Patents by Inventor Frederic Jean
Frederic Jean has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 11686203Abstract: The invention relates to a fibrous texture intended to form the fibrous reinforcement of a turbine engine blade made of composite material, the texture being in a single piece and having a three-dimensional weave between a plurality of first fiber warp yarns or strands extending in a radial direction and a plurality of first fiber weft yarns or strands extending in a chord direction, the texture comprising a blade root portion and a blade airfoil portion extending between the blade root portion and a free end of the fibrous texture. The blade airfoil portion has a reinforced area in the vicinity of the free end of the texture comprising weft yarns or strands made of second fibers different from the first fibers.Type: GrantFiled: February 19, 2021Date of Patent: June 27, 2023Assignee: SAFRAN AIRCRAFT ENGINESInventors: Frédéric Jean-Bernard Pouzadoux, Jérémy Guivarc'h, Thomas Alain De Gaillard
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Publication number: 20230148181Abstract: A protein capable of converting chlorogenic acid into isochlorogenic acid. The protein includes or is an amino acid sequence SEQ ID No. 1, a sequence having at least 80% identity with this sequence or a fragment of this sequence. Also, a process for producing isochlorogenic acid from chlorogenic acid, which includes producing the protein and bringing it into contact with chlorogenic acid.Type: ApplicationFiled: March 12, 2021Publication date: May 11, 2023Applicants: UNIVERSITE DE LORRAINE, UNIVERSITE DE LILLE, CELLENGOInventors: Frédéric Jean BOURGAUD, Sissi MIGUEL, Aleksander SALWINSKI, Cindy SIGNE, Alain HEHN, Jean-Louis HILBERT, David GAGNEUL, Guillaume LEGRAND
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Publication number: 20230144698Abstract: A heat exchanger for an electrical element is provided. The heat exchanger includes a first plate, a second plate adapted to contact the electrical element and a plurality of heat exchange channels. The plurality of heat exchange is between the first and second plates to enable heat exchange between a fluid flowing in the plurality of heat exchange channels and the electrical element. The heat exchanger further includes a first portion and a second portion. The first portion of the heat exchange channels is in thermal contact with a first of the electrical elements and the second portion of the heat exchange channels is in thermal contact with a second of the electrical elements.Type: ApplicationFiled: March 31, 2021Publication date: May 11, 2023Inventors: Frederic Jean Alain Bodino, Melissa Dawn Lee Hudson, Paul Xavier Martens, Claudiu Neagu, Marc Karman
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Publication number: 20230113922Abstract: The invention relates to a fibrous texture intended to form the fibrous reinforcement of a turbine engine blade made of composite material, the texture being in a single piece and having a three-dimensional weave between a plurality of first fiber warp yarns or strands extending in a radial direction and a plurality of first fiber weft yarns or strands extending in a chord direction, the texture comprising a blade root portion and a blade airfoil portion extending between the blade root portion and a free end of the fibrous texture. The blade airfoil portion has a reinforced area in the vicinity of the free end of the texture comprising weft yarns or strands made of second fibers different from the first fibers.Type: ApplicationFiled: February 19, 2021Publication date: April 13, 2023Applicant: SAFRAN AIRCRAFT ENGINESInventors: Frédéric Jean-Bernard POUZADOUX, Jérémy GUIVARC'H, Thomas Alain DE GAILLARD
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Patent number: 11593111Abstract: An apparatus and method are provided for inhibiting instruction manipulation. The apparatus has execution circuitry for performing data processing operations in response to a sequence of instructions from an instruction set, and decoder circuitry for decoding each instruction in the sequence in order to generate control signals for the execution circuitry. Each instruction comprises a plurality of instruction bits, and the decoder circuitry is arranged to perform a decode operation on each instruction to determine from the value of each instruction bit, and knowledge of the instruction set, the control signals to be issued to the execution circuitry in response to that instruction. An input path to the decoder circuitry comprises a set of wires over which the instruction bits of each instruction are provided.Type: GrantFiled: January 27, 2020Date of Patent: February 28, 2023Assignee: Arm LimitedInventors: Frederic Jean Denis Arsanto, Carlo Dario Fanara, Luca Scalabrino, Jean Sébastien Leroy
