Patents by Inventor Pierre Cabrera

Pierre Cabrera 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: 20250116971
    Abstract: System for controlling a device provided with at least one equipment item, the control system comprising at least one sensor capable of measuring operating quantities of the device, and two specific channels for measuring a redundant sensor for each equipment item, at least one embedded control means configured to determine a command intended for at least one equipment item as a function of the at least one measurement of the operating quantity of the device and a selected measurement of the controlled equipment item, the control system further comprising a calculating means configured to determine the selected measurement of the at least one controlled equipment item, by means of a Kalman filter observer, as a function of the at least one measurement of the operating quantity of the device and the measurements of the two specific channels for measuring a redundant sensor for the controlled equipment item.
    Type: Application
    Filed: January 16, 2023
    Publication date: April 10, 2025
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Seif Eddine Benattia, Pierre Cabrera
  • Patent number: 12176793
    Abstract: The invention relates to a method for regulating an acceleration of a turbomachine, the turbomachine comprising a combustion chamber, a high-pressure turbine located downstream of the combustion chamber and which drives a high-pressure shaft in rotation, and a low-pressure turbine located downstream of the high-pressure turbine and which drives a low-pressure shaft in rotation, characterized in that the method comprises the following steps: injecting mechanical power onto the high-pressure shaft until a speed of the high-pressure shaft attains a target value, then extracting mechanical power from the high-pressure shaft so as to maintain the speed at the target value.
    Type: Grant
    Filed: April 27, 2020
    Date of Patent: December 24, 2024
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Romain Guillaume Cuvillier, Pierre Cabrera
  • Patent number: 11808217
    Abstract: A method for regulating the temperature of the exhaust gases of a turbomachine, the method including regulation of the injection of fuel into a combustion chamber of the turbomachine so that the turbomachine generates a target thrust; regulation of the injection of mechanical power by an electric motor onto a shaft driven in rotation by a turbine, the electric motor being activated when a clearance between a casing and the blades of the turbine exceeds a threshold value.
    Type: Grant
    Filed: March 5, 2020
    Date of Patent: November 7, 2023
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Romain Guillaume Cuvillier, Pierre Cabrera
  • Patent number: 11674760
    Abstract: A method of regulating a temperature associated with a heat exchanger assembly of a turbine engine, the method includes, in a single cycle: measuring the temperature of an air stream at the outlet from a heat exchanger; receiving a setpoint temperature for the air stream at the outlet from the heat exchanger; estimating a theoretical temperature for the air stream at the outlet from the heat exchanger as a function of an estimate of the shutter position of a controlled valve bleeding off a cooling air stream for the heat exchanger; determining a correction current from the difference between the measured temperature and the theoretical temperature; and determining a control current for the shutter from the difference between the measured temperature and the setpoint temperature and the correction current determined during the preceding cycle, the shutter position being determined from the control and correction currents determined during the preceding cycle.
    Type: Grant
    Filed: October 29, 2021
    Date of Patent: June 13, 2023
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Cedrik Djelassi, Pierre Cabrera
  • Publication number: 20220231577
    Abstract: The invention relates to a method for regulating an acceleration of a turbomachine, the turbomachine comprising a combustion chamber, a high-pressure turbine located downstream of the combustion chamber and which drives a high-pressure shaft in rotation, and a low-pressure turbine located downstream of the high-pressure turbine and which drives a low-pressure shaft in rotation, characterized in that the method comprises the following steps: Injecting (100) mechanical power onto the high-pressure shaft until a speed of the high-pressure shaft attains a target value, then Extracting (200) mechanical power from the high-pressure shaft so as to maintain the speed at the target value.
    Type: Application
    Filed: April 27, 2020
    Publication date: July 21, 2022
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Romain Guillaume CUVILLIER, Pierre CABRERA
  • Publication number: 20220162997
    Abstract: A method for regulating the temperature of the exhaust gases of a turbomachine, the method including regulation of the injection of fuel into a combustion chamber of the turbomachine so that the turbomachine generates a target thrust; regulation of the injection of mechanical power by an electric motor onto a shaft driven in rotation by a turbine, the electric motor being activated when a clearance between a casing and the blades of the turbine exceeds a threshold value.
    Type: Application
    Filed: March 5, 2020
    Publication date: May 26, 2022
    Inventors: Romain Guillaume CUVILLIER, Pierre CABRERA
  • Publication number: 20220049911
    Abstract: A method of regulating a temperature associated with a heat exchanger assembly of a turbine engine, the method includes, in a single cycle: measuring the temperature of an air stream at the outlet from a heat exchanger; receiving a setpoint temperature for the air stream at the outlet from the heat exchanger; estimating a theoretical temperature for the air stream at the outlet from the heat exchanger as a function of an estimate of the shutter position of a controlled valve bleeding off a cooling air stream for the heat exchanger; determining a correction current from the difference between the measured temperature and the theoretical temperature; and determining a control current for the shutter from the difference between the measured temperature and the setpoint temperature and the correction current determined during the preceding cycle, the shutter position being determined from the control and correction currents determined during the preceding cycle.
