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WO/2010/040004 |
A composite truss structure (20) employs a sandwich-in-sandwich construction in which a composite fluted core (26) is sandwiched between two facesheets (22,24), and at least one structural foam stiffener (28) is sandwiched within the cor...
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WO/2010/037964 |
The invention relates to a panel assembly for an aircraft fuselage, in which a first panel (10) and a second panel (20) respectively have a first end portion (11) and a second end portion (21) overlapping one another and connected to one...
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WO/2010/037762 |
The invention provides a method of making a tubular element for a wind turbine blade where at least two sections of the blade are assembled to form the tubular element, e.g. a spar or a blade shell. According to the invention, the sectio...
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WO/2010/037612 |
The invention relates to a device (1, 15) for automatically laying and draping a plurality of portions in web form (8, 25, 45, 54) of a dry sheet-like formation (55), in particular of a multiaxial laid fibre fabric and/or a woven reinfor...
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WO/2010/037991 |
In the formation of a fibre reinforced composite material component (10) produced by a resin transfer infusion process such as to have an electrically conductive surface layer (11) for lightning strike protection wherein the component is...
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WO/2010/039377 |
A process for producing composite structures (10) having a core (14) between resin- impregnated composite layers (18), and composite structures formed by such a process. The process uses non-impregnated fabric layers (18) and a core laye...
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WO/2010/034594 |
In a fiber composite component for energy absorption in the event of a crash for an aircraft or spacecraft, the fiber composite component is designed as a laminate structure made from carbon fiber layers (4, 5, 7) and at least one integr...
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WO/2010/034755 |
Use of a composite article as spar component, the composite article comprising a panel (10) comprising a layer of a foamed plastic material (1), mounted between an upper (2) and a lower (3) layer of a fibrous reinforcing material, the pa...
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WO/2010/036406 |
The present invention relates to a method for producing fiber composites impregnated with a thermoplastic resin to be used as stab and ballistic composite structures. If compared with the manufacturing processes of the state of the art, ...
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WO/2010/035125 |
The invention relates to a manufacturing method for hollow components using a film hose (1) and a molding tool (3), comprising the following steps: Introducing a plastic tool in the area of an inner surface (4a, 4b) of the molding tool (...
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WO/2010/034771 |
The invention relates to the use of low molecular mass, non-evolutive polyamide resins for making composite articles. The articles have good mechanical properties, such as rigidity, breaking load, impact resistance, and fatigue behaviour...
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WO/2010/034283 |
The invention relates to a rotor blade for a wind energy installation, comprising at least one flange extending longitudinally from the base of a rotor blade to the tip of the rotor blade, the flange tapering off in the longitudinal dire...
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WO/2010/032048 |
The present invention provides a polymeric article formed from oriented polymeric strands (52) made using a hot compaction process and in which layers of said strands are lain one-on-top of the other and the bond therebetween is improved...
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WO/2010/031364 |
In a method for producing composite material components, thermoplastic prepreg ribbons (1) are placed onto a deposit surface of a composite material component (2) to be finished, heated by laser radiation (3) and pressed on using a conta...
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WO/2010/028720 |
The invention relates to a load-bearing structural fiber composite component which is produced of exactly intermeshing individual elements which define cavities in between them, said elements being preforms of layered semi-finished fiber...
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WO/2010/028720 |
The invention relates to a load-bearing structural fiber composite component which is produced of exactly intermeshing individual elements which define cavities in between them, said elements being preforms of layered semi-finished fiber...
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WO/2010/026054 |
The invention relates to a sandwich plate (19) comprising a core structure, in particular a honeycomb-like core structure (20), and on both sides thereof plane-parallel cover layers (21, 25) for forming a floor surface in a fuselage cell...
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WO/2010/025495 |
A method of molding a fibre-reinforced composite wheel using a mold assembly. The mold assembly includes an annular rim mold portion for defining an outer surface of a rim of the wheel and a disc mold portion for defining a front surface...
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WO/2010/027661 |
A method of forming an introducer sheath having a crease-free tapered distal tip portion. A mandrel is provided having an outer configuration comprising an elongated body and a tapered distal tip portion. A generally tubular inner liner ...
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WO/2010/026411 |
A method of assembling and shaping a laminate panel. An intermediate member is mounted on a lay-up table and a lay-up is assembling by laying a series of plies onto the intermediate member on the lay-up table. The intermediate member and...
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WO/2010/027661 |
A method of forming an introducer sheath having a crease-free tapered distal tip portion. A mandrel is provided having an outer configuration comprising an elongated body and a tapered distal tip portion. A generally tubular inner liner ...
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WO/2010/026411 |
A method of assembling and shaping a laminate panel. An intermediate member (3) is mounted on a lay-up table (4) and a lay-up is assembling by laying a series of plies onto the intermediate member (3) on the lay-up table (4). The interme...
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WO/2010/024990 |
A composite tie rod comprises an open lattice body formed of interlaced filaments held in a solid matrix. A pair of fittings rigidly connect rod ends with the ends of the body. The rod ends form attachment points on the tie rod.
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WO/2010/023476 |
A tubular element (1) adapted for use downhole in drilling and oil & gas prospecting comprises a metallic mandrel (6) adapted to be connected (2,3) within a string of elongate elements, with a GRP(GFK) composite material (7) upon an oute...
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WO/2010/025413 |
The shape of a laminated composite structure is optimized using finite element analysis. The optimized shape minimizes the weight of the structure while satisfying minimum strength and stiffness requirements.
