Patents Assigned to SOCIETE PAR ACTIONS SIMPLIFIEE
  • Publication number: 20100299559
    Abstract: A method for processing the volume of information handled during the debugging phase of an operational software onboard an aircraft includes: dividing the execution path of the operational software into functional intervals by placing progression points at each function of the program; placing control points associated with each progression point; normal execution of the program that includes: storing the execution state of the program at the location of each progression point, wherein the storage of an execution state results in the suppression of the execution state previously stored for said progression point; upon the detection of an error, searching the progression point corresponding to a faulty function; searching for a software start execution state; regenerating the start execution state; correcting the error in the faulty function; and re-executing the program.
    Type: Application
    Filed: September 12, 2008
    Publication date: November 25, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventor: Famantanantsoa Randimbivololona
  • Publication number: 20100287776
    Abstract: A method for assembling a part of a metal material and a part of a composite material, the junction of the two parts being achieved through a fastener having a substantially constant section and received in a first hole formed in the part of a metal material and a second hole formed in the part of a composite material. According to the disclosed embodiments and before assembling the aforementioned parts, the method includes: an expansion step for generating a field of compression stresses at the periphery of the first hole and locally in the material constituting the part of a metal material using an expansion tool; a single boring step for making the first hole and the second hole with a diameter Øfinal substantially larger than the diameter of the fastener in order to leave a gap between the inner walls of the holes and the outer surface of the fastener; and an assembling step for placing the fastener inside the holes for maintaining together the metal part and the composite part.
    Type: Application
    Filed: May 6, 2008
    Publication date: November 18, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Nicolas Dantou, Stephane Bianco, Christian Godenzi
  • Publication number: 20100253692
    Abstract: The present invention relates to a display device for a glass cockpit of an aircraft, intended to provide video streams to a plurality of viewing screens of said glass cockpit, said aircraft being partitioned into a secured area, a so-called avionic world (AW), and a non-secured area, a so-called open world (OW), said system comprising at least one first port intended to receive first data to be displayed from a system (210, 310, 410) belonging to the avionic area and at least one second port intended to receive second data to be displayed from a system (220, 320, 420) belonging to the open world, the display device comprising: predetermined hardware resources allocated to the processing of the second data; a processor (241, 341, 441), belonging to the avionic area, adapted to controlling the hardware resources used by said processing and interrupting this processing if said hardware resources used exceed said allocated resources.
    Type: Application
    Filed: July 2, 2008
    Publication date: October 7, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Lionel Cheymol, Vincent Foucart, Simon Innocent
  • Publication number: 20100252458
    Abstract: A tubular container, closed at its top part by a closure means of the stopper type including with a hinge, for packaging unit products stacked axially or in bulk such as pallets, tablets, cachets or pills, and provided with a compensation device, positioned at the bottom of the container. The container optionally includes a desiccating means and the compensation device includes a compensation means and a fastening means. The fastening means is secured to the compensation means and has a shape memory.
    Type: Application
    Filed: March 21, 2008
    Publication date: October 7, 2010
    Applicant: AIRSEC (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Bruno GUILLON, Valere LOGEL
  • Publication number: 20100257366
    Abstract: The invention relates to a method for authenticating a user (1) on the basis of a mobile terminal of the cellular phone type (2), in which said user (1) views through a browser a portal for accessing a service hosted on a server (4); said user (1) requests his authentication through the browser via said portal; said portal initiates a pre-session in such a way as to display, through said browser, temporary access data (5) independent from said user (1); said user (1) inputs into his telephone (2) the data viewed; said telephone (2) automatically dispatches a request (6) to said server (4), including at least one authentication certificate (7) specific to the user (1) and said viewed data (5); said request (6) is encrypted with the aid of the public key of a certificate (8) of said server (4) and, in the event of authentication of the user (1), access to the service is authorized through a secure session in the browser.
    Type: Application
    Filed: December 11, 2008
    Publication date: October 7, 2010
    Applicant: MEDISCS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Alain Leclercq, Yves Arnail, Bernard Delbourg
  • Publication number: 20100253125
    Abstract: The invention relates to a seat for a vehicle, that includes a headrest with a headstall for supporting the head of a passenger in the seat, wherein the occupant may or may not wear a protection helmet depending on the circumstances. The headstall can assume at least three stable positions: a first position for the cervical support of the head of the seat passenger in which the headrest provides a cervical support function with or without wearing a helmet; a second position for the occipital support of the head of the seat passenger in which the headrest provides an occipital support function without wearing a helmet; a third position for the occipital support of the head of the seat passenger in which the headrest provides an occipital support function while wearing a helmet.
