Patents by Inventor Matthieu Simon

Matthieu Simon 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).

  • Publication number: 20250129967
    Abstract: A thermal system for a facility includes a facility fluid circuit, a ground-source heat pump, and an air-source heat pump. The ground-source heat pump and the air-source heat pump each include a fluid circuit connected to the facility fluid circuit in parallel via a common facility heat exchanger. The ground-source heat pump includes a ground-source heat exchanger for transferring heat between a ground-source working fluid and a downhole fluid of a downhole fluid circuit. The air-source heat pump includes an air-source heat exchanger for transferring heat between an air-source working fluid and an ambient air. Heat can be transferred, at the facility heat exchanger, between the facility fluid and one or more of the ground-source working fluid or the air-source working fluid in order to provide thermal heating, cooling, or both to the facility.
    Type: Application
    Filed: October 23, 2024
    Publication date: April 24, 2025
    Inventors: Olivier Lecoq, Matthieu Simon
  • Publication number: 20250129965
    Abstract: A thermal system for providing thermal conditioning to a facility includes a facility air circuit for circulating a facility air throughout the facility and a downhole fluid circuit for circulating a downhole fluid. The facility air circuit is thermally connected to a heat pump for exchanging heat with the facility air. The downhole fluid circuit includes the heat pump for exchanging heat with the downhole fluid, a main loop, including a borehole heat exchanger (BHE) for exchanging heat between the downhole fluid and a geological formation, and an exhaust loop including an exhaust heat exchanger coupled to an exhaust of the facility air circuit, wherein the exhaust loop is configured to circulate at least some of the downhole fluid through the exhaust heat exchanger to exchange heat between the downhole fluid and an exhaust flow of the facility air exhausted from the facility at the exhaust.
    Type: Application
    Filed: October 23, 2024
    Publication date: April 24, 2025
    Inventors: Olivier Lecoq, Matthieu Simon
  • Patent number: 12282971
    Abstract: An energy management system for enhancing design and operation of a distributed energy resource system includes a two-level design system and a hierarchical optimization-based control system. The two-level design system includes a top-level designer configured to coordinate decentralized bottom-level designers for individual energy resources to seek a global target for the designed distributed energy resource system that satisfies the energy demand of a target deployment location within a confidence level, and multiple bottom-level designers configured to enhance detailed designs of local energy sub-systems.
    Type: Grant
    Filed: May 14, 2021
    Date of Patent: April 22, 2025
    Assignee: SCHLUMBERGER TECHNOLOGY CORPORATION
    Inventors: Ines da Mata Cecilio, Matthieu Simon, Simon Bittleston, Sylvain Thierry
  • Publication number: 20250034969
    Abstract: A wellhead container for a geothermal system includes a base configured to engage a bottom of a recess within a ground. The recess extends vertically from the bottom of the recess to a surface of the ground, the base includes at least one first opening, and the at least one first opening is configured to receive a drilling string. The wellhead container includes a top configured to support a load applied by a drilling machine to the wellhead container. The top includes second openings, and each second opening is configured to receive the drilling string. The wellhead container includes a sidewall extending along a vertical axis between the base and the top. The sidewall is configured to position an upper surface of the top substantially flush with the surface of the ground, and the sidewall is configured to transfer at least a portion of the load to the base.
    Type: Application
    Filed: October 15, 2024
    Publication date: January 30, 2025
    Inventors: Sylvain Thierry, Matthieu Simon, Cindy Demichel, Marco Alioto
  • Publication number: 20250035003
    Abstract: The present invention relates to a turbine rotor (1) comprising a rotor disc (2), provided at its periphery with a plurality of axial cells (23) for receiving a bilobed root (30) of a blade (3), each cell (23) comprising a radially inner cavity (232) and a radially outer cavity (231). This rotor is characterised in that it comprises a ring (4) for axially retaining the blade roots and an annular flange (5), the ring (4) comprising a radially inner portion provided with notches (43) and being arranged against the upstream face (21) of the disc (2), so that each of its notches (43) is located opposite a cell (23) of the disc (2), the flange (5) being secured against the upstream face of the ring (4), forming a space (E) with said disc (2), and comprising at least one air-intake opening (54) which opens into said space (E), and in that each blade (3) comprises a groove (33) for receiving the outer circumferential edge (46) of said ring (4).
    Type: Application
    Filed: February 7, 2023
    Publication date: January 30, 2025
    Applicant: Safran Aircraft Engines
    Inventors: Patrick Jean Laurent SULTANA, Matthieu SIMON, Loic ANSART, Joao Antonio AMORIM
  • Publication number: 20250003348
    Abstract: The present invention relates to a nozzle guide vane for a turbine, having an axis of revolution and comprising: a flange extending radially relative to the axis; —a ring seal mounted on the flange and comprising an inner face that is configured to bear an abradable element; —a ventilation cavity delimited radially on the inside by an outer face of the ring seal and downstream by an upstream face of the flange; —a baffle configured to guide an airflow toward the ventilation cavity; and—at least one through-opening formed in the ring seal and configured to put the ventilation cavity in fluidic communication with the inner face of the ring seal.