    Type: Application
    Filed: October 29, 2021
    Publication date: February 17, 2022
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Cedrik DJELASSI, Pierre CABRERA
  • Patent number: 11209227
    Abstract: A method of regulating a temperature associated with a heat exchanger assembly of a turbine engine, the method includes, in a single cycle: measuring the temperature of an air stream at the outlet from a heat exchanger; receiving a setpoint temperature for the air stream at the outlet from the heat exchanger; estimating a theoretical temperature for the air stream at the outlet from the heat exchanger as a function of an estimate of the shutter position of a controlled valve bleeding off a cooling air stream for the heat exchanger; determining a correction current from the difference between the measured temperature and the theoretical temperature; and determining a control current for the shutter from the difference between the measured temperature and the setpoint temperature and the correction current determined during the preceding cycle, the shutter position being determined from the control and correction currents determined during the preceding cycle.
    Type: Grant
    Filed: October 16, 2018
    Date of Patent: December 28, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Cedrik Djelassi, Pierre Cabrera
  • Publication number: 20190120576
    Abstract: A method of regulating a temperature (TM) associated with a heat exchanger assembly (10) of a turbine engine (1), the method comprising, in a single cycle: measuring (500) the temperature (TM) of an air stream at the outlet from a heat exchanger (14); receiving a setpoint temperature (TC) for the air stream at the outlet from the heat exchanger (14); estimating (510) a theoretical temperature (TT) for the air stream at the outlet from the heat exchanger (14) as a function of an estimate of the position of a shutter of a controlled valve (15) bleeding off a cooling air stream for the heat exchanger (14); determining a correction current (ICO) from the difference (?T1) between the measured temperature (TM) and the theoretical temperature (TT); and determining (530) a control current (IC) for the shutter from the difference (?T2) between the measured temperature (TM) and the setpoint temperature (TC) and while taking account of the correction current (ICO) determined during the preceding cycle, the position of t
    Type: Application
    Filed: October 16, 2018
    Publication date: April 25, 2019
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventors: Cedrik DJELASSI, Pierre CABRERA
  • Patent number: 7967206
    Abstract: An automatic data collection device is provided for reading barcodes, matrix codes, stacked codes, or other machine-readable symbol. The data collection device generates an aiming beam that serves a dual purpose of target locating and data acquisition, such as data acquisition using imaging methods. The aiming beam defines the field of view of the data collection device for imaging. The illumination pattern provided by the aiming beam for imaging can have its shape, size, and/or intensity adaptively changed depending on conditions.
    Type: Grant
    Filed: August 17, 2006
    Date of Patent: June 28, 2011
    Assignee: Intermec IP Corp.
    Inventors: Christophe Lopez, Vincent Bessettes, Pierre Cabrera, Mustapha Krichi, Philippe Lac, Pierre-Marie Manine, Jean-Michel Puech, Bernard Serres, Serge Thuries, Michael W. Dant, H. Sprague Ackley
  • Patent number: 7417809
    Abstract: An optical assembly includes a first tubular member having a pitched bearing surface proximate one end; a second tubular member having a pitched bearing surface proximate one end; a coupling tubular member fixedly coupled to the second tubular member and rotatably and slideably coupled to the first tubular member; and an optical element received in at least one of the first, the second or the coupling tubular members. At least a portion of the pitched bearing surface of the first tubular member is in engaging contact with at least a portion of the pitched bearing surface of the second tubular member. Rotating the first tubular member with respect to the second tubular member smoothly varies a distance between the first and second tubular members and allows a large, smooth adjustment with little effort. Rotation in a single direction returns the distances to an initial starting point.
    Type: Grant
    Filed: April 19, 2006
    Date of Patent: August 26, 2008
    Assignee: Intermec IP Corp.
    Inventors: Pierre Cabrera, Pierre-Marie Manine
  • Publication number: 20070084926
    Abstract: An automatic data collection device is provided for reading barcodes, matrix codes, stacked codes, or other machine-readable symbol. The data collection device generates an aiming beam that serves a dual purpose of target locating and data acquisition, such as data acquisition using imaging methods. The aiming beam defines the field of view of the data collection device for imaging. The illumination pattern provided by the aiming beam for imaging can have its shape, size, and/or intensity adaptively changed depending on conditions.
    Type: Application
    Filed: August 17, 2006
    Publication date: April 19, 2007
    Applicant: INTERMEC IP CORP.
    Inventors: Christophe Lopez, Vincent Bessettes, Pierre Cabrera, Mustapha Krichi, Philippe Lac, Pierre-Marie Manine, Jean-Michel Puech, Bernard Serres, Serge Thuries, Michael Dant, H. Ackley
  • Publication number: 20060273638
    Abstract: An optical assembly includes a first tubular member having a pitched bearing surface proximate one end; a second tubular member having a pitched bearing surface proximate one end; a coupling tubular member fixedly coupled to the second tubular member and rotatably and slideably coupled to the first tubular member; and an optical element received in at least one of the first, the second or the coupling tubular members. At least a portion of the pitched bearing surface of the first tubular member is in engaging contact with at least a portion of the pitched bearing surface of the second tubular member. Rotating the first tubular member with respect to the second tubular member smoothly varies a distance between the first and second tubular members and allows a large, smooth adjustment with little effort. Rotation in a single direction returns the distances to an initial starting point.
    Type: Application
    Filed: April 19, 2006
    Publication date: December 7, 2006
    Applicant: Intermec IP Corp.
    Inventors: Pierre Cabrera, Pierre-Marie Manine