Patents by Inventor Marcos Ubilla

Marcos Ubilla 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).

  • Systems and methods of sensing temperature of air in a passenger area of a fuselage
    Patent number: 11932406
    Abstract: An example temperature sensing device includes an air distribution inlet through which primary air is blown into via an environmental control system, a cabin air inlet through which secondary air enters from a passenger area of a fuselage and the cabin air inlet is coupled to the air distribution inlet through a duct and the secondary air is passively drawn into the cabin air inlet and to the duct due to a pressure difference present in the duct, and a temperature sensor coupled to the duct and positioned downstream of the cabin air inlet along an airflow path of the secondary air so as to be exposed to the secondary air drawn in through the cabin air inlet and flowing through the duct.
    Type: Grant
    Filed: November 1, 2022
    Date of Patent: March 19, 2024
    Assignee: The Boeing Company
    Inventors: Matthew P. Schonhoff, Jeffrey G. Hatchel, Marcos Ubilla, Spencer L. Savage, Scott P. Ellsworth, Blake J. Burton, Jackson Poscablo
  • Systems and Methods of Sensing Temperature of Air in a Passenger Area of a Fuselage
    Publication number: 20230053172
    Abstract: An example temperature sensing device includes an air distribution inlet through which primary air is blown into via an environmental control system, a cabin air inlet through which secondary air enters from a passenger area of a fuselage and the cabin air inlet is coupled to the air distribution inlet through a duct and the secondary air is passively drawn into the cabin air inlet and to the duct due to a pressure difference present in the duct, and a temperature sensor coupled to the duct and positioned downstream of the cabin air inlet along an airflow path of the secondary air so as to be exposed to the secondary air drawn in through the cabin air inlet and flowing through the duct.
    Type: Application
    Filed: November 1, 2022
    Publication date: February 16, 2023
    Inventors: Matthew P. Schonhoff, Jeffrey G. Hatchel, Marcos Ubilla, Spencer L. Savage, Scott P. Ellsworth, Blake J. Burton, Jackson Poscablo
  • Systems and methods of sensing temperature of air in a passenger area of a fuselage
    Patent number: 11518524
    Abstract: An example temperature sensing device includes an air distribution inlet through which primary air is blown into via an environmental control system, a cabin air inlet through which secondary air enters from a passenger area of a fuselage and the cabin air inlet is coupled to the air distribution inlet through a duct and the secondary air is passively drawn into the cabin air inlet and to the duct due to a pressure difference present in the duct, and a temperature sensor coupled to the duct and positioned downstream of the cabin air inlet along an airflow path of the secondary air so as to be exposed to the secondary air drawn in through the cabin air inlet and flowing through the duct.
    Type: Grant
    Filed: June 10, 2020
    Date of Patent: December 6, 2022
    Assignee: The Boeing Company
    Inventors: Matthew P. Schonhoff, Jeffrey G. Hatchel, Marcos Ubilla, Spencer L. Savage, Scott P. Ellsworth, Blake J. Burton, Jackson Poscablo
  • Systems and Methods of Sensing Temperature of Air in a Passenger Area of a Fuselage
    Publication number: 20210387736
    Abstract: An example temperature sensing device includes an air distribution inlet through which primary air is blown into via an environmental control system, a cabin air inlet through which secondary air enters from a passenger area of a fuselage and the cabin air inlet is coupled to the air distribution inlet through a duct and the secondary air is passively drawn into the cabin air inlet and to the duct due to a pressure difference present in the duct, and a temperature sensor coupled to the duct and positioned downstream of the cabin air inlet along an airflow path of the secondary air so as to be exposed to the secondary air drawn in through the cabin air inlet and flowing through the duct.
    Type: Application
    Filed: June 10, 2020
    Publication date: December 16, 2021
    Inventors: Matthew P. Schonhoff, Jeffrey G. Hatchel, Marcos Ubilla, Spencer L. Savage, Scott P. Ellsworth, Blake J. Burton, Jackson Poscablo