    Type: Application
    Filed: October 14, 2022
    Publication date: January 2, 2025
    Applicant: Safran Aircraft Engines
    Inventors: Kenny BEAUBOIT, Matthieu SIMON, Patrick Jean Laurent SULTANA, Julian Nicolas GIRARDEAU
  • Patent number: 12146391
    Abstract: A wellhead container for a geothermal system includes a base configured to engage a bottom of a recess within a ground. The recess extends vertically from the bottom of the recess to a surface of the ground, the base includes at least one first opening, and the at least one first opening is configured to receive a drilling string. The wellhead container includes a top configured to support a load applied by a drilling machine to the wellhead container. The top includes second openings, and each second opening is configured to receive the drilling string. The wellhead container includes a sidewall extending along a vertical axis between the base and the top. The sidewall is configured to position an upper surface of the top substantially flush with the surface of the ground, and the sidewall is configured to transfer at least a portion of the load to the base.
    Type: Grant
    Filed: March 26, 2021
    Date of Patent: November 19, 2024
    Assignee: Schlumberger Technology Corporation
    Inventors: Sylvain Thierry, Matthieu Simon, Cindy Demichel, Marco Alioto
  • Publication number: 20240318836
    Abstract: Certain aspects of the present disclosure provide techniques for recovery of waste energy from a battery energy storage system. A system includes a battery energy storage system including one or more rechargeable batteries; an energy recovery system coupled to the battery energy storage system, wherein the energy recovery system is configured to: capture heat generated by one or more of charging and discharging the one or more rechargeable batteries; and store or use energy associated with the captured heat.
    Type: Application
    Filed: May 16, 2023
    Publication date: September 26, 2024
    Inventors: Julien Toniolo, Matthieu Simon
  • Publication number: 20240318537
    Abstract: A method of producing a geothermal well includes obtaining site information including at least a site volume; obtaining drilling parameters; determining lengths and orientations of planned wellbores based at least partially on the site information and the drilling parameters.
    Type: Application
    Filed: March 22, 2024
    Publication date: September 26, 2024
    Inventors: Pontus Loviken, Matthieu Simon, Josselin Kherroubi, Andrew J. Parry, Ronan Meneu, Olivier Bernard, Delphine Coutrot, Elodie Daynac
  • Patent number: 12055674
    Abstract: The current disclosure is related to a downhole tool that comprises an electronic photon generator and at least one detector. The electronic photon generator comprises a cathode configured to emit electrons, a first target configured to generate photons when struck by the electrons, a second target configured to generate photons when struck by the electrons, and a beam steering device that directs the electrons to a first or second target. The at least one detector is configured to detect at least some of the photons emitted by the first target and at least some of the photons emitted by the second target.
    Type: Grant
    Filed: December 14, 2020
    Date of Patent: August 6, 2024
    Assignee: Schlumberger Technology Corporation
    Inventors: Matthieu Simon, Christian Stoller
  • Patent number: 11795828
    Abstract: A blade for a turbomachine intended to be disposed about an axis while extending radially between a radially outer end and a radially inner end, the blade having at least one cooling cavity opening out to the radially outer end of the blade and to the radially inner end of the blade, the blade having at least a first tubular liner and at least a second tubular liner each engaged in the cavity, the radially outer end of the first liner opening out to the radially outer end of the blade, and the radially inner end of the second liner opening out to the radially inner end of the blade.
    Type: Grant
    Filed: March 16, 2020
    Date of Patent: October 24, 2023
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Matthieu Simon, Jean-Luc Bacha, Paul Danre, Léandre Ostino
  • Publication number: 20230296023
    Abstract: A turbine has a first rotor and a second rotor configured to pivot about a longitudinal axis (X) according to two opposite directions of rotation. The first rotor has a radially outer drum from which bladesextend radially inwards. The first rotorand the second rotor are surrounded by a stator annular part. The stator annular partdelimits, with the drum, at least one upstream annular cavityand one downstream annular cavityseparated from each other by sealing means.
    Type: Application
    Filed: July 22, 2021
    Publication date: September 21, 2023
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Matthieu SIMON, Ulysse Jacques Bernard DANTENY
  • Publication number: 20230107830
    Abstract: A wellhead container for a geothermal system includes a base configured to engage a bottom of a recess within a ground. The recess extends vertically from the bottom of the recess to a surface of the ground, the base includes at least one first opening, and the at least one first opening is configured to receive a drilling string. The wellhead container includes a top configured to support a load applied by a drilling machine to the wellhead container. The top includes second openings, and each second opening is configured to receive the drilling string. The wellhead container includes a sidewall extending along a vertical axis between the base and the top. The sidewall is configured to position an upper surface of the top substantially flush with the surface of the ground, and the sidewall is configured to transfer at least a portion of the load to the base.
