Patents Assigned to AIRBUS DEFENCE & SPACE SAS
  • Patent number: 10196767
    Abstract: The subject matter of the invention is a method for draping on a form, which includes a step of deposition on the form of a first fold support in the form of one or more polymer nonwoven fabrics. The invention further relates to a thermoplastic nonwoven material manufactured with a nonwoven fabric of polymer fibers.
    Type: Grant
    Filed: January 28, 2013
    Date of Patent: February 5, 2019
    Assignee: AIRBUS DEFENCE & SPACE SAS
    Inventors: Jean-Baptiste Deyts, Florian Chotard, Eric Soccard
  • Patent number: 9981757
    Abstract: The invention relates to a propulsion unit for a reusable launch vehicle including a rocket engine supported by a cradle. According to the invention, the cradle includes at least three attachment elements for assembling the unit on the structure of the vehicle to which the unit is to be connected, the at least three attachment elements defining a plane for removing the unit, and in which the unit includes one or more fluid and/or electric links of the engine, each one of the links including a free end to be assembled with a corresponding circuit for supplying the vehicle, to which the unit is to be connected, the tip of at least some of the free ends being contained in the removal plane.
    Type: Grant
    Filed: July 4, 2014
    Date of Patent: May 29, 2018
    Assignee: AIRBUS DEFENCE & SPACE SAS
    Inventors: Yohann Coraboeuf, Jean-Philippe Dutheil
  • Patent number: 9938025
    Abstract: A device for mounting and supporting a generally cylindrical or tapered tank, having a main axis X, that includes a pair of first retaining rods for retaining the tank along a vertical axis Z on each of a first and second end of the tank, a second retaining rod for retaining the tank along a horizontal axis Y, perpendicular to the main axis, on the first end of the tank, and a third retaining rod for retaining in a ball-and-socket joint, the means being located around the vertical axis and connected to the second end of the tank.
    Type: Grant
    Filed: February 4, 2014
    Date of Patent: April 10, 2018
    Assignee: AIRBUS DEFENCE & SPACE SAS
    Inventors: Benjamin Faure, Jérôme Bertrand, Yohann Coraboeuf, Samuel Chevrollier, Robert Abadie-La-Haille, Pascal Mezieres, Angélique Santerre
  • Publication number: 20160257435
    Abstract: The invention relates to a propulsion unit for a reusable launch vehicle including a rocket engine supported by a cradle. According to the invention, the cradle includes at least three attachment elements for assembling the unit on the structure of the vehicle to which the unit is to be connected, the at least three attachment elements defining a plane for removing the unit, and in which the unit includes one or more fluid and/or electric links of the engine, each one of the links including a free end to be assembled with a corresponding circuit for supplying the vehicle, to which the unit is to be connected, the tip of at least some of the free ends being contained in the removal plane.
    Type: Application
    Filed: July 4, 2014
    Publication date: September 8, 2016
    Applicant: AIRBUS DEFENCE & SPACE SAS
    Inventors: Yohann CORABOEUF, Jean-Philippe DUTHEIL
  • Patent number: 9346994
    Abstract: A heat protection material for a surface, made of a mixture comprising a resin, cork granules and refractory fibers; the proportion of cork granules in the mixture is 50 to 80% by mass, wherein the corresponding proportion of refractory fibers in the mixture is 1 to 11% by mass.
    Type: Grant
    Filed: April 19, 2011
    Date of Patent: May 24, 2016
    Assignee: AIRBUS DEFENCE & SPACE SAS
    Inventors: Cédric Plaindoux, Jean-Marc Bouilly