Patents Assigned to Office National d'Etudes et de Recherches Aerospatiales
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Patent number: 10100396Abstract: The invention relates to a method and system for forming a layer of oxide on a pervious component made of a material or a stack of materials that are stable at 400° C., said component including an outer surface to be coated and at least one pore with a diameter of 50 to 1000 ?m leading onto said outer surface.Type: GrantFiled: December 1, 2014Date of Patent: October 16, 2018Assignee: Office National D'Etudes et de Recherches AerospatialesInventors: Marie-Pierre Bacos, Frederic Rousseau, Daniel Morvan
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Patent number: 10096113Abstract: A computer-implemented method for designing an electro-optical imaging system for estimating the distance of a source includes use of an optical subsystem, a detector subsystem and a digital image processing subsystem. The method includes the modelling of the propagation of radiation from its source through the optical subsystem, the detector subsystem and the digital image processing subsystem; the modelling being based on a spatial model of the source; the method including a joint step of simultaneously designing the optical subsystem and the digital image processing subsystem, the designing step being based at least on one performance metric depending on a comparison between the local estimation of the distance from the source and the actual distance from the source.Type: GrantFiled: October 9, 2013Date of Patent: October 9, 2018Assignee: OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA)Inventors: Pauline Trouve, Frederic Champagnat, Guy Le Besnerais, Guillaume Druart
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Patent number: 10090073Abstract: Disclosed is a method for measuring an external parameter by atomic interferometry using two sets of atoms that belong to different species. Two measurements are taken simultaneously at the same location, but independently from one another, in order to obtain two measurement results. Constant phase shifts that appear in the atomic interferences for the two atom sets are quadrature-adjusted in order to ensure that one of the two measurements provides a value for the external parameter with satisfactory accuracy.Type: GrantFiled: February 10, 2016Date of Patent: October 2, 2018Assignee: ONERA (OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Nassim Zahzam, Yannick Bidel, Alexandre Bresson, Alexis Bonnin
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Patent number: 10054773Abstract: Some embodiments are directed to a wide-field imaging system for the infrared spectral range. The system can include a vacuum chamber that is optically open for the passage of the field rays originating from the scene to be imaged, a cooled dark chamber placed inside the vacuum chamber and provided with a cold diaphragm, an infrared detector placed inside the cooled dark chamber, and a device for optically conjugating the field rays with the detector.Type: GrantFiled: December 21, 2015Date of Patent: August 21, 2018Assignee: Office National d'Études et de Recherches Aérospatiales (ONERA)Inventors: Guillaume Druart, Tatiana Grulois, Nicolas Guerineau, Joël Deschamps
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Patent number: 10036552Abstract: An air and fuel injection system for a turbine engine combustion chamber dome, including at least two fuel injection devices including a central injector and a peripheral annular injector arranged around the central injector, and an inner annular air inlet channel into which the central injector opens up to enable mixing between the fuel from the central injector and the air inlet into the inner annular channel, and at least one outer annular air inlet channel to enable enrichment of this mix with air and to stabilize the pilot combustion zone, wherein the inner annular channel and at least one outer annular channel are separated by an intermediate annular wall extending around the central injector and having a convergent inner profile.Type: GrantFiled: March 14, 2014Date of Patent: July 31, 2018Assignees: SNECMA, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Matthieu Francois Rullaud, Didier Hernandez, Christian Guin
