Patents by Inventor Neus BUSQUETS MORE

Neus BUSQUETS MORE 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: 10443623
    Abstract: An engine bleed air system of an aircraft, comprising a heat exchanger which comprises a rectangular core with a rectangular outlet section, a cylindrical outlet duct and a transition area between the rectangular outlet section of the rectangular core and the cylindrical outlet duct, and at least a downstream system, further comprising a flow deflector located at least in the cylindrical outlet duct, such that the outlet flow characteristics homogeneity are improved and a particular flow deflection and distribution of the outlet flow is achieved, avoiding the damage of the at least one downstream system. The invention also provides a method for homogenizing the temperature of the outlet flow of a heat exchanger outlet in an engine bleed air system of an aircraft.
    Type: Grant
    Filed: March 14, 2017
    Date of Patent: October 15, 2019
    Assignees: AIRBUS OPERATIONS S.L., AIRBUS OPERATIONS GMBH
    Inventors: Antón Méndez Díaz, Javier Fraile Martin, Neus Busquets More, Jan Barkowsky
  • Publication number: 20170268533
    Abstract: An engine bleed air system of an aircraft, comprising a heat exchanger which comprises a rectangular core with a rectangular outlet section, a cylindrical outlet duct and a transition area between the rectangular outlet section of the rectangular core and the cylindrical outlet duct, and at least a downstream system, further comprising a flow deflector located at least in the cylindrical outlet duct, such that the outlet flow characteristics homogeneity are improved and a particular flow deflection and distribution of the outlet flow is achieved, avoiding the damage of the at least one downstream system. The invention also provides a method for homogenizing the temperature of the outlet flow of a heat exchanger outlet in an engine bleed air system of an aircraft.
    Type: Application
    Filed: March 14, 2017
    Publication date: September 21, 2017
    Inventors: Antón MÉNDEZ DÍAZ, Javier FRAILE MARTIN, Neus BUSQUETS MORE, Jan BARKOWSKY