Airbus Operations Sl

José Luis Lozano García

Vicente Martínez Valdegrama

Pedro Nogueroles Viñes

José Orencio Granado Macarrilla

Antonio De Julián Aguado

Gonzalo Ramírez Blanco

Abel Lobo Barros

Jesús Vicente Bajo González

Antonio Francisco Pintor Archilla

Jesús Rodrígues Bodas

Oscar De La Cruz GARCÍA

Method of manufacture of one or more pairs of components in composite material (') intended to form part of aerofoils located on both sides of the axis of symmetry of an aircraft whose shape has a conical tendency in the longitudinal direction, the angle of conicity being less than 10&#xb0;, that comprises the following stages: a) Lay-up of layers on a flat tape lay-up table forming the laminate of a hypothetical component formed by all of the components of said pairs (), the components of each pair being arranged adjacently and the first components () and the second components () of each pair being arranged alternately, and the whole being arranged symmetrically relative to a hypothetical horizontal axis X-X of the tape lay-up jig; b) Cutting of the flat laminates corresponding to each of said components); c) Forming and curing said components.

Method for the manufacture of one or more pairs of components in composite material

A device provides electrical continuity between aeronautical components including a first fixed component and a second component displaceable with respect to the first component. The first and second components include electrically conducting surfaces. A first conductive piece is fixed to the first component and a second conductive piece is fixed to the second component. The first and second pieces are joined together with the possibility of sliding one on the other, in such a way that the first piece is connected to the conductive surface of the first component and the second piece is connected to the conductive surface of the second component, so that, when displacements take place of the second component with respect to the first component, the first piece slides on the second piece maintaining the electrical conductivity between the first and second components.

Device for providing electrical continuity between aeronautical components with relative movement

The lifting surfaces comprise a torsion box capable of bearing aerodynamic and inertial loads. The torsion box has lateral parts that are connected together by an attachment comprising a rib, having a central upper part and a central support lower part joined only by angled cross bars, forming a truss structure along the length of the central support upper part and the central support lower part. The angled cross bars are attached to the upper and the lower parts of the central support: alternatively to both sides of a plane of symmetry defined by said upper and lower parts of the central support, dividing the torsion box in the two lateral parts making a zone of access perpendicular to the length of the central supports, where said zone of access is closed with a piece provided with at least one hole for permanent access.

Integration system for lifting surface lateral parts in an aircraft

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Madrid, Spain

José Luis Lozano García