    Type: Application
    Filed: June 10, 2008
    Publication date: October 7, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Maxime Le Texier, Regis Leymat, Louis Duroch, Laurent Cecinas
  • Publication number: 20100230122
    Abstract: A fire extinguisher device for aircraft has a hanger structure (4) and a reservoir (3) of extinguishing agent, said reservoir being hung beneath said hanger structure by metal fittings (300, 301a, 301b) held by fasteners to said hanger structure. Said extinguisher is characterized in that the reservoir (3) has means of suspension (31) and the hanger structure (4) has carriers (41) complementary to the means of suspension (31), said means of suspension and said carriers being such that when the fasteners are withdrawn, the reservoir (3) is in a position called the “intermediate position,” in which the metal fittings (300, 301a, 301b) are free and the reservoir (3) is suspended by interaction of the means of suspension (31) and the carriers (41). The invention also relates to a method for fastening such an extinguishing device.
    Type: Application
    Filed: March 5, 2010
    Publication date: September 16, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Stéphane MACHADO, Frédéric ROSSI, Julien CAYSSIALS, Nicolas VOYER
  • Publication number: 20100218172
    Abstract: A method for simulating a real on-board system for testing an operating software program. The disclosed embodiments include preparation of a test to be carried out on the operating software program, by adding and/or removing control functions to/from a library; execution of the operating software program of the real on-board system in a simulated environment; simulation of a dedicated peripheral by activating functions from the library; transmission of the test results from the dedicated peripheral to the results folders stored on the host platform and recording of the aforementioned results.
    Type: Application
    Filed: May 19, 2008
    Publication date: August 26, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventor: Famantanantsoa Randimbivolona
  • Publication number: 20100201517
    Abstract: The invention relates to a device for protection against intrusions into the landing gear housings of an aircraft, including at least one sensor, for at least one housing, covering at least one housing entry area and connected to a calculator (6) capable of processing the data from said sensor (4) for detecting the intrusion of a target and generating intrusion occurrence information for triggering an alarm, wherein the calculator (6) is connected to a device (9) for providing aircraft flight phases and/or ground speed information, the device including a means adapted for changing the detection status from an active mode to an inactive mode based on said flight phases and/or ground speed information.
    Type: Application
    Filed: April 22, 2008
    Publication date: August 12, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventor: Olivier Pujol
  • Publication number: 20100192540
    Abstract: A closing system for a fan cowling on a jet engine of an aircraft that has at least one assembly including a male contrivance integral with the cowling, and a female contrivance integral with the jet engine that has a lower element forming at least one first guide ramp and an upper element forming at least one second guide ramp, with the aforementioned female contrivance being suitable on the one hand for guiding the male contrivance during the opening and/or the closing of the fan cowling, and on the other hand providing a limitation of the radial and circumferential displacements of the male contrivance.
    Type: Application
    Filed: December 2, 2009
    Publication date: August 5, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Robert ANDRE, Loic DUSSOL, Frederic RIDRAY
  • Publication number: 20100198431
    Abstract: A maintenance computer system for an aircraft, including a network partitioned into a secured avionics zone and an open zone. The system includes a first software module accommodated in the avionics zone and a second software module accommodated in the open zone, the first module configured to follow a fault-finding logic tree, and the second module configured to present an electronic maintenance document, with the path along the fault-finding logic tree followed by the first module automatically and synchronously generating a presentation by the second module of pages of the maintenance document associated respectively with nodes of the tree.
    Type: Application
    Filed: June 5, 2008
    Publication date: August 5, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventor: Jean-Philippe Corbefin
  • Publication number: 20100184102
    Abstract: A device for the determination and/or the detection of erythrocyte blood groups from a whole blood sample, and a process that implements this device, as well as a kit for the determination and the detection of blood groups are disclosed.
    Type: Application
    Filed: July 2, 2008
    Publication date: July 22, 2010
    Applicant: ABO DIAG, SOCIETE PAR ACTIONS SIMPLIFIEE
    Inventor: Najim Chaibi
  • Publication number: 20100176241
    Abstract: The invention relates to an aircraft front portion (1) including a sealed bulkhead (10) separating a non-pressurized radome area (20) from a pressurized area (30), whereof the volume of the pressurized area (30) is optimized. For this, said sealed bulkhead (10) is delimited by two surfaces (11,12) opposite to each other, one (11) being substantially concave when it is seen from said radome area (20) and the other one (12) being substantially convex when it is seen from said pressurized area (30).
