Abstract: Multi-layered drink-containers including an inner liquid-container and an outer shell in an at least partially overlapping, telescopic relation relative to the inner-liquid-container and methods of assembling the same. In some examples of multi-layered drink-containers, the inner liquid-container includes a lower portion having an outer cross-sectional area, an orthogonal projection of which at least partially overlaps an orthogonal projection of an inner cross-sectional area of an upper portion of the outer shell. Some examples of methods of assembling multi-layered drink-containers include reducing a resiliently deformable restrictive-portion of an inner liquid-container, positioning an outer shell in an at least partially overlapping, telescopic relation relative to the inner liquid-container, and returning the resiliently deformable restrictive-portion to a neutral, un-deformed and un-reduced state.

Abstract: A method and apparatus for forming a batt of particulate material which may be used in an absorbent article. The apparatus may include a vacuum zone, an air impermeable fence zone adjacent to the vacuum zone, and an air permeable fence zone adjacent to the vacuum zone. The air permeable fence zone may comprise an ambient air entry conduit in communication with an ambient air exit port. The method may include providing a laydown drum and a first web of material, positioning the first web of material substantially adjacent to the laydown drum, generating a vacuum through the laydown drum, depositing particulate matter onto the first web of material, and rotating the laydown drum.

Abstract: In a method of manufacturing a blade shell half of a pre-bent wind turbine blade by means of vacuum-assisted resin transfer moulding (VARTM), a fibre lay-up (16) is placed on a mould surface (14) and a distribution layer (24) is placed above the fibre lay-up (16). At least one segmentation area is provided in the distribution layer by providing at least one transversely extending flow barrier in the distribution layer (24) preventing or restricting longitudinal resin flow to the distribution layer. A longitudinally extending first feed channel (27) is placed above the distribution layer (24). The first feed channel (27) is divided into at least two feed channel sections, a feed channel section being arranged in each distribution layer segment. A vacuum bag (43) is arranged on top of the mould part (13) to define a mould cavity. The mould cavity (44) is evacuated and liquid resin is supplied to each feed channel section through a resin inlet to fill the mould cavity and impregnate the fibre lay-up.

Abstract: A vacuum-induced injection molding apparatus is disclosed. The apparatus includes a tool surface having an injection port extending therethrough. A flexible film extends over and is sealingly coupled to the tool surface. The flexible film comprises an outer surface and an inner surface such that the flexible film inner surface and the tool surface define a volume. A vacuum chamber is sealingly coupled to the outer surface of the flexible film. A vacuum port is in fluid communication with the volume. A method of injection molding a polymer matrix composite is also disclosed.

Abstract: A method for fabricating an air-filled cellular structure for use as a resilient cushion. The method includes providing a molding structure including a shelf substantially surrounding a depression, and a platform that fits within the depression and is selectively movable between a plurality of positions relative to the shelf, moving the platform to a preselected position relative to the shelf, wherein the preselected position corresponds to a substantially predetermined amount of air to be contained by the air-filled cellular structure, and using a vacuum device to draw air from within the depression.

Abstract: Disclosed is a method for preparing a multilayer film laminate having a first film layer comprising a perfluorinated copolymer resin layer adhered to a polymeric second film layer that has been surface treated with an aminosilane. The multilayer laminate is useful as a photovoltaic module component. Methods for preparing photovoltaic modules that include the multilayer laminate are also disclosed.

Abstract: Disclosed is a method for preparing a multilayer film laminate having a first layer comprising a perfluorinated copolymer resin layer adhered to a second layer comprising an olefin ester copolymer that has been blended with an organosilane. The multilayer laminate is useful in photovoltaic modules. Methods for preparing photovoltaic modules are also included.

Abstract: A mold and method for vacuum assisted resin transfer molding of a fiber reinforced laminated structure are provided. The mold includes a first mold part and a second mold part. The first mold part defines a negative impression of the laminated structure, being structurally stable and forming a support for fiber reinforcement layers of the laminated structure. The second mold part connectable to the first mold part for closing the mold and defines together with the first mold part an enclosed space which can be evacuated. The mold further includes a flow duct for guiding a liquid polymer which is formed as a recess in the first mold part and/or a recess in the second mold part that is open towards the enclosed space and extends along a section of the periphery of the first mold part and/or the second mold part.

