Patent application number | Description | Published |
20100084819 | SURFACE SEAL AS WELL AS METHOD FOR PRODUCING SEALED JOINTS WITH THIS SURFACE SEAL - A surface seal for sealing a riveted and/or screwed joint between a first and a second component of an aircraft. The surface seal is arranged in the region of joining surfaces of the first and the second component. The surface seal is formed with a pressure-resistant plastic film that is provided with a pressure-sensitive adhesive layer on both sides. The surface seal | 04-08-2010 |
20100086804 | FIBRE METAL LAMINATE PANEL - A fibre metal laminate panel with a number of layers, arranged in the form of a laminate, of a planar metal material and a fibre material, the planar metal material being joined at splices by a metal-metal connection to overlapping metal layers, and, in reinforced regions which are used to attach the panel to a support structure with longitudinally extending support elements, additional layers of at least the planar metal material being provided. The additional metal layers reinforcing the panel are formed by overlapping metal-metal connections of the splices. | 04-08-2010 |
20100148004 | Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer - The present invention provides a casing structure of low weight provided with a laminate stringer of high rigidity. The stringer has the form of a laminate with a plurality of metallic layers and at least one synthetic fibre layer, which is produced at least partially from Zylon fibres, provided between two metallic layers. | 06-17-2010 |
20100206987 | Fire Protection Space for Aircraft Passengers Provided with the Aid of Fuselage Skin of Fibre-Metal Laminates - This invention provides a fuselage of an aircraft or space vehicle with a fuselage section having an outer skin, wherein at least the outer skin of the fuselage section consists of a glass-fibre reinforced aluminium laminate to form a safety zone for passengers in the event of a fire. | 08-19-2010 |
20110236711 | STRUCTURAL ELEMENT FOR REINFORCING A FUSELAGE OF AN AIRCRAFT - A structural element for reinforcing a fuselage cell of an aircraft is provided. The structural element comprises a reinforcement profile which is made in one piece from a metallic material. The profile is provided with a strap at least in regions. As a result of the strap which is made of a fibre-reinforced layer material or fibre metal laminate and is adhesively bonded, at least in regions, to a flange of the reinforcement profile the structural element has high damage tolerance and advantageous fatigue properties. The fibre metal laminate or layer material is made of a plurality of metal layers and fibre-reinforced plastics material layers which are stacked in alternating fashion and adhesively bonded to one another over the entire surface. The reinforcement profile and the strap are joined by means of a joining layer. Said joining layer is preferably constructed from two prepreg layers and a non-fibre-reinforced adhesive layer. | 09-29-2011 |
20130196121 | Sheet entity and an aircraft fuselage with a sheet entity of this type - A sheet entity, in particular for use as a skin panel for an aircraft fuselage, with a carbon fibre-reinforced plastic laminate and an aluminum-based metal laminate in the edge region, which are connected with one another by means of an adhesive bond, and thereby are electrically insulated from one another, and are stepped back by layers. Also disclosed is a fuselage cell of an aircraft with at least one sheet entity of this type. | 08-01-2013 |