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Patent number: 11504664Abstract: An adapter (1) for use in a dedicated coupling system (2) for releasably coupling an air filter cartridge (20) and a housing (36) of a dedicated air filter assembly (34), the adapter (1) comprising: a first surface area (4) being rotatably coupleable with a housing-side coupling element (6) of the coupling system (2), and a second surface area (8) preferably being non-rotatably coupleable. Cartridges, components, features and methods are described.Type: GrantFiled: May 8, 2018Date of Patent: November 22, 2022Assignee: Donaldson Company, Inc.Inventors: Sebastien Olivier Bessone, Paul Gerard Gallais, Frederic Jean Jordi Miralles
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Patent number: 11479725Abstract: An improved process is provided for catalytic pyrolysis of biomass, comprising pneumatically injecting a biomass feed via a pneumatic injection line into a fluidized heat medium, for example, hot catalyst, with a carrier gas at a velocity of from 5 to 40 m/s in at least one mixing zone in communication with a pyrolysis reactor in which catalytic pyrolysis occurs, and maintaining a catalyst/biomass mixture flowrate ratio (C/B) of from 4 to 40 downstream from the point of catalyst injection via a catalyst injection line in the at least one mixing zone.Type: GrantFiled: July 16, 2019Date of Patent: October 25, 2022Assignee: ANELLOTECH, INC.Inventors: Benjamin Thomas Amblard, Raghava Dasarathy, Frédéric Jean-Michel Feugnet, Thierry Albert Pierre Gauthier, Eugene Schmelzer, Charles Mitchel Sorensen, Jr., Sina Tebianian
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Patent number: 11449642Abstract: An electronic circuit includes a plurality of processing elements, a register bank, and a control circuit. The processing elements consume power by processing a plurality of operands to generate a plurality of result values. The register bank has a plurality of registers. The control circuit is configured to determine one or more unused processing elements among the processing elements by snooping one or more incoming operands and an instruction type, control routing of one or more random operands from the register bank to the unused processing elements, and control routing of a random result value generated by one of the unused processing elements into a trash register of the registers. The power consumed by the unused processing elements in the generation of the random result value and a write of the random result value into the trash register temporally blurs a total power consumed by the electronic circuit.Type: GrantFiled: September 4, 2020Date of Patent: September 20, 2022Assignee: Arm LimitedInventors: Carlo Dario Fanara, Frederic Jean Denis Arsanto, Luca Scalabrino
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Patent number: 11434430Abstract: A process comprising separating from a biomass catalytic pyrolysis process effluent, a naphthalene-rich oil phase, a phenolic oil and a vapor phase containing off gas, water and BTX, whereby said vapor phase can be condensed to separate liquid water and liquid hydrocarbons from gaseous off gas and BTX.Type: GrantFiled: July 27, 2017Date of Patent: September 6, 2022Assignee: ANELLOTECH, INC.Inventors: Romina Digne, Cristina Ruiz Martinez, Alexandre Bernard Pagot, Marc François Philippe Jacquin, Frédéric Jean-Michel Feugnet, Charles Mitchel Sorensen
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Patent number: 11280197Abstract: A turbine unit for an aircraft turbine engine, comprises a rotor disc (17) axially continued by a rim (36) and carrying rotary blades (18) defining together with the disc (17) channels for air flow (43); an annular flange (33) including a bearing end (34) and defining together with the rim (36) an air passage (42) communicating with the channels for air flow (43); a member (32) for axially retaining the blades applied against the disc (17) by the bearing end (34), this turbine unit being characterised in that at least one element, out of the retaining member (32) and the flange (33), comprises a groove (44) formed facing the other element, out of the retaining member (32) and the flange (33), and into which a sealing joint (45) against which the other element axially bears is inserted.Type: GrantFiled: February 11, 2020Date of Patent: March 22, 2022Assignee: SAFRAN AIRCRAFT ENGINESInventors: Camille Maryse Martine Palomba, Erwan Perrot, Antoine Frédéric Jean Satre, Marc-Antoine Anatole Got