Abstract: The invention concerns an apparatus and a process for the production of a structure from fiber composite material, comprising a mold tool for receiving material which can be joined to provide a structure, and a vacuum system for molding and fixing the structure, wherein the vacuum system has a flexible layer, in particular a separation film or separation layer and/or a tear-off film, and a vacuum film for covering the structure. In accordance with the invention the vacuum system is free from ventilation material and/or tear-off material at least at a portion which corresponds to a portion of the structure to be covered, in which a step extends.

Abstract: A process for bonding aircraft components with a surface, such as an aircraft skin, includes positioning the skin on a tool surface and placing a floorless component on the skin, with bonding agent therebetween. A vacuum bag is placed within the floorless component via a vent in the component, and sealed with opposing inner, lower walls of the component, creating a sealed surface over the skin within the component. Additional vacuum bags seal between lower, exterior legs of the floorless component and either (a) the tool surface (enclosing the skin) or (b) lower walls of adjacent aircraft components. Lower, opposing sides of the adjacent component are also bagged, and loose bag ends are sealed to the tool surface, such that the skin and all feet of the aircraft components are enclosed in vacuum bagging material. The bagged assembly is autoclave cured to bond the aircraft components with the skin.

Abstract: A method of controlling the geometry of a composite component (3). The method comprises applying pressure to the component with a pressure transmitter (6), and during said application of pressure: heating the component; measuring the position of the pressure transmitter to produce a feedback signal; and moving the pressure transmitter in response to a change in the feedback signal.

Abstract: A forming tool (100) for and a method of making a three dimensional composite component using double diaphragm forming. The forming tool (100) comprises a forming side having two or more regions of changing profile and one or more through holes associated with each region, the through holes exit on the forming side and are connectable to one or more vacuum sources such that vacuum can be selectively and discretely applied to each region.

Abstract: Disclosed is a film sticking device that sticks a first film substrate and a second film substrate together on a curved-surface shape. The film sticking device includes a mold having a curved attachment surface formed into a desired curved-surface shape; an attracting and holding unit capable of relatively moving on the curved attachment surface and having plural vacuum chambers on which an attracting surface for attracting and holding the second film substrate is provided; and a suctioning unit capable of separately applying suction processing to the plural vacuum chambers. The suctioning unit starts, as the attracting and holding unit moves, the suction processing of the vacuum chamber corresponding to a position opposing the second film substrate and sequentially stops, as the second film substrate is stuck to the first film substrate, the suction processing of the vacuum chamber corresponding to the stuck second film substrate.

Abstract: An intermediate sealing element and method for unsealing a vacuum membrane from one tool surface and transferring it to another tool surface without damaging the vacuum membrane. The intermediate sealing element forms a continuous path around the periphery of a vacuum membrane and is sealed directly to one or more vacuum membranes and a tool surface using any means known in the art to create an airtight seal between two surfaces. The intermediate sealing element is able to withstand high temperatures and high pressure without altering its structural characteristics. Because of its durability, the intermediate sealing element can be removed from the tool surface without tearing or elongating, subsequently allowing the vacuum membranes to be detached from the tool surface without tearing or elongating.

Abstract: In a method for reinforcing a fiber composite component for aviation and space flight, a vacuum mat is configured with at least one receiving portion for reproducibly receiving at least one reinforcing element. The at least one reinforcing element is introduced into the at least one receiving portion of the vacuum mat. The vacuum mat with at least one introduced reinforcing element is applied reproducibly in a sealed manner to the fiber composite component to be reinforced to form a mold portion and at least the formed mold portion is cured to connect the at least one reinforcing element to the fiber composite component. The vacuum mat is then removed from the reinforced fiber composite component so that the vacuum mat can be reused.

Abstract: An acrylic resin film material comprising at least a multilayer structure polymer with a particular structure prevent a molded item from being whitened during insert- or in-mold molding and meet the requirement for surface hardness, heat resistance, and transparency or matting performance for vehicle applications. It is also possible to use an acrylic resin film material exhibiting a difference of 30% or less between haze values as determined in accordance with the testing method of JIS K7136 (haze measurement method) after and before a tensile test where a test piece with a width of 20 mm is pulled under the conditions of an initial inter-chuck distance of 25 mm, a rate of 50 mm/min and a temperature of 23° C. until an end-point inter-chuck distance becomes 33 mm as well as having a pencil hardness of 2 B or higher as determined in accordance with JIS K5400.

Abstract: A reinforcement insert includes superposed laps of fiber which are coupled to each other by a coupling fiber which passes through the laps in order to form fiber sections wherein at least certain sections thereof are rectilinear. The fiber sections and laps are immersed in a cured resin. The total density of the fibers that make up the insert ranges from 50% to 60% of the volume of the insert and the fiber sections take up 3%-10% of the volume of the insert. A method for creating a sandwich structure includes at least one such insert.

