Abstract: Disclosed is an instrument panel designed to be integrated into an aircraft cockpit, the instrument panel comprising a main structure, extending longitudinally and having a concave shape defining a cavity, this cavity being configured to receive a plurality of navigation command and/or control units, and at least one inner wall, configured to delimit at least two recesses each intended to receive at least one of the plurality of navigation command and/or control units, the instrument panel being characterized in that the main structure is made from a single piece made from a composite material.

Abstract: A cockpit suitable for being installed in a pilot's cabin of an aircraft, the cockpit comprising a floor, a plurality of interior furniture items and a dashboard configured to receive a plurality of devices for commanding and/or controlling the aircraft, the cockpit comprising a securing system which connects the dashboard solely to the floor and/or to the plurality of interior furniture items.

Abstract: Disclosed is an instrument panel designed to be integrated into an aircraft cockpit, the instrument panel comprising a main structure, extending longitudinally and having a concave shape defining a cavity, this cavity being configured to receive a plurality of navigation command and/or control units, and at least one inner wall, configured to delimit at least two recesses each intended to receive at least one of the plurality of navigation command and/or control units, the instrument panel being characterized in that the main structure is made from a single piece made from a composite material.

Abstract: A device for shaping a blank for forming a thermoplastic structural part, the blank comprising reinforcing fibres embedded in a thermoplastic matrix, said shaping device comprising a support member for supporting a blank along a longitudinal axis, at least one heating member, at least one inclination member configured to modify the inclination of at least one part of the longitudinal portion of the blank at an angle of inclination that can be parameterised with respect to the horizontal plane in a plane transverse to the longitudinal axis, and a movement system from upstream to downstream along the longitudinal axis of the heating member and of the inclination member relative to the support member so as to successively modify the inclination of a part of each longitudinal portion of the blank.

Abstract: A system for producing at least one structural thermoplastic part, said structural thermoplastic part being formed from a rough part comprising reinforcing fibres immersed in a thermoplastic matrix, the structural thermoplastic part to be produced comprising an outer face and an inner face, opposite the outer face, the production system comprising at least one inflatable pressure member made of a material having a thermal resistance greater than the heating temperature, the inflatable pressure member being mounted between the first counter-mould and the second mould, the inflatable pressure member being configured to develop between the deflated idle state and an inflated state to flatten the rough part between the imprint of the first mould and the imprint of the first counter-mould so as to consolidate the rough part and to form the structural thermoplastic part.

Abstract: The invention relates to a long tubular pipe comprising an outer tube, an inner fluid-transporting tube mounted in the outer tube, and a separating member designed to transmit bending efforts between said outer tube and said inner tube when said outer tube is bent, the separating member comprising means for the longitudinal passage of fluid between the inner tube and the outer tube, the separating member comprising a first edge and a second edge together defining an assembly slot, the first edge and the second edge respectively comprising a first connecting element and a second connecting element designed to cooperate mechanically on the outer periphery of the inner tube.

Abstract: A seat including a seat portion, a backrest, and a headrest attached to a structure of the backrest. The headrest includes a head cushion attached to the backrest by at least one headrest arm; the arm is hingedly attached to the backrest structure by a pivot link with a transverse axis; the head cushion is hinged to the arm by a pivot link with a transverse axis. Moreover, the first axis is situated at a rear face of a structural part of the backrest; the second axis is situated close to the bottom edge of the head cushion; in the lowered position, the arm holds the head cushion bearing against the front face of the backrest; in the raised position, the arm holds the head cushion above and in front of the lowered position.

Abstract: The invention relates to a long tubular pipe comprising an outer tube, an inner fluid-transporting tube mounted in the outer tube, and a separating member designed to transmit bending efforts between said outer tube and said inner tube when said outer tube is bent, the separating member comprising means for the longitudinal passage of fluid between the inner tube and the outer tube, the separating member comprising a first edge and a second edge together defining an assembly slot, the first edge and the second edge respectively comprising a first connecting element and a second connecting element designed to cooperate mechanically on the outer periphery of the inner tube.

Abstract: A method for manufacturing a pipe is described, wherein the method comprises a step of fastening a second mechanical quick connection member to a rectilinear hollow tubular body, a step of positioning the rectilinear hollow tubular body in a bending machine so that the angular coding mechanism of the second mechanical quick connection member is in a reference angular position with respect to said bending machine, and a step of bending the rectilinear hollow tubular body as a function of said angular reference position.

Abstract: A set includes seats, each seat includes a chair and a lateral pedestal arranged laterally on one side of the chair. The chairs and the lateral pedestals are arranged in a staggered configuration in two parallel rows. Each seat has a covering shell determining a rear surface in a rear zone of the chair and determining a front surface in a front zone of the lateral pedestal. A space between a rear surface of a front seat and a front surface of a rear seat forms a passage for an occupant of the rear seat. In a vertical cross section the rear surface and the front surface have convex profiles facing one another, a width of the passage increasing in the direction of decreasing heights from a height of minimum width, and increasing in the direction of increasing heights from the height of minimum width.