    Type: Application
    Filed: March 26, 2021
    Publication date: April 6, 2023
    Inventors: Sylvain Thierry, Matthieu Simon, Cindy Demichel, Marco Alioto
  • Patent number: 11566495
    Abstract: A downhole tool may include a high-voltage power supply disposed within a housing to transform input power to the downhole tool from a first voltage to a second voltage greater than the first voltage. The high-voltage power supply may include an array of capacitors, which may include multiple rows of capacitors. The rows of capacitors may be parallel with a symmetric cross section as viewed from an end of the array of capacitors. The high-voltage power supply may also include diodes electrically coupled to the array of capacitors.
    Type: Grant
    Filed: December 20, 2019
    Date of Patent: January 31, 2023
    Assignee: SCHLUMBERGER TECHNOLOGY CORPORATION
    Inventors: Jani Reijonen, Giovana Stefan, Austin Jones, Matthieu Simon, Anthony Durkowski, Marc-Andre de Looz, Justin Mlcak
  • Patent number: 11402536
    Abstract: A downhole tool may include a voltage multiplier within a housing. The voltage multiplier may transform input power to the downhole tool from a first voltage to a second voltage higher than the first. The downhole tool may also include multiple shielding rings surrounding at least the voltage multiplier to reduce electric field stresses within the downhole tool. Additionally, the downhole tool may include an insulator located between the shielding rings and the housing.
    Type: Grant
    Filed: July 17, 2020
    Date of Patent: August 2, 2022
    Assignee: SCHLUMBERGER TECHNOLOGY CORPORATION
    Inventors: Matthieu Simon, Jani Reijonen
  • Patent number: 11389860
    Abstract: A hollow turbomachine turbine blade including rising cavities communicating with a squealer tip of the blade through standard dust removal holes intended to remove dust and through inclined cooling bores intended to cool a barrier of the squealer tip by leading to a pressure side face of the blade, at least one rising cavity including a tip with no dust removal hole and an inclined cooling bore formed in its lateral wall and intended to cool the squealer tip barrier is enlarged to have a diameter at least equal to the standard diameter of a dust removal hole and thus also serve as a dust removal hole, so that the air flow extracted for cooling the blade is reduced, at least one of the cavities positioned facing the tip of one of the rising cavities having an increased volume corresponding to at least a volume deducted from the tip of the rising cavity.
    Type: Grant
    Filed: October 11, 2018
    Date of Patent: July 19, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Leandre Ostino, Matthieu Simon
  • Publication number: 20220170377
    Abstract: A blade for a turbomachine intended to be disposed about an axis while extending radially between a radially outer end and a radially inner end, the blade having at least one cooling cavity opening out to the radially outer end of the blade and to the radially inner end of the blade, the blade having at least a first tubular liner and at least a second tubular liner each engaged in the cavity, the radially outer end of the first liner opening out to the radially outer end of the blade, and the radially inner end of the second liner opening out to the radially inner end of the blade.
    Type: Application
    Filed: March 16, 2020
    Publication date: June 2, 2022
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Matthieu SIMON, Jean-Luc BACHA, Paul DANRE, Léandre OSTINO
  • Publication number: 20210358058
    Abstract: An energy management system for enhancing design and operation of a distributed energy resource system includes a two-level design system and a hierarchical optimization-based control system. The two-level design system includes a top-level designer configured to coordinate decentralized bottom-level designers for individual energy resources to seek a global target for the designed distributed energy resource system that satisfies the energy demand of a target deployment location within a confidence level, and multiple bottom-level designers configured to enhance detailed designs of local energy sub-systems.
    Type: Application
    Filed: May 14, 2021
    Publication date: November 18, 2021
    Inventors: Ines da Mata Cecilio, Matthieu Simon, Simon Bittleston, Sylvain Thierry
  • Publication number: 20210189838
    Abstract: A downhole tool may include a high-voltage power supply disposed within a housing to transform input power to the downhole tool from a first voltage to a second voltage greater than the first voltage. The high-voltage power supply may include an array of capacitors, which may include multiple rows of capacitors. The rows of capacitors may be parallel with a symmetric cross section as viewed from an end of the array of capacitors. The high-voltage power supply may also include diodes electrically coupled to the array of capacitors.
    Type: Application
    Filed: December 20, 2019
    Publication date: June 24, 2021
    Inventors: Jani Reijonen, Giovana Stefan, Austin Jones, Matthieu Simon, Anthony Durkowski, Marc-Andre de Looz, Justin Mlcak
  • Publication number: 20210187594
    Abstract: A hollow turbomachine turbine blade including rising cavities communicating with a squealer tip of the blade through standard dust removal holes intended to remove dust and through inclined cooling bores intended to cool a barrier of the squealer tip by leading to a pressure side face of the blade, at least one rising cavity including a tip with no dust removal hole and an inclined cooling bore formed in its lateral wall and intended to cool the squealer tip barrier is enlarged to have a diameter at least equal to the standard diameter of a dust removal hole and thus also serve as a dust removal hole, so that the air flow extracted for cooling the blade is reduced, at least one of the cavities positioned facing the tip of one of the rising cavities having an increased volume corresponding to at least a volume deducted from the tip of the rising cavity.
    Type: Application
    Filed: October 11, 2018
    Publication date: June 24, 2021
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Leandre OSTINO, Matthieu SIMON