Abstract: A method for performing resin infusion into a dry reinforcement on a layup mandrel comprises placing resin at a resin zone on the mandrel; bagging the reinforcement and the resin with a bagging film; heating the resin while applying compaction pressure to the bagging film to cause the resin to be infused into the reinforcement; and creating a pressure differential outside of the bagging film over the resin zone to control rate and pressure at which the resin is infused into the reinforcement. As a result, the resin pressure and infusion rate are controlled independently of the compaction pressure on the reinforcement.

Abstract: The invention relates to a part (11) made of a composite formed from a thermosetting resin, which includes lightning protection element including, on an upper surface (12) of the part (11) liable to be exposed to lightning strikes, a continuous layer of a metal foil (1) having perforations (2) with a degree of perforation between 0.005% and 20%.

Abstract: An apparatus and method for forming a fiber reinforced resin composite component by a resin transfer infusion (RTI) process in which a preform is laid up on a hard base tool and a bagging blanket is applied as a flexible upper tooling. Edge and/or other regions of the preform are superimposed by localized control plates which, together with spacer pins passing through the preform, serve to determine localized dimensional accuracy in the component without the need for hard upper tooling throughout.

Abstract: A method for manufacturing an elongate stiffening element and a rigid shell structure integrated with at least one elongate stiffening element. The method includes providing a preformed, form-stable reinforcement member, which has a hat profile with two inwardly directed, opposing flange portions, covering the reinforcement member with a curable composite material to form an external hat profile having outwardly directed flanges, and integrating this assembly with either a curable or preformed shell structure of composite material.

Abstract: A method for making a honeycomb composite structure wherein the method allows for fluid flow from cells of a honeycomb core during a cure process. More specifically, the method involves forming one or more vents in a skin of the structure, which are preferably filled with venting wicks, to allow for fluid flow before being sealed by the polymer matrix during a skin bonding process. Additionally, the structure preferably comprises a scrim that allows for fluid flow between multiple cells of the honeycomb core. The honeycomb composite structure produced according to this process comprises, among other things, a sealed venting region that comprises a polymer matrix and fibers that are transverse to the skin.

Abstract: The present invention relates to a horizontal molding method and apparatus of an interior material of a vehicle.

Abstract: A method for producing an aortic or mitral heart valve prosthesis and the resulting aortic or mitral heart valve. The method is characterized in that it essentially consists in producing the prosthesis by shaping a textile material. The invention is more particularly applicable in the field of medicine, in particular repair surgery, and especially in heart surgery, more particularly heart prostheses.

Abstract: The present invention relates to a radome which has excellent transmission loss of radio waves and structural strength, which can be easily produced, and which has favorable workability, and a method of producing the same. The radome includes an olefin woven material and a glass cloth, in which the olefin woven material and the glass cloth are impregnated with a matrix resin to be integrated with each other, and the glass cloth is disposed closer to an inner side of the radome than the olefin woven material. As the olefin woven material, a woven material formed of an ultrahigh molecular weight polyethylene fiber can be used. As the matrix resin, an epoxy resin, a vinyl ester resin, an unsaturated polyester resin, or a silicone resin can be used.

Abstract: The invention relates to a manufacturing method for hollow components using a tubular film (1) and a mould (3) having the following steps: feeding a plastic material in the area of an inner surface (4a, 4b) of the mould (3), conforming the material to the inner surface (4a, 4b) of the mould (3), feeding a tubular film (1) into the mould (3) so that the material is positioned between an outer surface of the tubular film (1) and the mould (3), expanding the tubular film (1) using pressure and/or a vacuum, applying a pressure (p) above atmospheric pressure and/or heating the mould so that the material is partly or completely melted and is adapted to conform to an inner contour of the mould (3) and an outer contour of the expanded tubular film (1).

Abstract: A method of producing a panel having at least one feature comprising a discontinuation in curvature of surface in the surface, the method comprising the steps of: providing a first reinforced layer of long and/or continuous parallel fiber reinforced thermoplastic of a first polymer (102a, 104a); providing a core layer of thermoplastic with at least roughly 70% by volume of a second polymer which is compatible with the first polymer (106); providing a second reinforced layer of long or continuous parallel fiber reinforced thermoplastic of the first polymer (102b, 104b); stacking the layers such that the reinforced layers are separated by the core layer; introducing the stack into a panel mould and heating the mould to at least the melting point of the predetermined polymer to consolidate the layers and form the panel.

