Patents by Inventor Antoine Marie Georges Caratge

Antoine Marie Georges Caratge 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: 11035372
    Abstract: Controller for controlling a bleed valve including a first body with an internal cavity connected to an air inlet port and an air outlet port, a second body including a chamber, a mobile member in the cavity and in the chamber, connecting the two bodies. The member is mobile between a position whereby the ports fluidly communicate and a position whereby the ports are isolated, the member further including two pistons housed in the chamber and defining in this chamber at least two spaces. The controller also includes a fluid supply for at least one of the spaces for the purpose of moving the pistons in the chamber.
    Type: Grant
    Filed: April 3, 2019
    Date of Patent: June 15, 2021
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventor: Antoine Marie George Caratge
  • Patent number: 10865800
    Abstract: Controller, control actuator and bleed valve including a first chamber for the circulation of a discharge air stream when the valve is open and preventing it when the valve is closed, an inner housing, in which a mobile blocking unit is moved between a position for opening and a position for closing the valve, this unit delimiting, in the inner housing, two chambers, the second chamber including a mechanism for returning the blocking unit to the open position, and the third chamber, being used to be in fluidic connection with the control actuator in order to actuate the blocking unit against the return mechanism, the three chambers being isolated in a sealed manner from one another by way of the blocking unit. The device includes a regulation valve.
    Type: Grant
    Filed: April 3, 2019
    Date of Patent: December 15, 2020
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventor: Antoine Marie Georges Caratge
  • Publication number: 20190309762
    Abstract: Controller, control actuator and bleed valve including a first chamber for the circulation of a discharge air stream when the valve is open and preventing it when the valve is closed, an inner housing, in which a mobile blocking unit is moved between a position for opening and a position for closing the valve, this unit delimiting, in the inner housing, two chambers, the second chamber including a mechanism for returning the blocking unit to the open position, and the third chamber, being used to be in fluidic connection with the control actuator in order to actuate the blocking unit against the return mechanism, the three chambers being isolated in a sealed manner from one another by way of the blocking unit. The device includes a regulation valve.
    Type: Application
    Filed: April 3, 2019
    Publication date: October 10, 2019
    Inventor: Antoine Marie Georges CARATGE
  • Publication number: 20190309647
    Abstract: Controller for controlling a bleed valve including a first body with an internal cavity connected to an air inlet port and an air outlet port, a second body including a chamber, a mobile member in the cavity and in the chamber, connecting the two bodies. The member is mobile between a position whereby the ports fluidly communicate and a position whereby the ports are isolated, the member further including two pistons housed in the chamber and defining in this chamber at least two spaces. The controller also includes a fluid supply for at least one of the spaces for the purpose of moving the pistons in the chamber.
    Type: Application
    Filed: April 3, 2019
    Publication date: October 10, 2019
    Inventor: Antoine Marie George CARATGE
  • Patent number: 9951694
    Abstract: An emergency start system for a turbine engine of an aircraft including at least one solid propellant gas generator, an electrically controlled ignition device, a computer connected to the ignition device, and at least one starter motor comprising a turbine for driving a shaft which is for coupling to a shaft of the turbine engine The outlet of the gases from the generator are connected to the inlet of the turbine of the starter motor.
    Type: Grant
    Filed: September 12, 2014
    Date of Patent: April 24, 2018
    Assignees: SAFRAN AIRCRAFT ENGINES, SAFRAN HELICOPTER ENGINES
    Inventors: Romain Thiriet, Patrick Marconi, Camel Serghine, Antoine Marie Georges Caratge, Francois Danguy, Laurent Fabbri, Pierre Yvart, Laurent Soulie, Philippe Barrat
  • Publication number: 20160230672
    Abstract: The invention relates to an emergency start system (20) for a turbine engine of an aircraft, characterised in that it comprises at least one solid-propellant gas generator (22), an electrically controlled ignition device (24), a computer (28) connected to the ignition device, and at least one starter motor (18) comprising a turbine (38) for driving a shaft (34) intended for being coupled to a shaft (54) of the turbine engine, the outlet of the gases from the generator being connected to the inlet (44) of the turbine of the starter motor.
    Type: Application
    Filed: September 12, 2014
    Publication date: August 11, 2016
    Inventors: Romain Thiriet, Patrick Marconi, Camel Serghine, Antoine Marie Georges Caratge, Francois Danguy, Laurent Fabbri, Pierre Yvart, Laurent Soulie, Philippe Barrat