Patent application number | Description | Published |
20090166921 | Method for Manufacturing a Composite Fiber Component for Aerospace - Method for manufacturing a composite fibre component ( | 07-02-2009 |
20090166935 | Method for Producing a Fiber Composite Component for Aerospace - The invention relates to a method and a moulding core for producing a fibre composite component ( | 07-02-2009 |
20100007044 | METHOD FOR PRODUCING A FIBRE COMPOSITE COMPONENT - Disclosed is a moulding core for producing a fibre composite component, in particular a stringer on a base component in aerospace, of a spiral construction, wherein the moulding core is a hollow profile with an outer geometry adapted to the moulding core and with a slit provided in the wall of the hollow profile and extending spirally around its periphery; and wherein the slit hollow profile is provided with positional fixing, wherein the slit extending spirally around the periphery penetrates the wall of the hollow profile with the exception of at least three locations arranged such that they are distributed around the circumference of the wall of the hollow profile. A method for producing a fibre composite component, such as a fibre composite component for aerospace, is also disclosed. | 01-14-2010 |
20100028480 | Connection Device for a Moulding Core for Producing a Fibre Composite Component, in Particular for Aerospace - The present invention relates to a connection device ( | 02-04-2010 |
20100092708 | Method For Producing A Fibre Composite Component For Aerospace - Method for producing a fibre composite component, in particular for aerospace, having the following method steps: forming a moulding core from a core material with a predetermined narrow melting range in a moulding tool to establish an outer geometry of the moulding core at least partly laying at least one semifinished fibre product on the moulding core that is formed, for the shaping of at least one moulded portion of the fibre composite component to be produced; and multistage exposure of at least the moulded portion to heat and/or pressure to produce the fibre composite component; a corresponding moulding core for producing such a fibre composite component and a corresponding fibre composite component with at least one stringer. | 04-15-2010 |
20110076461 | Method for producing a fibre composite component for aviation and spaceflight - Method for producing a fibre composite component, in particular for aerospace, having the following method steps: forming a moulding core that comprises a predetermined number of hollow bodies for defining an external geometry of the moulding core, the hollow bodies being designed such that they extend in the longitudinal direction of the moulding core and are expandable elastically at least in their lateral direction, and are fixed to one another, the formed moulding core having a flexible outer layer for smoothing the contour of its outer surfaces, and a core sleeve surrounding the moulding core, for sealing the moulding core from the fibre composite component to be produced; placing at least one fibre semi-finished product, at least in places, on the moulding core that has been formed, in order to shape at least one moulding section of the fibre composite component to be produced; and applying heat and/or pressure to the at least one moulding section in order to produce the fibre composite component. | 03-31-2011 |
20110148007 | PROCESS FOR PRODUCING FIBRE PREFORMS - A process for producing fibre preforms for composite material components makes it possible to directly produce complex geometries in a flexible and low-cost manner by applying a plurality of dry fibre rovings independently of one another even in spatially uneven contours. It is no longer necessary to use cut fabric strips since fibre preforms are produced straight from the dry fibre rovings. This obviates the need to carry out production, transport and order picking processes. It is not necessary to cut fibre strips to size, and therefore a saving may be made on material. In addition, it is possible to increase the mechanical characteristic values in the composite material because it is not necessary to sew fibre webs. The described process can also readily be scaled since the number of dry fibre rovings arranged next to one another make it possible to vary the area which can be covered. | 06-23-2011 |
20120279662 | APPARATUS FOR THE PRODUCTION OF AN AIRCRAFT FUSELAGE SHELL CONSISTING OF A FIBRE COMPOSITE - An apparatus for the production of a fuselage shell for an aircraft made of fibre composite, which is to be equipped with a plurality of stringers disposed spaced apart for reinforcement, comprising a main frame to form a supporting substructure having an outwardly curved mounting surface for positive mounting, having longitudinal mounting grooves for receiving of formed parts for deformably positioning the stringers relative to the mounting surface, wherein a plurality of short formed parts spaced apart from each other are disposed in each mounting groove, and which are adjustable relative to the corresponding mounting groove in the transverse direction (Y) by means of adjusters, and which can be raised in the vertical direction (Z) by means of lifters for guiding the stringers in the direction of a laminating adhesive bonding unit brought over the mounting surface. | 11-08-2012 |
20140306372 | Method And Apparatus For Producing A Fiber-Reinforced Plastics Casting - An apparatus and method for producing a fiber-reinforced plastics casting (FRP), includes a moulding box filled with free flowing moulding material, in what a prototype of casting or a textile preform is inserted, forming a mould cavity for infiltration the inserted preform of textile with synthetic resin material in order to form a fiber-reinforced plastics casting (FRP). | 10-16-2014 |