Abstract: Disclosed is a folding and shape-forming apparatus for a prepreg which includes a vacuum chamber which can generate a vacuum pressure in the inside thereof, an expanding portion disposed inside the vacuum chamber, provided with a prepreg thereon, and expanding because of the vacuum pressure inside the vacuum chamber, a heating portion disposed inside the vacuum chamber for heating the prepreg, a mandrel loaded at a portion of an upper surface of the prepreg, a first pressing portion which is brought into contact with an upper surface of the mandrel to press the mandrel, and a second pressing portion which simultaneously presses both another portion of the upper surface of the prepreg and the expanding portion.

Abstract: A mold and method for vacuum assisted resin transfer molding of a fiber reinforced laminated structure are provided. The mold includes a first mold part and a second mold part. The first mold part defines a negative impression of the laminated structure, being structurally stable and forming a support for fiber reinforcement layers of the laminated structure. The second mold part connectable to the first mold part for closing the mold and defines together with the first mold part an enclosed space which can be evacuated. The mold further includes a flow duct for guiding a liquid polymer which is formed as a recess in the first mold part and/or a recess in the second mold part that is open towards the enclosed space and extends along a section of the periphery of the first mold part and/or the second mold part.

Abstract: A method of forming a composite article having a decal occurs in a mold. The mold includes a surface that defines a mold cavity. A decal is introduced to the surface of the mold. A polyurethane elastomer composition is applied into the mold cavity to form an elastomeric layer over the decal. The composite article including the elastomeric layer and the decal may then be demolded from the mold. Alternatively, a paint composition is applied into the mold cavity to form a paint layer over the decal. The polyurethane elastomer composition is applied into the mold cavity to form an elastomeric backing layer over the paint layer. The composite article including the paint layer, the decal, and the elastomeric backing layer may then be demolded from the mold. The composite article may be a seat for an all-terrain vehicle.

Abstract: A method is provided for making a composite laminate aircraft skin for a fuselage in multiple composite panels. A resin-impregnated composite tape is placed on a lay-up surface of a mandrel tool to form the composite laminate aircraft skin as a barrel that is substantially the shape of a fuselage section. The barrel is cut into a plurality of panels on the mandrel tool, and at least one panel of the plurality of panels is transferred, individually and independently of all other of the plurality of panels, from the lay-up surface of the mandrel tool to a first cure tool of a plurality of cure tools having an aero surface tooled to an outer mold line. The at least one of the panels is cured on the first cure tool to form a cured composite panel. The first cure tool defines and controls the outer mold line of the at least one panel. The cured composite panel is removed from the first cure tool.

Abstract: A method and apparatus for forming a wad of particulate material which may be used in an absorbent article. The apparatus may include a laydown drum having a plurality of vacuum zones, a plurality of fence zones, and a plurality of blow-off zones. The plurality of vacuum zones may be substantially permeable to permit vacuum air to pass through and into the laydown drum. The plurality of fence zones may be substantially impermeable to inhibit air to pass through. The plurality of blow-off zones may be substantially permeable to permit blown air to pass out of and through said laydown drum. The apparatus may also include a deposition chute for depositing particulate material on a web of material in close proximity to the laydown drum. A shield may also be attached to the deposition chute.

Abstract: Disclosed is a composition for biodegradable starch bowl consisting of unmodified starch of 20-60 wt. %, pulp fiber powder of 5-30 wt. %, solvent of 30-60 wt. %, photo catalyst of 0.1-2.0 wt. %, preservative of 0.01-1 wt. % and releasing agent of 0.5-5 wt. %. In the present invention, further disclosed is a biodegradable starch bowl being prepared by heating and pressurizing said composition for biodegradable starch bowl so as to have a desired shape. The composition for a biodegradable starch bowl and the biodegradable starch bowl using the same according to the present invention have improved sterilizing, deodorizing, preservative and releasing properties.

Abstract: A cured sandwiched article may be used to enhance a portion of a vehicle. In some embodiments, a cured sandwiched article may include a core sandwiched between one or more backing layers and one or more top layers cured to conform to a surface of a vehicle. A cured sandwiched article may be made by steps including shaping a core, positioning the core between one or more backing layers and one or more top layers to form the sandwiched article, and curing the sandwiched article. A cured sandwiched article may be connected to a surface of a vehicle by providing adhesive to a bottom surface of the cured sandwiched article, positioning the cured sandwiched article on a surface of the vehicle, and curing the adhesive. In some embodiments, the cured sandwiched article may include a plurality of fiber-optic fibers.

