Patents by Inventor Jean-Luc MANCHO

Jean-Luc MANCHO 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: 11821328
    Abstract: The invention relates to a regulator, configured to receive a hot air flow via an air inlet (12), to treat this hot air and to transmit the treated hot air to an air outlet (14) configured to supply a pneumatic actuator (16), comprising at least one temperature-sensitive electrical and/or mechanical element (36, 37), and a regulator body (100). The regulator is characterized in that the regulator body is composed of a heat-conducting hollow enclosure (28) at least partially surrounding a duct (22) for transporting the hot air flow, said cavity being at least partially filled with a metal mesh produced by additive manufacturing that allows the cooling air to circulate, and in that the temperature-sensitive electrical and/or mechanical element (36, 37) is arranged in, or in contact with, the regulator so as to be cooled by the cooling air by thermal conduction.
    Type: Grant
    Filed: May 20, 2020
    Date of Patent: November 21, 2023
    Assignee: LIEBHERR-AEROSPACE TOULOUSE SAS
    Inventors: Damien Maury, David Lossouarn, Jean-Luc Mancho, Mickael Bregoli, Romain Angelique
  • Publication number: 20220261018
    Abstract: The invention relates to a regulator, configured to receive a stream of hot air carrying pneumatic power via an air inlet (12), to treat this hot air and to send the treated hot air to an air outlet (14) configured 5 to supply a pneumatic actuator (16), comprising a reference pressure source and an air expansion device comprising a diaphragm (22), the diaphragm (22) being configured to control the flow rate of the hot air stream by comparing the pressure of said hot air stream with the reference pressure of the reference pressure source. The regulator is characterized in that it 10 comprises an air intake (24) configured to receive a cold source, and a pipe (25) for guiding the cold source to the diaphragm (22), so that the cold source forms the reference pressure source and a source for cooling the diaphragm (22).
    Type: Application
    Filed: June 12, 2020
    Publication date: August 18, 2022
    Inventors: Jean-Luc MANCHO, David LOSSOUARN, Antoine PEYRE
  • Publication number: 20220220863
    Abstract: The invention relates to a regulator, configured to receive a hot air flow via an air inlet (12), to treat this hot air and to transmit the treated hot air to an air outlet (14) configured to supply a pneumatic actuator (16), comprising at least one temperature-sensitive electrical and/or mechanical element (36, 37), and a regulator body (100). The regulator is characterized in that the regulator body is composed of a heat-conducting hollow enclosure (28) at least partially surrounding a duct (22) for transporting the hot air flow, said cavity being at least partially filled with a metal mesh produced by additive manufacturing that allows the cooling air to circulate, and in that the temperature-sensitive electrical and/or mechanical element (36, 37) is arranged in, or in contact with, the regulator so as to be cooled by the cooling air by thermal conduction.
    Type: Application
    Filed: May 20, 2020
    Publication date: July 14, 2022
    Inventors: Damien MAURY, David LOSSOUARN, Jean-Luc MANCHO, Mickael BREGOLI, Romain ANGELIQUE
  • Patent number: 11242932
    Abstract: The invention relates to an air bleed system comprising an air bleed port provided on an engine of an aircraft, an air supply pipe, a pressure sensor, a pressure relief valve mounted in said air supply pipe, characterized in that said pressure relief valve comprises: a valve body (11); a closure member (121) pivotally mounted in said air circulation duct; and an air discharge channel (13) passing through said valve body (11); at least one air discharge opening (15) formed on said upstream face of said closure member (121) and at least one air evacuation opening (19) which opens out to the outside of the air circulation duct.
    Type: Grant
    Filed: May 2, 2019
    Date of Patent: February 8, 2022
    Assignee: LIEBHERR-AEROSPACE TOULOUSE SAS
    Inventors: Jean-Luc Mancho, Damien Maury, Frédéric Bristiel
  • Publication number: 20210108733
    Abstract: The invention relates to an air bleed system comprising an air bleed port provided on an engine of an aircraft, an air supply pipe, a pressure sensor, a pressure relief valve mounted in said air supply pipe, characterized in that said pressure relief valve comprises: a valve body (11); a closure member (121) pivotally mounted in said air circulation duct; and an air discharge channel (13) passing through said valve body (11); at least one air discharge opening (15) formed on said upstream face of said closure member (121) and at least one air evacuation opening (19) which opens out to the outside of the air circulation duct.
    Type: Application
    Filed: May 2, 2019
    Publication date: April 15, 2021
    Inventors: Jean-Luc MANCHO, Damien MAURY, Frédéric BRISTIEL