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Patent number: 9796581Abstract: The invention relates to a process for fabricating a high-precision object made of at least one inorganic material, comprising the following steps: using a high-resolution photolithography process, employing X-rays or UV rays depending on the desired degree of precision, in a chosen direction Z, to form a negative mold, which does not deform at the microscale during the steps of the process, in a material able to withstand a step for forming the object by dry deposition and capable of either being removed without altering the object fabricated or being separated from said object; choosing, independently of the normal redox potential of its constituent elements, at least one inorganic material from the set of materials that can be deposited by dry deposition and that allow the object to be fabricated to meet its thermomechanical and environmental specifications; and forming, by means of the non-deformable negative mold, the object to be fabricated by dry deposition of said at least one inorganic material, therType: GrantFiled: December 26, 2011Date of Patent: October 24, 2017Assignee: ONERA (OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES)Inventors: Stéphane Landais, Fayçal Bouamrane, Thomas Bouvet, Olivier Dessornes, Pierre Josso, Stéphan Megtert, Roger Valle
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Patent number: 9640166Abstract: A soundproof panel has a sandwich structure, which includes two outer walls, a core, and modifying elements that are maintained in a fractal distribution by the core. The panel has an improved trade-off between sound attenuation efficiency and the weight of the panel.Type: GrantFiled: January 28, 2015Date of Patent: May 2, 2017Assignees: ONERA (OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES), ATECAInventors: Frank Simon, Jean-Luc Brian, Valia Fascio, Philippe Vie
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Patent number: 9591741Abstract: The invention, which relates to a miniaturizable plasma thruster, consists of: —igniting the plasma by microhollow cathode discharge close to the outlet and inside the means for injecting the propellant gas, said injection means being magnetic and comprising a tip at the downstream end thereof; —bringing the electrons of the magnetized plasma into gyromagnetic rotation, at the outlet end of said injection means; —sustaining the plasma by means of Electron Cyclotron Resonance (ECR), said injection means being metal and being used as an antenna for electromagnetic (EM) emission, the volume of ECR plasma at the outlet of said injection means being used as a resonant cavity of the EM wave; —accelerating the plasma in a magnetic nozzle by diamagnetic force, the ejected plasma being electrically neutral.Type: GrantFiled: December 19, 2012Date of Patent: March 7, 2017Assignee: ONERA (Office National d'Etudes et de Recherches Aerospatiales)Inventor: Serge Larigaldie
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Publication number: 20170012401Abstract: According to one aspect, the invention relates to a device comprising an optical fibre having a high Brillouin threshold, said device including an optical fibre (101) suitable for propagating a high-power optical signal beam, means (11) for coupling a signal beam to an entrance end of the optical fibre (101) and a tubular structure (10) comprising at least one first tube (103) and at least one first adhesive material (102). According to the present description, at least one portion of the optical fibre is immobilized in the tubular structure (10) by means of the first adhesive material (102), which adheres both to the internal surface of the first tube (103) and to the external surface of the optical fibre (101).Type: ApplicationFiled: January 23, 2015Publication date: January 12, 2017Applicant: Office National d'Etudes et de Recherches Aérospatiales-ONERAInventors: Guillaume Canat, William Renard, Laurent Lombard, Didier Fleury
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Patent number: 9494472Abstract: The invention is a device for measuring the temperature of the vibrating beam of a vibrating-beam sensor. It comprises a resonator (10) vibrating in torsion in resonant mode and exhibiting a torsional vibration node (N), said node being its zone of fixing in the vicinity of the middle of the length (L3) of the vibrating beam, said fixing allowing thermal transfers between the resonator and the beam. The frequency of the resonator and the variations of this frequency are representative respectively of the mean temperature T of the beam and of the variations of this temperature T, the effects of which may be compensated by a model.Type: GrantFiled: January 23, 2012Date of Patent: November 15, 2016Assignee: OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA)Inventors: Oliver Le Traon, Claude Chartier, Vincent Gaudineau, Jean Guerard, Denis Janiaud, Raphaël Levy