Abstract: An apparatus and method of forming a stringer or an integral stringer and fuselage skin. The apparatus may be a solid bladder made of silicone, urethane, or any similar material or combination thereof. The method may comprise placing composite material onto a surface of a tooling having a channel sized and shaped to correspond to a desired stringer size and shape. Then the solid bladder may be placed onto the composite material relative the channel. The shape of the solid bladder may correspond to the shape of the channel. Composite material may then be placed over the solid bladder, vacuum-sealed against the bladder and the tooling, and cured to harden the composite material, thereby forming a stringer or an integral stringer and fuselage skin.

Abstract: A method and apparatus for encapsulating items such as electronic devices. A mold material is dispensed onto the electronic device and the device is situated between first and second molds. One mold is moved towards the other so as to vary the size of a cavity defined by the first and second molds. A vacuum is applied to the cavity and the vacuum is varied in response to the size of the cavity. The vacuum can be varied in response to a predetermined vacuum profile. For example, in certain embodiments the vacuum is varied in response to the position of the first mold relative to the second mold, wherein the vacuum is increased as the cavity height is reduced.

Abstract: A method for making a preform includes creating a pressure differential between an inside and an outside of a perforated shape memory polymer mandrel in its temporary shape. The pressure differential is such that pressure outside the perforated shape memory polymer mandrel is greater than pressure inside the perforated shape memory polymer mandrel. The perforated shape memory polymer mandrel has i) a predetermined preform shape as the temporary shape and ii) a shrunken shape as its permanent shape, wherein the shrunken shape is configured such that it is removable from the predetermined preform shape. The method further includes depositing, as the pressure differential is maintained, at least one material onto a surface of the perforated shape memory polymer mandrel. The at least one material is set in the predetermined preform shape, thereby forming the preform.

Abstract: A method and apparatus for forming a batt of particulate material which may be used in an absorbent article. The apparatus may include a vacuum zone, an air impermeable fence zone adjacent to the vacuum zone, and an air permeable fence zone adjacent to the vacuum zone. The air permeable fence zone may comprise an ambient air entry conduit in communication with an ambient air exit port. The method may include providing a laydown drum and a first web of material, positioning the first web of material substantially adjacent to the laydown drum, generating a vacuum through the laydown drum, depositing particulate matter onto the first web of material, and rotating the laydown drum.

Abstract: A vacuum mandrel for use in fabricating an implantable electrode comprises a hollow body member and a first groove provided radially on an outer surface of the hollow body member. The first groove is adapted to receive an implantable electrode and retain the electrode in place with a vacuum pressure during an elastomeric encapsulation of the electrode. The vacuum mandrel further comprises a vacuum port provided in the first groove.

Abstract: A method for manufacturing a composite is provided. A first fibre mat is laid onto an inner surface of a mould. Suction is applied between the inner surface of the mould and the first fibre mat. A second fibre mat is laid over the first fibre mat, wherein the second fibre mat is covered with a vacuum bag. Vacuum is introduced between the vacuum bag and the mould and resin is injected under vacuum between the vacuum bag and the mould. After the resin is set, the mould will be removed.

Abstract: A method of making a fenestration framing member includes providing a core of size and shape corresponding to the desired size and shape of the fenestration framing members. A fiberglass mat is placed on the core to form a fiberglass-engaged core, and resin is vacuum infused into the mat to form a fenestration framing member that includes fiberglass-reinforced resin engaging the core. The starting core and the final fenestration framing member preferably are of curved geometry lengthwise of the core and member. The step of vacuum infusing resin into the mat surrounding the core preferably is carried out by placing the fiberglass-engaged core into a vacuum enclosure, preferably a vacuum bag, and connecting the vacuum enclosure to a vacuum source and a resin source. In one embodiment of the disclosure, the mat surrounds the core so that the core is part of the fenestration framing member.

Abstract: A method includes heating a thermoplastic sheet to a predetermined temperature, and placing the heated sheet between a male die and a female die. The female die has a grain pattern on an inner surface thereof and a plurality of minute holes extending therethrough. The method further includes closing the male die and the female die to press the sheet against the inner surface of the female die, drawing the sheet to the female die by vacuum pressure through the plurality of minute holes, and thereby the grain pattern on the female die is transferred to the sheet. After that, thermoplastic molten plastic material is injected into a space between the laminate material and the male die, and is cooled down so that the plastic product is formed by integrating the sheet and the injected material.

