Patents Assigned to EADS Launch Vehicles
  • Publication number: 20060065663
    Abstract: A process for the production of a vessel for high pressure gas, particularly helium, for a space launcher or for a satellite with a short lifetime. The process includes the step of producing an internal skin of a plastic material selected from polyethylene and crystallized polyamide. The process also includes winding a reinforcement of fibers and resins around the internal skin, and then providing the obtained vessel with the necessary conduits and control valves.
    Type: Application
    Filed: August 4, 2005
    Publication date: March 30, 2006
    Applicant: EADS LAUNCH VEHICLES
    Inventor: Jack Gauthier
  • Patent number: 6967179
    Abstract: The aim of the present invention is a process for manufacturing boron nitride fibers, in particular continuous boron nitride fibers with good mechanical properties, which may be used for producing ceramic composite materials such as BN/BN composites, thermostructural parts or antenna radomes. It provides and uses a precursor polymer of formula (I) below: in which n is a whole number, R1 and R2, identical or different, represent independently an alkyl group, and R3 represents an amino group, a hydrogen atom, an alkyl, a cycloalkyl or a boryl.
    Type: Grant
    Filed: January 21, 2003
    Date of Patent: November 22, 2005
    Assignee: Eads Launch Vehicles
    Inventors: Philippe Miele, Berangere Toury, Samuel Bernard, David Cornu, Khaled Ayadi, Loic Rousseau, Guy Beauhaire
  • Patent number: 6962672
    Abstract: A process for the production of a vessel for high pressure gas, particularly helium, for a space launcher or for a satellite with a short lifetime, includes the steps of: a production of an internal skin of a plastic material selected from polyethylene and crystallized polyamide, a winding a reinforcement of fibers and resins, and a providing the obtained vessel with the necessary conduits and control valves.
    Type: Grant
    Filed: May 20, 2002
    Date of Patent: November 8, 2005
    Assignee: EADS Launch Vehicles
    Inventor: Jack Gauthier
  • Patent number: 6913045
    Abstract: A process for selectively lacing filaments on multi-dimensional textile preforms made of rods, the rods are displaced by the filament and pressed vertically downwardly by a needle with an open eye which, after passing through the piece to be laced, is opened at an insertion station for the filament to receive the filament, then is raised to pass the filament through the space freed by the rod.
    Type: Grant
    Filed: June 6, 2003
    Date of Patent: July 5, 2005
    Assignee: EADS Launch Vehicles
    Inventors: Lucien Fantino, Didier Glayal, François Monget
  • Patent number: 6901740
    Abstract: The pointed end of a central spike, used in an engine of a space launcher, may have a deformable structure that can adopt either a folded position or a deployed position.
    Type: Grant
    Filed: May 13, 2003
    Date of Patent: June 7, 2005
    Assignee: Eads Launch Vehicles
    Inventor: Max Calabro
  • Patent number: 6843280
    Abstract: A weaving device for the production of thick textile armatures constituted by superposed layers of threads secured together by a binding thread traversing the layers, includes a frame provided laterally and at its periphery with regularly distributed hooking pins, elements for depositing with the aid of the pins, thread and elements for flattening the layers. The pins have a first section with a slight inclination outwardly of the frame and a second straight section prolonging the first and having an a substantially greater inclination outwardly of the frame. The elements for depositing thread include a plurality of guides each supplying a thread, and are moved simultaneously and spaced at an interval equal to n times the interval between pins. The elements for weaving the layers include elements adapted to press the assembly of the layers about their periphery.
    Type: Grant
    Filed: November 27, 2002
    Date of Patent: January 18, 2005
    Assignee: EADS Launch Vehicles
    Inventors: Georges Cahuzac, Jean-Louis Darrieux
  • Patent number: 6820559
    Abstract: The temporary connection of two elements (12, 14) is ensured by U-shaped connecting components (16) held in place by a moving part (18). A pyrotechnic composition (20) is housed between two shoulders (32, 36) situated respectively on the first of the elements (12) and on the moving part. Igniting the pyrotechnic composition (20) causes the moving part (18) to slide over the first element (12). The connecting components (16) are released and the connection between the elements (12, 14) is eliminated without breaking any parts.
    Type: Grant
    Filed: April 30, 2003
    Date of Patent: November 23, 2004
    Assignee: Eads Launch Vehicles
    Inventor: Patrick Comtesse
  • Publication number: 20040226474
    Abstract: The temporary connection of two elements (12, 14) is ensured by U-shaped connecting components (16) held in place by a moving part (18). A pyrotechnic composition (20) is housed between two shoulders (32, 36) situated respectively on the first of the elements (12) and on the moving part. Igniting the pyrotechnic composition (20) causes the moving part (18) to slide over the first element (12). The connecting components (16) are released and the connection between the elements (12, 14) is eliminated without breaking any parts.
    Type: Application
    Filed: April 30, 2003
    Publication date: November 18, 2004
    Applicant: EADS LAUNCH VEHICLES
    Inventor: Patrick Comtesse
  • Patent number: 6774074
    Abstract: The invention concerns a method for making boron nitride fibers by drawing a polymer precursor and treating with ceramics the polymer fibers obtained by drawing. The invention is characterized in that the precursor polymer is obtained by thermal polymerization of a borazine of formula (I) wherein: R1, R3, R4 and R5, identical or different, represent an alkyl, cycloalkyl or aryl group; and R2 represents a hydrogen atom or an alkyl, cycloalkyl or aryl group.
