and carbon nanotubes powders that are compressed together and then cold rolled into sheets for aligning the carbon nanotubes for providing a composite matrix having a low coefficient of thermal expansion, high thermal conductivity, and high electrical conductivity, for preferred use as a conducting heat sink, such as a laser submount, for heat sinking dissipation and electrical grounding of high-power electrical components and circuits, such as a laser diode.

Abstract: A method for manufacturing a combined driveshaft tube and yoke assembly includes the initial step of orienting a first component having a first wall thickness and a second component having a second wall thickness to define an overlap region. The first and second components may have the same or different wall thicknesses, may be formed from the same or different materials, and may have the same or different lengths. Portions of the first and second components are deformed to provide the overlap region with a third wall thickness that is the sum of the first wall thickness and the second wall thickness. Lastly, a pair of yoke arms having respective openings therethrough is formed in the overlap region to provide a combined driveshaft tube and yoke assembly. A pair of combined driveshaft tube and yoke assembly can also be manufactured in accordance with this method.

Abstract: The invention relates to stainless steel fibers obtained by bundled drawing of stainless steel wires embedded in a matrix material. The composition of the stainless steel fibers comprises iron and the following components expressed in percent by weight: C £ 0.05%, Mn £ 5%, Si £ 2%, 8 £ Ni £ 12%, 15% £ Cr £ 20%, Mo £ 3%, Cu £ 4%, N £ 0.05%, S £ 0.03% and P £ 0.05%. The invention further relates to a method of manufacturing stainless steel fibers.

Abstract: A method of forming a fitting assembly in a filament-reinforced pressure vessel, and a pressure vessel having a fitting assembly secured therein. In the method, a first fitting portion is bonded to an inner surface of a thermoplastic liner in a fluid tight manner. A layer of commingled reinforcing filaments and plastic material is applied to an outer surface of the thermoplastic liner to form a vessel wall. A portion of the vessel wall adjacent to the opening bounded by the fluid-tight seal between the first fitting portion and the inner surface of the thermoplastic liner is removed. Then, a second fitting portion is bonded to the first fitting portion so as to define a port for access into the interior of the vessel.

Abstract: A large surface area electrode well-suited to electrochemical applications is produced by winding many turns of a metallic fiber tow on to a sheet metal rectangle. In the preferred embodiment, an anode that can be used to purify water by electrochemical production of hydroxyl free radical is made by winding titanium fiber tow on to a rectangular substrate made of titanium sheet, and applying a suitable multilayered electrocatalytic coating. Made of other metals, an electrode of this description can also serve as the cathode of an electrochemical cell, or as a battery plaque.

Abstract: An electric traction motor for a vehicle including a housing, a wound stator field located in the housing, a rotor magnetically interacting with the wound stator field, high energy magnets configured in the rotor, and low energy magnets configured in the rotor.

Abstract: A finished laminate is provided. The laminate includes an imperforate metal layer having a metallic surface, and a metallic felt layer having a first surface attached to the metallic surface and an exposed second surface facing away from the metallic surface. Also provided is multi-layer tubing including a thermally conductive metal layer having a metallic surface, and a substantially thermally non-conductive, metallic felt layer having an outer felt layer surface attached to the metallic surface and an exposed inner felt layer surface. The metal layer and the metallic felt layer collectively form a laminate configured as a substantially cylindrical structure with the metallic felt layer positioned radially inward of the metal layer. In certain embodiments, the metal the laminate has opposite side edge portions overlapping and coupled to one another at a coupling portion, without a thermally conductive path through the coupling portion.

Abstract: The present invention provides a method for producing a bending-resistant, elongated body, preferably a shaft or beam. The invention is characterized in that an elongated blank is produced having at least one cavity extending essentially along the entire length of the blank, the inner surface of which cavity is at a distance from the mass center of the blank seen in a section at right angles to its longitudinal axis and that affixed in the cavity is a fiber composite body with an outer surface essentially congruent with the inner surface of the cavity and that majority of the fibers in the fiber composite body both extend essentially parallel to the longitudinal axis of the elongated blank and are elongated along the whole of its length. The invention also relates to an arrangement produced according to the method.

Abstract: The present invention provides a metallic fiber nonwoven fabric manufacturing apparatus mainly including a metallic fiber manufacturing apparatus (7), an ejection nozzle heater (5), a metallic fiber flying apparatus (6), a nonwoven fabric surface density control mechanism, a method for manufacturing an aluminum fiber fabric by using the metallic fiber nonwoven fabric manufacturing apparatus, and a method for manufacturing a laminated aluminum material. By using the metallic fiber nonwoven fabric manufacturing apparatus, manufacture of a high-quality metallic fiber nonwoven fabric and manufacture of an aluminum fiber nonwoven fabric are possible. Further, manufacture of a laminated aluminum material is also possible.

Abstract: A dual lumen catheter system for the positioning of a radioactive material for therapeutic radiation treatment of the body is disclosed. The dual lumen catheter includes a guidewire lumen and a blind lumen provided for introduction of a radiation source wire. The dual lumen catheter provides the advantage that the radiation source wire does not contact body tissue thereby eliminating the need for sterilization of the wire for reuse. Also disclosed are a radiation source wire having a tapered distal end of the wire core such that radioactive material and other components of the source wire can be applied to the outer surface thereof without exceeding a predetermined maximum outside diameter. Also disclosed is a source train cask for use with the catheter system and radiation source wire of the invention. The source train cask permits convenient handling and feeding of the radiation source wire without exposure of the medical personnel to radiation.

Abstract: A tensioning element (1), especially for the suspension of building components, is provided with a number of wires (3) arranged approximately in parallel forming a wire cable (2). These wires (3) are anchored at each end in an end piece (6) absorbing the tensile forces exerted on the wire cable. The end piece (6) is at least partly provided with a plastic deformable sheath (6b) which serves to house one end of a wire cable, where this sheath (6b) is compressible with the end of the wire cable. This enables rapid anchoring of the wire cable in the end piece and this guarantees a high breaking load.

Abstract: Method for manufacturing elements made from composite material using the co-bonding technique, in which uncured elements (preformed beams (2)) are bonded onto another cured element (the skin (3)) with multiple thickness changes, using a rigid tooling made of invar used for support and positioning during the curing process. Each element is made with preimpregnated material using automated tape laying. The preform of the beams (J-section) is obtained by hot forming of flat laminates. The final curing and bonding to the precured skin (co-bonding) is performed using a direct vacuum bag in an autoclave. A flat development of the vacuum bag is performed, it is traced with a numerical control machine and it is made prior to being placed on the tool. For large surfaces with difficult access the final adjustment is performed with the tool and the part in a vertical position, due to the ergonomic difficulties involved in working on certain areas of same. The invention is applicable to the field of aeronautics.