Abstract: The main purpose of the invention is a device for manufacturing a composite part, comprising a mould, designed to be associated with a reinforcement of the composite part comprising a preform, into which the resin forming the matrix of the composite part will be injected, possibly a support element on which the mould is supported, a preform vacuum creation membrane supported on the mould and/or the support element, if there is one; characterised in that it also comprises a vacuum chamber covering the vacuum creation membrane, the vacuum chamber comprising a flexible wall designed to apply a mechanical pressure to the vacuum creation membrane.

Abstract: A storage compartment is provided for a transportation means, for mounting in an overhead region. The storage compartment includes, but is not limited to a universal housing module and a transformable container module. Various container modules, in particular fixed bins and pivot bins, can be installed in the universal housing module without this requiring any alteration of the housing module. The transformable container module can be converted within the housing module from a state as a fixed container to a state as a movable chute.

Abstract: A system for managing a user's access rights to avionic information, loaded on board an aircraft, that includes at least one identification device able to read the user's identity information contained on a personal card, and an avionic computer having means of managing access rights able to authenticate the user and determine access rights to avionic information based on the user's identity.

Abstract: An avionic system for an aircraft including at least two pieces of equipment which can exchange information by means of at least one electrical bus for simultaneous bidirectional communication, in which the information can be exchanged between pieces of equipment via an optical bus that can be connected to the electrical interfaces of the equipment. The optical bus of the avionic system includes at least one optical cable having at least one optical fiber and, at each end, a connector having means for converting electrical signals into optical signals and means for converting optical signals into electrical signals. The optical bus is connected to the electrical outlets of existing equipment.

Abstract: The invention relates to a curtain support assembly to receive a curtain rail for a curtain for separating at least two regions in a cabin of a vehicle, comprising one or several header components for covering a space formed between the curtain rail and a ceiling in the cabin. The assembly according to the invention comprises one or several load-bearing frame structures, each comprising at least one profile component, on which in each case on at least one side the header components are arranged. The frame structure may be made from standard components and may comprise header components that are hardly subjected to any mechanical loads and that are therefore less demanding to produce.

Abstract: The invention relates to a method for producing a composite component reinforced by stiffening elements. Composite component is produced by the inside gluing of a monolithic component to a multiplicity of stiffening elements by means of an adhesive suitable for this particular application. Stiffening elements are formed with a fiber reinforced, amorphous thermoplastic material. Monolithic component of composite component consists of a fiber reinforced duroplastic material—for example a composite epoxy matrix—in which are embedded, for reinforcement, carbon fibers, basalt fibers, natural fibers, ceramic fibers, Aramide® fibers, Kevlar® fibers or any combination thereof. Monolithic component is glued to thermoplastic stiffening elements by an adhesive under the influence of pressure and temperature. Here a tolerance compensation is carried out essentially by stiffening elements, if necessary being plastically deformed, so that high dimensional stability is achieved.

Abstract: An oxygen supply system is provided for generating oxygen from cabin air in an aircraft. The oxygen supply system exhibits a modular cabin unit with an oxygen port and a decentralized oxygen supply unit with an oxygen outlet, and the decentralized oxygen supply unit is set up in the modular cabin unit. The decentralized oxygen supply unit is set up to generate oxygen-enriched air from the cabin air by means of electrical power, and the oxygen-enriched air can be provided to the oxygen port of the modular cabin unit via the oxygen outlet.

Abstract: A process for the production of a stiffener made of composite material that includes a central part with wings on both sides such that when the wings are resting against an element to be reinforced, the central part is separated from the element to be reinforced, with the process including producing a flat strip (16) that includes at least one layer of fibers, placing it on a mold (26) that includes at least one hollow shape that corresponds to the central part of the stiffener that is to be produced, heating the strip (16), and deforming it in such a way as to make it assume the shapes of the mold (26), characterized in that it includes exerting a transverse traction on the strip (16) during the deformation of the strip.

Abstract: The present invention relates to a system (1) and an associated method for managing audio warning messages in an aircraft. The system (1) comprises a plurality of monitoring systems (10, 20) capable of detecting the establishment of at least one warning condition (CA), and comprises a central broadcasting module (40), to which each of the monitoring systems is connected and which is capable of broadcasting an audio message (SIG) corresponding to a detected warning condition. In particular, in this system (1), the said central broadcasting module (40) comprises means (402, 420) for determining at least one priority warning condition among the warning conditions detected by the monitoring systems, and means (410, 430) for generating at least one audio message (SIG) corresponding to the at least one determined priority warning condition, in order to broadcast it.

Abstract: A storage system for an emergency apparatus provided in a conveyance includes at least one structure-holder connectable to a structural component of the conveyance. A frame is attached to the at least one structure-holder, and a carrier is configured to receive the emergency apparatus. A locking apparatus has a locking position in which the carrier is fastened to the frame, and an unlocking position in which the carrier is detached from the frame. A belt element is fixedly connected to the carrier. A first end of a retaining belt is connectable to a structural component of the conveyance via a belt-winder, and a second end of the retaining belt is fastenable in a detachable manner via a belt lock to the belt element.