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Publication number: 20160281991Abstract: An air and fuel injection system for a turbine engine combustion chamber dome, including at least two fuel injection devices including a central injector and a peripheral annular injector arranged around the central injector, and an inner annular air inlet channel into which the central injector opens up to enable mixing between the fuel from the central injector and the air inlet into the inner annular channel, and at least one outer annular air inlet channel to enable enrichment of this mix with air and to stabilise the pilot combustion zone, wherein the inner annular channel and at least one outer annular channel are separated by an intermediate annular wall extending around the central injector and having a convergent inner profile.Type: ApplicationFiled: March 14, 2014Publication date: September 29, 2016Applicants: SNECMA, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Matthieu Francois RULLAUD, Didier HERNANDEZ, Christian GUIN
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Publication number: 20160233412Abstract: An actuator providing a large shear movement in a chosen direction. The angle of inclination of the fibres relative to the chosen direction is larger than 2° and smaller than 40°; the spaces between the piezoelectric fibres of the active layer are filled with an incompressible elastic material; the active layer comprises at least two dimensionally stable elongate elements parallel to the chosen direction; the ends of each fibre are adhesively bonded to said dimensionally stable elements using a rigid adhesive; and said dimensionally stable elements are adhesively bonded, by a rigid adhesive, to said electrode-bearing layers.Type: ApplicationFiled: September 11, 2014Publication date: August 11, 2016Applicant: Office National d'Études et de Recherches Aérospatiales (ONERA)Inventors: Hugues MERCIER DES ROCHETTES, Didier JOLY
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Patent number: 9363484Abstract: A method for range imaging allows determining respective distances to multiple objects, based on a single image. The image is captured through a component having a transmittance function of which the Fourier transform is inscribed on a circle within a plane of spatial frequencies. A Fourier transform of the captured image is calculated in order to obtain a total spectrum for the image content. The distance to each object is then calculated based on several homothetic superimpositions of a reference spectrum with the total spectrum, so that said reference spectrum coincides with a portion of the total spectrum each time.Type: GrantFiled: August 21, 2013Date of Patent: June 7, 2016Assignee: ONERA (Office National d'Etudes et de Recherches Aerospatiales)Inventors: Martin Piponnier, Jerome Primot, Guillaume Druart, Nicolas Guerineau
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Patent number: 9316541Abstract: The imaging system for imaging field rays comprises a detection surface, a device for focusing the field rays with said detection surface, and a diaphragm. Said device comprises a Fresnel lens comprising a first dioptre, the non-plane surface of which, called the active zone, makes it possible to focus the field rays towards said detection surface, and said diaphragm allows controlled distribution of the field rays over said active zone.Type: GrantFiled: April 16, 2012Date of Patent: April 19, 2016Assignees: OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA), ULISInventors: Guillaume Druart, Florence De La Barriere, Arnaud Crastes
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Patent number: 9315376Abstract: An inertial sensor for measuring information relating to rotation in three orthogonal axes, comprising a support and a vibrating sensitive element secured to the support; the sensitive element having a deformable frame and at least two deformable projections which extend in a plane (X-Y); wherein the inertial sensor extends in the same plane; the deformable frame and the at least two deformable projections have a plane of symmetry parallel to the plane; the at least two projections are rectilinear beams which have an approximately square cross section, are not collinear and are preferably approximately orthogonal to one another; each of the deformable beams being connected by only one end to the deformable frame at a location at which the amplitude of the primary vibration mode is at a maximum; and in that the sensor has a device for detecting each of the secondary vibration modes.Type: GrantFiled: December 20, 2011Date of Patent: April 19, 2016Assignee: ONERA (OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES)Inventors: Iannis Roland, Steve Masson, Olivier Ducloux
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Patent number: 9302946Abstract: The invention relates to a process for producing a ceramic matrix composite (CMC) part by infiltration of a suspension (S) of a ceramic powder into a fibrous reinforcement (14). A suspension (S) of ceramic powder containing particles of chosen particle size, dispersed in at least one solvent, is prepared. The infiltration of the suspension is carried out in a single step in the fibrous reinforcement (14) positioned between a mold (12) and a permeable membrane (16), which makes it possible to apply a vacuum (V) and to subsequently remove the solvent from the suspension through the permeable membrane (16). The invention applies to the production of large-sized parts of complex shape, in particular in the field of aeronautics and aerospace engineering.Type: GrantFiled: April 18, 2011Date of Patent: April 5, 2016Assignee: OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA)Inventors: Marie-Hélène Ritti, Bertrand Laine, Michel Parlier, Aurélie Julian-Jankowiak
