Patents by Inventor Antoine Costeux

Antoine Costeux 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).

  • Patent number: 11652393
    Abstract: A rotor assembly for an electric motor for a turbomachine defines an axis of rotation. The rotor assembly includes a jacket member that is hollow and that defines an inner radial surface facing inwardly toward the axis of rotation. Furthermore, the rotor assembly includes a magnet member that is received within the jacket member. The magnet member includes an outer radial surface facing outwardly from the axis of rotation. The jacket member is made of a sintered composite material having carbon filament and a sintered matrix. Additionally, the inner radial surface of the jacket member abuts against the outer radial surface of the magnet member to retain the magnet member in a radial position relative to the axis.
    Type: Grant
    Filed: July 1, 2020
    Date of Patent: May 16, 2023
    Assignee: GARRETT TRANSPORTATION I INC
    Inventors: Jeffrey Lotterman, Todd Ratke, Sushank Singampalli, Antoine Costeux, Carlos Chavez Castellanos
  • Publication number: 20220006369
    Abstract: A rotor assembly for an electric motor for a turbomachine defines an axis of rotation. The rotor assembly includes a jacket member that is hollow and that defines an inner radial surface facing inwardly toward the axis of rotation. Furthermore, the rotor assembly includes a magnet member that is received within the jacket member. The magnet member includes an outer radial surface facing outwardly from the axis of rotation. The jacket member is made of a sintered composite material having carbon filament and a sintered matrix. Additionally, the inner radial surface of the jacket member abuts against the outer radial surface of the magnet member to retain the magnet member in a radial position relative to the axis.
    Type: Application
    Filed: July 1, 2020
    Publication date: January 6, 2022
    Applicant: Garrett Transportation I Inc
    Inventors: Jeffrey Lotterman, Todd Ratke, Sushank Singampali, Antoine Costeux, Carlos Chavez Castellanos
  • Patent number: 9593690
    Abstract: A turbocharger includes an annular bypass volute to allow exhaust gas to bypass the turbine wheel. An annular bypass valve is disposed in the bypass volute. The bypass valve comprises a fixed annular valve seat and a rotary annular valve member arranged coaxially with the valve seat. The valve member is disposed against the valve seat and is rotatable about the axis for selectively varying a degree of alignment between respective orifices in the valve seat and valve member. The valve member is rotatably driven by a rotary actuator and drive linkage that rotates about an axis parallel to and offset from the axis about which the valve member rotates.
    Type: Grant
    Filed: June 26, 2013
    Date of Patent: March 14, 2017
    Assignee: Honeywell International Inc.
    Inventors: Alain Lombard, Andrew Love, Antoine Costeux
  • Patent number: 9422858
    Abstract: A turbocharger includes an annular bypass passage with an annular bypass valve disposed therein. The bypass valve includes a fixed annular valve seat and a rotary annular valve member disposed against the valve seat. The valve member is rotatable about the axis for varying a degree of alignment between orifices in the valve seat and valve member so as to form flow passages having a flow area A for exhaust gas. The orifices are shaped to provide a first phase of evolution of the flow area A from zero up to a value A1 and then a second phase of evolution from the value A1 up to a value A2, and such that the first and second phases have distinctly different slopes on a curve of flow area versus rotational position of the valve member, with a distinct break point in the curve between the first and second phases.
    Type: Grant
    Filed: March 18, 2014
    Date of Patent: August 23, 2016
    Assignee: Honeywell International Inc.
    Inventors: Alain Lombard, Valerie Bribant, Antoine Costeux
  • Publication number: 20150267605
    Abstract: A turbocharger includes an annular bypass passage with an annular bypass valve disposed therein. The bypass valve includes a fixed annular valve seat and a rotary annular valve member disposed against the valve seat. The valve member is rotatable about the axis for varying a degree of alignment between orifices in the valve seat and valve member so as to form flow passages having a flow area A for exhaust gas. The orifices are shaped to provide a first phase of evolution of the flow area A from zero up to a value A1 and then a second phase of evolution from the value A1 up to a value A2, and such that the first and second phases have distinctly different slopes on a curve of flow area versus rotational position of the valve member, with a distinct break point in the curve between the first and second phases.
    Type: Application
    Filed: March 18, 2014
    Publication date: September 24, 2015
    Applicant: Honeywell International Inc.
    Inventors: Alain Lombard, Valerie Bribant, Antoine Costeux
  • Publication number: 20150004020
    Abstract: A turbocharger includes an annular bypass volute to allow exhaust gas to bypass the turbine wheel. An annular bypass valve is disposed in the bypass volute. The bypass valve comprises a fixed annular valve seat and a rotary annular valve member arranged coaxially with the valve seat. The valve member is disposed against the valve seat and is rotatable about the axis for selectively varying a degree of alignment between respective orifices in the valve seat and valve member. The valve member is rotatably driven by a rotary actuator and drive linkage that rotates about an axis parallel to and offset from the axis about which the valve member rotates.
    Type: Application
    Filed: June 26, 2013
    Publication date: January 1, 2015
    Inventors: Alain Lombard, Andrew Love, Antoine Costeux