Abstract: A method for obtaining the inertial properties of a movable rotating around a hinge line in an aircraft control surface. The method includes the steps of removing the mechanical connections of the actuators from the movable, leaving the movable free to rotate around its hinge line, further balancing the movable and calculating in a first approach its coarse static momentum. The method includes refining the coarse static momentum and obtaining simultaneously a frictional momentum of the movable; incorporating an elastic element on the control surface and configuring a second order mechanical system; inducing forced oscillations on the movable at a certain frequency, this frequency being increased until it is sensibly close to the resonance frequency of the movable to produce a wave response; calculating, from the wave response, the momentum of inertia of the movable.

Abstract: A method of joining a first component to a second component, the method comprising forming an array of projections extending from a bond surface of the first component, the projections having a plurality of different profiles; and embedding the array of projections in the second component formed of a plurality of laminate plies, wherein each projection profile is adapted to best transfer load into a respective one of the laminate plies. The resultant joint is able to transfer load more progressively between the two components leading to improved tensile strength.

Abstract: A profile plate portion is disclosed for use as an outer wall of a flow body including a first profile plate panel that is fluid permeable, a second profile plate panel extending along the first profile plate panel, and a reinforcing device for supporting the first profile plate panel and the second profile plate panel on one another. Fluid can flow through the reinforcing device, and/or fluid of the flow present at the first profile plate panel, which flows through the first profile plate panel, can flow through the reinforcing device in the local profile plate thickness direction from the first profile plate panel to the second profile plate panel and in some regions can flow through to an inside that is situated opposite the flow side. A method is disclosed for manufacturing a profile plate portion and a flow body component with a suction-extraction device for fluid.

Abstract: The support (1) comprises a main body (3) which has a convex shape comprising facets which are planar and curved and free of edges, and it is provided with main contact surfaces (5) each of which is able to accept an electric cable, and with openings (6) surrounding each of the main contact surfaces (5).

Abstract: A method of manufacturing a structure, the method comprising: forming a panel assembly by bonding a stack of thickness control plies of composite material to a laminar composite panel, the stack of thickness control plies having a first edge proximate an edge of the laminar composite panel, a second edge opposite the first edge, and a ramp where the thickness of the stack of thickness control plies decreases towards the first or second edge; measuring the thickness of the laminate composite panel or the panel assembly; controlling the number of thickness control plies in accordance with the measured thickness; attaching a first component to the panel assembly, the first component having a surface which engages the laminar composite panel and a ramp which engages the ramp in the stack of thickness control plies; and attaching the laminar composite panel at or near its edge to a further component.

Abstract: It is intended for installing and fitting, in conjunction with other iron fittings, a fairing on an aircraft in correspondence with a housing located at the junction of a stabilizer and a fuselage of an aircraft structure. Wherein each iron fitting comprises: a base plate (5) joined integrally to a torsion box (6) of the stabilizer (3); a mobile support (7) joined integrally to the fairing (1) and which is guided, over a linear movement, over the base plate (5); an adjustment screw (8) that is coupled into a threaded opening (15) of the base plate (5), which screw joins this base plate (5) to the mobile support (7), with the rotation of said adjustment screw (8) in combination with a retaining plate (23) dragging the respective mobile support (7) that is integral to the fairing (1).

Abstract: A preferred embodiment of the invention relates to a cyclone separator for a vacuum toilet system, with a casing; an input-side swirl generator, whose input openings impart a swirl to the inflowing fluid; a separating wall arranged in the casing, which encloses the fluid stream in the cyclone separator ring-like and whose interior cross section tapers downstream; and a collection tank in the casing for receiving and accumulating constituents separated out of the fluid. In addition, the invention relates to a wastewater tank and vacuum toilet system having such a cyclone separator.

Abstract: The invention relates to a sensor network for determining the position of devices and gear in an aircraft. The sensor network exhibits several sensor nodes, which have an autonomous power supply. The sensor nodes can communicate wirelessly with each other and with a central processing unit. The position of each individual sensor node can be determined by evaluating high-frequency signal parameters.

Abstract: A data transmission network comprising: a base comprising: a base light source and a base light detector; a plurality of nodes, each node comprising a node light source and a node light detector; and a plurality of optical fibers arranged to form a optical fiber network. Each optical fiber is arranged to receive light from the base light source, transmit the light received from the base light source to one or more of the node light detectors via an air gap, receive light from one or more of the node light sources via an air gap, and transmit the light received from the node light source(s) towards the base light detector.

Abstract: A method for producing a connector, in particular for repair, in particular in the field of aviation and aerospace, including the steps of: providing a base layer; attaching a first layer of fibre composite material having a first rigidity to the base layer; attaching a second layer of fibre composite material having a second rigidity to the first layer, offset therefrom, the second rigidity being greater than the first rigidity; and riveting the first layer to the base layer and riveting the second layer to the first layer and to the base layer.