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Publication number: 20220075901Abstract: An electronic circuit includes a plurality of processing elements, a register bank, and a control circuit. The processing elements consume power by processing a plurality of operands to generate a plurality of result values. The register bank has a plurality of registers. The control circuit is configured to determine one or more unused processing elements among the processing elements by snooping one or more incoming operands and an instruction type, control routing of one or more random operands from the register bank to the unused processing elements, and control routing of a random result value generated by one of the unused processing elements into a trash register of the registers. The power consumed by the unused processing elements in the generation of the random result value and a write of the random result value into the trash register temporally blurs a total power consumed by the electronic circuit.Type: ApplicationFiled: September 4, 2020Publication date: March 10, 2022Applicant: Arm LimitedInventors: Carlo Dario Fanara, Frederic Jean Denis Arsanto, Luca Scalabrino
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Publication number: 20210372428Abstract: The invention relates to a blade (3) of a fan (1) of a turbomachine having a structure made of a composite material comprising a fibrous reinforcement (5) obtained by three-dimensional weaving and a matrix in which the fibrous reinforcement (5) is embedded, the fibrous reinforcement (5) comprising first strands (9) having a predetermined elongation at break, a portion of the fibrous reinforcement (5) further comprising second strands (10) having an elongation at break higher than that of the first strands (9).Type: ApplicationFiled: October 30, 2019Publication date: December 2, 2021Applicant: SAFRAN AIRCRAFT ENGINESInventors: Thomas Alain DE GAILLARD, Gilles Pierre-Marie NOTARIANNI, Frédéric Jean-Bernard POUZADOUX
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Patent number: 11131196Abstract: A leading-edge shield for a turbomachine blade includes a pressure-side wing and a suction-side wing. Both the pressure-side wing and suction-side wing extend heightwise from a bottom edge to a top edge and lengthwise from the leading edge to a respective rear edge. They are connected together via the leading edge. The rear edge of the suction-side wing presents at least one shaped segment that is shaped in such a manner that the length of the suction-side wing within this segment is shorter than the length of the suction-side wing at each end of this segment.Type: GrantFiled: December 21, 2016Date of Patent: September 28, 2021Assignee: SAFRAN AIRCRAFT ENGINESInventors: Frédéric Jean-Bernard Pouzadoux, Alain Jacques Michel Bassot, Jérémy Guivarc'h, Jean-Louis Romero, Thibault Ruf
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Patent number: 11105210Abstract: The invention provides a blade (16) comprising a blade body (30) made of organic matrix composite material reinforced by fibers and a leading edge shield (32) made of a material that withstands point impacts better than the composite material of the blade body. The leading edge shield (32) is assembled on the blade body (30) and the blade (16) includes bonding reinforcement (46) adhesively bonded on the leading edge shield (32) and on the blade body (16). The invention also provides a turbojet including a fan including such blades, and also a method of fabricating such a blade.Type: GrantFiled: September 27, 2016Date of Patent: August 31, 2021Assignee: SAFRAN AIRCRAFT ENGINESInventors: Matthieu Arnaud Gimat, Jérémy Guivarc'h, Gilles Pierre-Marie Notarianni, Frédéric Jean-Bernard Pouzadoux, Thibault Ruf
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Publication number: 20210232396Abstract: An apparatus and method are provided for inhibiting instruction manipulation. The apparatus has execution circuitry for performing data processing operations in response to a sequence of instructions from an instruction set, and decoder circuitry for decoding each instruction in the sequence in order to generate control signals for the execution circuitry. Each instruction comprises a plurality of instruction bits, and the decoder circuitry is arranged to perform a decode operation on each instruction to determine from the value of each instruction bit, and knowledge of the instruction set, the control signals to be issued to the execution circuitry in response to that instruction. An input path to the decoder circuitry comprises a set of wires over which the instruction bits of each instruction are provided.Type: ApplicationFiled: January 27, 2020Publication date: July 29, 2021Inventors: Frederic Jean Denis ARSANTO, Carlo Dario FANARA, Luca SCALABRINO, Jean Sébastien LEROY