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WO/2010/023476 |
A tubular element (1) adapted for use downhole in drilling and oil & gas prospecting comprises a metallic mandrel (6) adapted to be connected (2,3) within a string of elongate elements, with a GRP(GFK) composite material (7) upon an oute...
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WO/2010/025413 |
The shape of a laminated composite structure is optimized using finite element analysis. The optimized shape minimizes the weight of the structure while satisfying minimum strength and stiffness requirements.
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WO/2010/020237 |
It is desirable in many uses of fiber composite components to have improved properties (e.g. fire resistance) which are often impossible or difficult to obtain by means of conventional matrix materials (e.g. epoxy resin systems). The inv...
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WO/2010/020237 |
It is desirable in many uses of fiber composite components to have improved properties (e.g. fire resistance) which are often impossible or difficult to obtain by means of conventional matrix materials (e.g. epoxy resin systems). The inv...
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WO/2010/019697 |
A method for forming a resin-fiber composite shell includes introducing a resin-fiber pre-preg packet between a rigid cavity (10) and a rigid core (22). A flexible member (24) is introduced between the rigid cavity and the rigid core. Th...
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WO/2010/018292 |
Protection for elements (1) made from composite material that are protected where the geometry thereof is complex, e.g. borders, ridges, edges and corners, against electrical discharges to which those elements are potentially exposed, sa...
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WO/2010/019948 |
A method and system for fabricating a geometrically versatile composite lattice support structure having a seamless three-dimensional configuration is disclosed. The lattice support structure can be created by forming two or more cross s...
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WO/2010/019966 |
A method and system for fabricating a geometrically versatile composite lattice support structure having a seamless three-dimensional configuration. The lattice support structure is created by forming two or more cross supports, such as ...
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WO/2010/019948 |
A method and system for fabricating a geometrically versatile composite lattice support structure having a seamless three-dimensional configuration is disclosed. The lattice support structure can be created by forming two or more cross s...
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WO/2010/019966 |
A method and system for fabricating a geometrically versatile composite lattice support structure having a seamless three-dimensional configuration. The lattice support structure is created by forming two or more cross supports, such as ...
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WO/2010/018094 |
The present invention relates to a substrate-free conductive surface covering, and a process to manufacture such covering, said surface covering comprising a core layer of sheet particles which are agglomerated and embedded in a polymer ...
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WO/2010/018094 |
The present invention relates to a substrate-free conductive surface covering, and a process to manufacture such covering, said surface covering comprising a core layer of sheet particles which are agglomerated and embedded in a polymer ...
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WO/2010/018229 |
A method of manufacturing a wind turbine blade shell part comprising fibre material impregnated with cured resin is described. The method comprises the steps of : a) providing a first mould part (110) having a first forming surface (112)...
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WO/2010/016756 |
The invention relates to a method for manufacturing a semi-finished product. The method comprises the steps of positioning a plurality of elongated reinforcing elements, excluding drawn polyethylene reinforcing elements, onto a mandrel, ...
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WO/2010/016834 |
A method of manufacturing a polymer foam composite is described, the method comprising forming an article having a first surface and an opposite second surface from a precursor composition, the precursor composition comprising a polymer ...
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WO/2010/016756 |
The invention relates to a method for manufacturing a semi-finished product. The method comprises the steps of positioning a plurality of elongated reinforcing elements, excluding drawn polyethylene reinforcing elements, onto a mandrel, ...
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WO/2010/015783 |
The subject of the invention is a method for producing a component made of a composite material comprising a fibre preform (50) embedded in a matrix, consisting in placing said preform (50) in a first enclosure (54) bounded by a first wa...
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WO/2010/015782 |
The invention relates to a device (32; 58) for supplying a rubber band (10), comprising: a spool (42) of product around which are wound the rubber band (10) and an intermediate band (12) on which the rubber band (10) is carried; a drive ...
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WO/2010/015782 |
The invention relates to a device (32; 58) for supplying a rubber band (10), comprising: a spool (42) of product around which are wound the rubber band (10) and an intermediate band (12) on which the rubber band (10) is carried; a drive ...
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WO/2010/012348 |
The invention relates to a process for producing a composite component (100), said process comprising the following steps: 1.1 a decorative composition (110) is produced from at least one backing layer (114) and at least one colour-impar...
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WO/2010/013085 |
Flame-retarding arrangement for reinforced-plastic boats which may be of two kinds: 1.1 Solid laminate arrangement formed by various layers of reinforced plastic with flame-retarding additives, with a coating of intumescent paint; or, 1....
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WO/2010/013029 |
A method of manufacturing a composite element and an apparatus therefore. A stack of plies (1) is assembled on a lay-up table, each ply comprising a plurality of reinforcement elements such as thy-fibres. A first part of the stack of pli...
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WO/2010/012348 |
The invention relates to a process for producing a composite component (100), said process comprising the following steps: 1.1 a decorative composition (110) is produced from at least one backing layer (114) and at least one colour-impar...
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WO/2010/012348 |
The invention relates to a process for producing a composite component (100), said process comprising the following steps: 1.1 a decorative composition (110) is produced from at least one backing layer (114) and at least one colour-impar...
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WO/2010/014107 |
Methods for preparing carbon nanotube layers are disclosed herein. Carbon nanotube layers may be films, ribbons, and sheets. The methods comprise preparing an aligned carbon nanotube array and compressing the array with a roller to creat...
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