Abstract: An assembly including an electrically conductive strip extending along a longitudinal axis, including a first carrier layer having a first face and a second face opposite the first face; a first electrically conductive track placed on the first face or the second face of the first carrier layer; an electrical connector with a first clamping portion and a second clamping portion that are securely fastened to each other and that define a clamping region for clamping the electrically conductive strip. The first and second clamping portions clamp the electrically conductive strip. At least one of the first and second clamping portions includes a first contact segment making electrical contact with the first electrically conductive track.

Abstract: The invention relates to a heating structure (30) intended in particular for installation inside a passenger compartment of a vehicle, this structure being in particular a radiant panel, the heating structure (30) comprising at least one resistive layer arranged to give off heat when an electric current flows through this layer (31), this structure further comprising an array of electrodes (32) comprising a plurality of contact electrodes (33) that are arranged so as to be in electrical contact with the resistive layer in order to make electric current flow through this resistive layer, at least two of these contact electrodes being in contact with a region of the resistive layer (31), these two contact electrodes facing one another such that electric current can flow from one of these electrodes to the other of the contact electrodes by passing through this region of the resistive layer, these two contact electrodes (33) on either side of said region taking a shape chosen such that the two electrodes get clo

Abstract: Metal electrical connector (1) for flexible electrically conductive strip (2) extending along a longitudinal axis (A), said conductive strip (2) comprising: —a flexible support layer (3) comprising a first face and a second face opposite the first face, and —a conductive path (4) arranged on the first face of the flexible support layer (3), said electrical connector (1) comprising: —a base (10) having a generally parallelepiped shape and configured to cover a portion of the conductive strip (2), said base (10) comprising at least one leading edge (101) intended to face the conductive strip (2) perpendicular to the longitudinal axis (A), —connecting teeth (12a, 12b) configured to pass through the conductive path (4) and the flexible support layer (3), —a connecting member (11) projecting from one of the edges of the base (10) other than the leading edge (101), the leading edge (101) of the base (10) having an inwardly curved profile over the width of the base (10).

Abstract: The invention relates to a heating structure (30) which is intended in particular to be installed inside a passenger compartment of a vehicle, the heating structure (30) comprising at least one resistive layer arranged to release heat when an electric current passes through this layer (36), this panel further comprising art electrode array comprising a plurality of contact electrodes (34) arranged to be in electrical contact with the resistive layer in order to Sallow electric current to flow through this resistive layer.

Abstract: A heating structure (1) configured to be installed inside a passenger compartment of a vehicle is disclosed. The heating structure (1) includes at least one resistive layer arranged so as to release heat when an electric current passes through this layer (4), this panel further comprising an electrode array (5) comprising a plurality of contact electrodes (6) arranged so as to be in electrical contact with the resistive layer in order to allow electric current to flow through this resistive layer.

Abstract: A radiant panel (1) intended to be installed inside a vehicle (80) passenger compartment (3), in particular a motor vehicle passenger compartment, the radiant panel (1) comprising at least one array of electrodes with at least two primary electrodes of different polarities, the array of electrodes being arranged such that at least two primary electrodes of different polarities each define at least one spiral winding around one another.

Abstract: An aircraft propulsion unit comprising a nacelle with a fan cowl locking and closing mechanism. The fan cowls of the nacelle can be closed by a single operator in accordance with the ergonomic standards defined for a single individual. A nacelle is provided with a lateral locking mechanism configured to keep one of the two fan cowls in the closed position, so as to reduce the spacing between the two lower sides of the fan cowls, whereas the presence of a stop between a first elastic member provided on one fan cowl and a second elastic member provided on the other fan cowl allows the operator to provide only that effort required to overcome the force exerted by a single spring at a time.

Abstract: A control device for controlling a variable section nozzle of an aircraft power plant, the variable section nozzle including one or several movable parts capable of modifying the nozzle section and connected by a mechanical transmission chain to an actuator. The control device includes a system for regulating the power plant connected to a control member configured to control the actuator. The control device includes a single control member, an immobilization unit configured to immobilize all the movable parts which are deactivated only when the regulation system controls the positional change of the movable part or parts and a determination unit configured to determine the actual position of the movable part or parts.

Abstract: An aircraft propulsion unit comprising a nacelle with a fan cowl locking and closing mechanism. The fan cowls of the nacelle can be closed by a single operator in accordance with the ergonomic standards defined for a single individual. A nacelle is provided with a lateral locking mechanism configured to keep one of the two fan cowls in the closed position, so as to reduce the spacing between the two lower sides of the fan cowls, whereas the presence of a stop between a first elastic member provided on one fan cowl and a second elastic member provided on the other fan cowl allows the operator to provide only that effort required to overcome the force exerted by a single spring at a time.

Abstract: A control device for controlling a variable section nozzle of an aircraft power plant, the variable section nozzle including one or several movable parts capable of modifying the nozzle section and connected by a mechanical transmission chain to an actuator. The control device includes a system for regulating the power plant connected to a control member configured to control the actuator. The control device includes a single control member, an immobilization unit configured to immobilize all the movable parts which are deactivated only when the regulation system controls the positional change of the movable part or parts and a determination unit configured to determine the actual position of the movable part or parts.

Abstract: A power plant includes a nacelle with a bypass turbojet engine having a ducted fan with a low compression ratio. A secondary flow, drawn in and accelerated by the fan, is channeled through a secondary duct installed in the nacelle between the inner surface of the nacelle and the outer surface of the turbojet, toward a fan nozzle. The power plant has at least two moving parts on either side of a vertical plane of symmetry of the nacelle, at least one moving part being able to adopt one of a discrete number of positions, the moving part containing or releasing a portion of the secondary flow, depending on the moving part's position. A control unit controls a different displacement of each of the moving parts between their possible positions in order to create asymmetry of the moving parts relative to the vertical plane of symmetry.

Abstract: The invention relates to a nacelle for a variable area nozzle propulsion unit comprising a nacelle, hosting a turbofan jet engine, of dual-flow type. The propulsion unit includes: a fixed part, carried by the inboard half-nacelle defined by a vertical plane of symmetry of the nacelle; and a movable part carried by the outboard half-nacelle. The moving part containing or releasing part of the secondary flow, depending on its open or closed position. The moving part being able to move to a discrete number of positions including a closed position, an open position, and one or more intermediate positions so as to provide variable area nozzle configurations for the turbofan engine.