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Publication number: 20210187423Abstract: An adapter (1) for use in a dedicated coupling system (2) for releasably coupling an air filter cartridge (20) and a housing (36) of a dedicated air filter assembly (34), the adapter (1) comprising: a first surface area (4) being rotatably coupleable with a housing-side coupling element (6) of the coupling system (2), and a second surface area (8) preferably being non-rotatably coupleable. Cartridges, components, features and methods are described.Type: ApplicationFiled: May 8, 2018Publication date: June 24, 2021Applicant: Donaldson Company, Inc.Inventors: Sebastien Olivier BESSON, Paul Gerard GALLAIS, Frederic Jean Jordi MIRALLES
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Patent number: 10914184Abstract: A turbine includes a stator and a movable rotor, rotating around an axis, in relation to the stator. The rotor comprises at least one disc, the radially outer periphery of which comprises cavities. The rotor further includes blades, each having a blade root axially engaged in a cavity of the disc so as to radially hold the blade on the disc. At least one of the blade roots has an axially flaring shape, with the corresponding cavity having a matching shape so as to axially lock the blade root in the cavity in a first axially oriented direction. Locking means lock the blade root in the cavity in a second axially oriented direction, opposite the first direction.Type: GrantFiled: August 17, 2018Date of Patent: February 9, 2021Assignee: SAFRAN AIRCRAFT ENGINESInventors: Antoine Frederic Jean Satre, Simon Jean-Marie Bernard Cousseau, Erwan Perrot
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Patent number: 10902113Abstract: Data processing circuitry comprises a set of two or more computational units to perform respective computational operations; an instruction decoder to decode successive data processing instructions and, for a given data processing instruction, to control one or more of the computational units to perform those computational operations required to execute the given data processing instruction; and control circuitry responsive to the given data processing instruction, to control one or more others of the computational units to perform further computational operations, other than the computational operations required to execute the given data processing instruction, during execution of the given data processing instruction.Type: GrantFiled: October 25, 2017Date of Patent: January 26, 2021Assignee: ARM LimitedInventors: Guillaume Schon, Frederic Jean Denis Arsanto, Carlo Dario Fanara, Jocelyn François Orion Jaubert
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Patent number: 10883374Abstract: A blade including a blade body made of organic matrix composite material and a leading edge shield made of a material that withstands point impacts better than the composite material of the blade body. The blade includes a blade tip. The leading edge shield is assembled on the blade body and includes a pressure-side fin and a suction-side fin. The pressure-side fin includes a pressure-side tab and the suction-side fin includes a suction-side tab, the pressure-side tab and the suction-side tab are folded one on the other and being secured to each other so as to form a partial covering of the blade tip. A turbojet includes a fan including such blades, and also a method of fabricating such a blade.Type: GrantFiled: September 27, 2016Date of Patent: January 5, 2021Assignee: SAFRAN AIRCRAFT ENGINESInventors: Gilles Pierre-Marie Notarianni, Jeremy Guivarc'H, Frederic Jean-Bernard Pouzadoux, Dominique Raulin, Thibault Ruf
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Patent number: 10865645Abstract: The invention relates to a method (100) for manufacturing a turbomachine fan comprising a plurality of blades mounted on a disc extending along a longitudinal axis, said method comprising the following steps of: —measuring (102) at least one structural parameter of each of the blades in the cold state, and, for each of the blades, estimating (103) at least one structural parameter in operation relating to a blade from the structural parameter(s) measured on said blade in the cold state, —determining (104) an optimal sequence of the blades around the disc from the structural parameters estimated in operation for each of the blades, and —mounting (105) the blades on the disc in the optimal sequence thus determined.Type: GrantFiled: June 8, 2016Date of Patent: December 15, 2020Assignee: SAFRAN AIRCRAFT ENGINESInventors: Anthony Bernard Germain Lafitte, Jean-Frederic Pierre Joseph Bruhat, Frederic Jean-Bernard Pouzadoux, Jean-Michel Roux