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Patent number: 9281555Abstract: Method and monopole antenna for making uniform the radiation of the antenna, when disposed inside a radome. According to the invention, on the surface of the monopole antenna is formed a protruding longitudinal ridge which is disposed at least approximately opposite an area of the radiating pattern of the assembly radome (1)-monopole antenna having a reduced gain in comparison with the radiating pattern of said monopole antenna alone.Type: GrantFiled: February 21, 2014Date of Patent: March 8, 2016Assignees: Airbus Operations (S.A.S.), ONERA (Office national d'études et de recherches aérospatiales)Inventor: Hervé Jeuland
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Patent number: 9236704Abstract: According to one aspect, the invention relates to an optic fiber amplifier having a high Brillouin threshold, and including: an amplification optic fiber (16) comprising a core and a sheath and suitable for amplifying a signal beam travelling in said core; means for coupling the signal beam in an input end of said amplification optic fiber; means for coupling a pump laser beam for pumping said amplification optic fiber; a structure (330, 340) including a deformable portion around which at least one portion of said amplification optic fiber is wound in the shape of turns, said turns being in contact with a surface of said deformable portion, wherein the friction of said optic fiber on said surface resulting, during the deformation of said deformable portion, in an elongation of said amplification optic fiber according to an elongation profile that varies from one turn to the other.Type: GrantFiled: July 2, 2013Date of Patent: January 12, 2016Assignee: Office National d'Etudes et de Recherches Aérospatiales-ONERAInventors: Guillaume Canat, Laurent Lombard, Julien Le Gouët, Didier Fleury
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Publication number: 20150301333Abstract: According to one aspect, the invention relates to a device (20, 50) for controlling the phase of an incident optical wavefront of wavelength comprised in a spectral band of given use, comprising a substrate (21) that is at least partially transparent in said spectral band and a set of strips (22i, 23i, 24i) arranged substantially perpendicularly to the surface of the substrate, characterised in that: said set of strips comprises an alternation of juxtaposed strips respectively made of a metal (22i), of a first dielectric (23i) and of at least one second dielectric (24i) different from the first dielectric, such as to form juxtaposed metal/multi dielectric/metal (MmultiDM) structures (Si) of subwavelength widths (wi), each structure forming a cavity having one or more propagation modes—the respective thicknesses of the strips made of the first dielectric and of the second dielectric(s) are adjusted in each of said MmultiDM structures to induce a local shift (??i) in the phase of the wavefront, the local phaseType: ApplicationFiled: November 29, 2013Publication date: October 22, 2015Applicant: Office National d'Etudes et de Recherches Aérospatiales-ONERAInventors: Quentin Levesque, Patrick Bouchon, Riad Haidar, Fabrice Pardo
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Patent number: 9110197Abstract: Device and method for anticipating the deposition of ice on a runway, comprising an object having a non-zero relative velocity with respect to the atmosphere surrounding the runway, this surrounding atmosphere being at a certain temperature, a means for determining the thickness of ice present on said moving object, which further includes a temperature sensor for measuring the temperature of the runway, a means for regulating the temperature of said object in such a way that the temperature of said moving object is substantially equal to or slightly below the temperature of the runway, a computing means, for defining at time t0 a level of icing at time t1 of the runway as a function of the thickness of ice present on the object, and a warning means allowing the results obtained by the computing means to be communicated to a monitoring station.Type: GrantFiled: October 13, 2011Date of Patent: August 18, 2015Assignees: AER, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA)Inventors: Didier Guffond, Robert Schegerin, Hervé Lachaud