    Type: Application
    Filed: January 13, 2010
    Publication date: July 15, 2010
    Applicant: SOCIETE PAR ACTIONS SIMPLIFIEE
    Inventors: Cédric Meyer, Bernard Guering
  • Publication number: 20100163676
    Abstract: An aircraft in which it is possible to replace windshield panes of the mineral type with windshield panes of the organic type and vice versa, without the frame of the aircraft structure having to be modified. The pane is held in place on the frame by a window pane retainer specific to the pane. The frame has no through-holes opening to the outside of the aircraft for fastening the pane. The window pane retainer specific to a pane of the organic type has pins passing through the acrylic panes. The disclosed embodiments also relate to a method of replacing a pane of a first type with a pane of a second type.
    Type: Application
    Filed: December 2, 2009
    Publication date: July 1, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Samuel BURGUNDER, Pascal CHAUMEL, Patrick LIEVEN, Christophe MIALHE
  • Publication number: 20100140410
    Abstract: The icing indicator for an aircraft, of the type that can be directly and visually read by a pilot, includes means of installation at the surface of the fuselage and projecting therefrom, in combination with an already-existing device positioned above a through-hole in the fuselage, the device being modified to allow a power cable that powers the icing indicator to pass through the fuselage within its fastening. The icing indicator is preferably combined with a rain repellent spray device or on the spindle about which the windscreen wiper rotates.
    Type: Application
    Filed: December 8, 2009
    Publication date: June 10, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventor: Patrick Lieven
  • Publication number: 20100136293
    Abstract: The disclosed embodiments concern a curved structural part composed of a composite material with reinforced, continuous fibers whose cross section includes at least two wings, with said fibers extending from one wing to the other, with said structural part having a variation in the width of its section parallel to the local radius of curvature. The structural element that results from assembling the parts in the disclosed embodiments therefore has local widening of the section at the connections between the parts constituting a structural element, such as an aircraft fuselage frame, and widening at the connection with the floor profiles, if such a profile is used to make an aircraft fuselage structure. The disclosed embodiments also concern a process for manufacturing such a part, as well as a device for advantageously implementing such a process.
    Type: Application
    Filed: November 19, 2009
    Publication date: June 3, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Vanessa Kubryk, Nathalie Hellard-Lambic
  • Publication number: 20100133377
    Abstract: An aircraft includes a fuselage having a shape elongated along a longitudinal axis X of the aircraft and at least one wing fixed to the fuselage between the front end and the rear end of the fuselage. The fuselage includes a substantially cylindrical central part and a rear tapered part on which a vertical empennage is fixed. Between a section connecting the rear part with the central part of the fuselage and the rear end the maximum width of each section of the fuselage is constant or increasing rearwards up to a maximum width L of the fuselage, the height of each section of the fuselage is decreasing rearwards in the direction of the negative X, so that the rear end of the fuselage forms a trailing edge having a small thickness which is substantially horizontal in an aircraft reference system and substantially rectilinear.
    Type: Application
    Filed: October 14, 2009
    Publication date: June 3, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Olivier Cazals, Jaime Genty De La Sagne
  • Publication number: 20100127126
    Abstract: The subject matter of the disclosed embodiments is a device for mounting a window glass including a seal covering a peripheral edge of the window glass and provided with a strip bearing against a peripheral flat of a frame of the window. The seal includes a flange engaging in the recess of the window and is provided with a squeegee lip bearing against the edge of the frame.
    Type: Application
    Filed: November 25, 2009
    Publication date: May 27, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventor: Patrick Lieven
  • Publication number: 20100102169
    Abstract: The invention concerns a floor for a transport vehicle that can be attached to a vertical frame structure (30) of said vehicle and that includes: a horizontal boxed structure (1) having a plurality of boxes (13) positioned side by side to form a continuous, uniform upper surface (14) and lower surface (15), with the upper surface (14) covered with an upper skin (11) and the lower surface covered with a lower skin (12) and means of attachment (20) to attach the boxed structure (10) laterally to the frame structure (30). The invention also concerns a process for manufacturing this floor.
    Type: Application
    Filed: October 13, 2009
    Publication date: April 29, 2010
    Applicant: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE)
    Inventors: Daniel ZORZETTO, Jean-Christophe LATAILLADE
  • Publication number: 20090314899
    Abstract: A rear frame of an air intake of a nacelle of an aircraft, is made in part of composite material that is based on a fiber-reinforced geopolymer resin and includes at least one part (56) that encompasses an orifice that is provided for the passage of a defrosting system that is made of composite material that is based on a fiber-reinforced geopolymer resin and at least one other metal part (58).
    Type: Application
    Filed: July 30, 2007
    Publication date: December 24, 2009
    Applicant: AIRBUS FRANCE, SOCIETE PAR ACTIONS SIMPLIFIEE
    Inventors: Alain Porte, Bruno Medda