    Type: Grant
    Filed: September 6, 2002
    Date of Patent: August 10, 2004
    Assignee: Eads Launch Vehicles
    Inventors: Loïc Rousseau, Jean-Christophe Pasquet, Samuel Bernard, Marie-Paule Berthet, Jean Bouix, David Cornu, Philippe Mielé, Bérangère Toury, Pascaline Toutois, Christiane Vincent
  • Publication number: 20040118855
    Abstract: The invention concerns a method for manufacturing a tank (1) for fluids under pressure comprising two compartments (8, 10).
    Type: Application
    Filed: May 28, 2003
    Publication date: June 24, 2004
    Applicant: EADS LAUNCH VEHICLES
    Inventor: Max Calabro
  • Publication number: 20040044162
    Abstract: The aim of the present invention is a process for manufacturing boron nitride fibres, in particular continuous boron nitride fibres with good mechanical properties, which may be used for producing ceramic composite materials such as BN/BN composites, thermostructural parts or antenna radomes.
    Type: Application
    Filed: January 21, 2003
    Publication date: March 4, 2004
    Applicant: EADS LAUNCH VEHICLES
    Inventors: Philippe Miele, Berangere Toury, Samuel Bernard, David Cornu, Khaled Ayadi, Loic Rousseau, Guy Beauhaire
  • Publication number: 20030226246
    Abstract: The invention relates to a process for selectively lacing filaments on multi-dimensional textile preforms made of rods, in which the rods are displaced by the filament, the rods being pressed vertically downwardly by a needle (3) of the type with an open eye which, after passing through the piece to be laced and ejection of the rod, is opened at a so-called insertion station (9) for the filament to receive the filament to be laced (21), then is raised to pass the filament through the space freed by said rod, characterized by the following steps:
    Type: Application
    Filed: June 6, 2003
    Publication date: December 11, 2003
    Applicant: EADS LAUNCH VEHICLES
    Inventors: Lucien Fantino, Didier Glayal, Francois Monget
  • Publication number: 20030196544
    Abstract: A temporary connection and pyrotechnic separation device (10) normally connects two elements (12, 14). This device comprises a connecting part (18), of which a bottom portion (38) is fixed to one (12) of the elements. Active portions (40) of the connecting part (18) cover a space (20) in which there is pyrotechnic expansion tube (16). The active portions are deformable and comprise hook-shaped ends (50) that fit into a notch (36) formed in the second element (14), so that normally there is a pressure connection between the two elements. The effect of firing is to deform the active parts and consequently break this pressure connection.
    Type: Application
    Filed: March 31, 2003
    Publication date: October 23, 2003
    Applicant: EADS LAUNCH VEHICLES
    Inventor: Patrick Comtesse
  • Patent number: 6629353
    Abstract: The invention concerns a dome (34) consisting of a round-shaped vessel (30) provided with an opening (28) at the top and by a cap (33) welded on said basin to close said opening (28). The basin is obtained by hot forming under pressure of a truncated blank (5) made of non tempered aluminum alloy.
    Type: Grant
    Filed: January 9, 2002
    Date of Patent: October 7, 2003
    Assignee: Eads Launch Vehicles
    Inventors: Georges Favre-Marinet, Jean-Pierre Bonnafe, Jacques Chanteranne, Joël Delmotte
  • Publication number: 20030180206
    Abstract: The present invention concerns high performance boron nitride fibres and a process for manufacturing said fibres.
    Type: Application
    Filed: January 17, 2003
    Publication date: September 25, 2003
    Applicant: EADS LAUNCH VEHICLES
    Inventors: Philippe Miele, Berangere Toury, David Cornu, Samuel Bernard, Marie-Paule Berthet, Loic Rousseau, Guy Beauhaire
  • Patent number: 6397595
    Abstract: A pyrotechnic actuator comprises a deformable membrane (24) separating a first chamber (20), which is able to receive pyrotechnic combustion gases, from a second chamber (22) containing a control member (32) displaceable by the membrane (24) during the operation of the actuator. In the inoperative state, the membrane (24) is prestressed counter to its deformation controlled by the intake of gases into the first chamber (20). In this way the functional travel is increased, which e.g. makes it possible to open or close a circuit with a larger cross-section without increasing the actuator size.
    Type: Grant
    Filed: May 17, 2001
    Date of Patent: June 4, 2002
    Assignee: Eads Launch Vehicle
    Inventors: Emmanuel Benoit, Jean-François Beau, Erwan Le Floch
  • Publication number: 20020007634
    Abstract: A pyrotechnic actuator comprises a deformable membrane (24) separating a first chamber (20), which is able to receive pyrotechnic combustion gases, from a second chamber (22) containing a control member (32) displaceable by the membrane (24) during the operation of the actuator. In the inoperative state, the membrane (24) is prestressed counter to its deformation controlled by the intake of gases into the first chamber (20). In this way the functional travel is increased, which e.g. makes it possible to open or close a circuit with a larger cross-section without increasing the actuator size.
    Type: Application
    Filed: May 17, 2001
    Publication date: January 24, 2002
    Applicant: EADS LAUNCH VEHICLES
    Inventors: Emmanuel Benoit, Jean-Francois Beau, Erwan Le Floch