Abstract: A process for making a fiberglass chipper body. The process includes first providing a mold having a flange extending around an outside periphery of the mold. Next, the mold is coated with a gel-coat layer. At least one layer of fiberglass is then placed onto the mold over the gel-coat layer. The next step is to place a cover over the mold to completely cover the fiberglass. Breather strips are then inserted around the outside periphery of the mold, a plenum is placed onto the mold flange, and a vacuum is attached to the plenum. Once a resin is injected through the cover into the fiberglass, the fiberglass is cured under vacuum before the fiberglass chipper body is removed from the mold.

Abstract: To fabricate a composite item from a layup of composite material, the layup is degassed, debulked, and cured. To degas the layup, an envelope pressure within an envelope that includes the layup is reduced, a chamber pressure within a chamber that includes the envelope is reduced, and the layup is heated. To debulk the layup, the chamber pressure is increased relative to the envelope pressure so that the envelope exerts a compressive force upon the layup in response to the relatively higher chamber pressure as compared to the envelope pressure. To cure the layup, the layup is exposed to radiation.

Abstract: Load-bearing articles are manufactured from shape defining compressible cores and thermoplastic shells. The manufacture of these articles requires specific methods and tools. Articles that can be manufactured using these methods include relatively lightweight pallets with high load-bearing capacity.

Abstract: A mask is used to make an article having two or more layers. The layers are formed from either a paint or polyurethane elastomer composition. The article is made in a mold including a surface defining a mold cavity and having a first and second effect region. For the method, a mask is placed into the mold cavity adjacent the first effect region. Pressure is applied to the mask to retain the mask adjacent the first effect region. A first composition is applied into the mold cavity to form a first layer adjacent the second effect region. The mask is removed from the first effect region. A second composition is applied into the mold cavity to form a second layer adjacent the first effect region. Benefits of pressure applied to a mask are also realized when making the article from a preformed part using the mask outside of a mold.

Abstract: Process for manufacturing monolithic composite structures comprising providing first and second subcomponents (1, 2) of composite material, attaching an expansion compensating tooling to the second subcomponent, placing the second subcomponent along with said tooling on the first subcomponent and bonding it to the latter by means of an uncured structural adhesive, covering the assembly comprising the first and second subcomponents and the tooling with a vacuum bag, performing an autoclave cycle for curing the curable material contained in said assembly under high temperature and pressure conditions, withdrawing said assembly from the curing autoclave and removing the expansion compensating tooling to obtain the desired monolithic composite structure. The tooling for carrying out the process comprises metal L- or I-shaped beams having a rough surface adapted to be applied to the second subcomponent. The invention is useful for manufacturing aircraft parts.

Abstract: The present invention relates to a method for producing a composite structure comprising fibre reinforced material by means of vacuum assisted resin transfer moulding, where fibre material is impregnated with liquid resin. The method comprises an evacuation process of a mould cavity by initially providing an under-pressure in a part of the mould cavity in order to provide a first vacuum front having a first pressure gradient oriented towards a first side of the forming structure, and a second vacuum front with a second pressure gradient oriented towards a second side of the forming structure, and controlling the first vacuum front and the second front to move towards the first side and the second side of the forming structure, respectively.

Abstract: The invention provides methods and apparatus for producing flexible, stretchable, and/or elastic products comprised principally of material such as natural elastomers and other synthetic polymers. The method and apparatus for producing stretchable products by spraying product material over a workpiece former, and method and apparatus for creating perforated products by spraying product material over a perforated surface or partly breathable surface, The invention also provides methods and apparatus for making double sided fibre coating of the product and, or to at least coating the product surface on the side facing the wall without the need for removing the product from the wall. The method and apparatus also enable easy removal of the product from the former. Workpiece formers are also provided.

Abstract: A use of a core block for an impregnation process as well as a composite structure comprising such a core block is described. The core block has a first surface and a second surface, and a number of first grooves is formed in the first surface of the core. Furthermore, a number of second grooves is formed in the second surface of the core. The first grooves have a first height (h1) and a bottom, and the first grooves and the second grooves are part of a resin distribution network formed in the core block. The distance (t) between the bottom of the first grooves and the second surface of the core block is of such a size that the core block is flexible along the first grooves. Additionally, the sum of the first height and the second height is larger than the thickness of the core block, and at least one of the first grooves in the first surface of the core block crosses at least one of the second grooves in the second surface of the core block.