Abstract: A support for overlengths of cable bundles, includes a rear wall by which the support is fixed, an almost-toroidal cavity, at least one axial indentation, and a cover. The almost-toroidal cavity is delimited by: the rear wall; an inner wall determining a small diameter of the almost-toroidal cavity; and an outer wall determining a large diameter, greater than the small diameter, of the almost-toroidal cavity. The cover is fixed removably such that: the almost-toroidal cavity is open, on the front side of the support, over a whole length of the almost-toroidal cavity when the cover is removed and forms an almost-circular groove; and the almost-toroidal cavity is closed, except for the at least one axial indentation, when the cover is fixed. A vehicle including such a support and a method for installing a cable bundle are also provided.

Abstract: A seat, including a seat bottom for which a seat frame is supported by a base, and a seat back, the seat including a “seated” position, a “lying” position and an intermediate “resting” position. A seat plate can be moved in rotation around a rear axis located at the side of a rear edge of the seat, the seat plate being movable in rotation around a tilting axis in front of the rear axis, the seat frame is moved forward during conversion from the “seated” position to the “lying” position. An essentially horizontal rear segment. An intermediate rear segment with a downward slope greater than the slope followed by the tilting axis. An intermediate front segment with an essentially horizontal upward slope.

Abstract: Machine for bending at least one longitudinal cylindrical pipe, the bending machine having at least one heating module configured so as to heat a longitudinal cylindrical pipe and at least one deformation module configured so as to deform a longitudinal portion of a longitudinal cylindrical pipe in order to bend it, said heating module having a plurality of heating units, each heating unit can include a peripheral heating body defining an internal opening adapted to allow the passage of a longitudinal portion of a longitudinal cylindrical pipe to be heated.

Abstract: A fluid circuit, particularly for an aircraft, comprising a first pipe, a second pipe and a coupling comprising an outer sleeve which extends along an axis X and is mounted with the ability to slide along the axis X at a connection ends of the first pipe, a sealing member which extends along the axis X and is mounted with the ability to slide along the axis X in said outer sleeve, the sealing member being configured to sealingly connect the connection ends of the pipes, locking means configured to collaborate with a blocking member of the second pipe so as to block the translational movement of said outer sleeve towards the first pipe, the coupling being configured to move the sealing member between the two connection ends in order to provide sealing as the outer sleeve is moved as far as the blocking member of the second pipe.

Abstract: A driving seat comprises a base and a back rest forming a support structure. The back rest is articulated onto the base about an axis of inclination of the back rest to provide an adjustable back rest inclination angle. The base comprises a rear base panel of fixed inclination and a front base panel with an adjustable base inclination angle relative to the rear base panel. The back rest comprises a lower back rest panel and an upper back rest panel with an adjustable raising angle relative to the lower back rest panel. In operation, the back rest inclination angle, the base inclination angle and the raising angle are adjustable to adapt the configuration of the seat to a working configuration, a standby configuration, a rest configuration or a crash configuration.

Abstract: An aircraft fuselage includes a structure, considered in respect of all or part of the fuselage, with fuselage upper sub-structure constituting an upper part of the fuselage and a fuselage bottom sub-structure constituting a lower part of the fuselage. Openings in the structure of the fuselage are intended for the installation of windows or doors for exiting the fuselage. Furthermore, the fuselage upper sub-structure are the fuselage bottom sub-structure form fuselage sub-structures that are assembled with one another via at least one lintel in which all or some of the openings intended for installing the exit doors or windows are formed.

Abstract: An aircraft cabin having seats with at least one of which is paired with a passenger terminal to communicate wirelessly. A control unit of the seat transmits data on the capabilities for adjusting the seat to the passenger terminal. The passenger terminal transmits instructions for adjusting the seat to the control unit of the seat. The passenger terminal includes application software to interpret the data received from the control unit of the seat to display a representation of the possible adjustments on a screen of the passenger terminal and to interpret actions by an operator on keys of the passenger terminal as instructions for adjusting the seat. A main computer of the cabin handles the communication between the passenger terminals and crew terminals to transmit, via displays on screens of the terminals, requests from a passenger to the crew and from the crew to a passenger or group of passengers.

Abstract: An aircraft seat includes a seat bucket that is integral by its seatback with a single beam oriented along an axis that is approximately perpendicular to the aircraft floor, which beam is integral with fastening points located on at least two separate lines on the aircraft floor.

Abstract: The invention relates to a single-piece stringer for an aeronautic structure, the stringer comprising a single-piece body including at least one hollow longitudinal portion so as to define an outer enclosure, said outer enclosure including a plurality of openings.

Abstract: A set includes two blocks each of two seats convertible for lying down, wherein the two blocks are arranged with the seats of one block face-to-face with the seats of the other block inside a circumscribed rectangle. Each block includes a first seat and a second seat. The first-seats of the two blocks are arranged along a first diagonal of the circumscribed rectangle and the longitudinal axes of the first seats are oriented so that their directions are close to the first diagonal and the first seats are substantially face-to-face. The distance between the two first seats is such that a foot area of a first seat of a block is superposed when seen from above with a foot area of the first seat of the other block. In the recumbent configuration, the planes to lie down on of the two first seats are at different heights.