Patents by Inventor Scott William WEBER

Scott William WEBER 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).

  • Oxygen Pressure Relief and Ventilation System and Method
    Publication number: 20230150675
    Abstract: An oxygen pressure relief and ventilation system includes a flow fuse fluidly coupled downstream of a pressure regulator. The pressure regulator is operatively coupled to an oxygen tank, and the oxygen tank is located in an unpressurized compartment of an aircraft. A pressure relief valve is fluidly coupled downstream of the flow fuse. A ventilation pathway fluidly couples the unpressurized compartment with a pressurized compartment. The flow fuse and the pressure relief valve are configured to cooperatively mitigate downstream flow of pressurized oxygen if the pressure regulator fails. The ventilation pathway is configured to allow air from the pressurized compartment to pass through to the unpressurized compartment for diluting a concentrated oxygen in the unpressurized compartment.
    Type: Application
    Filed: November 18, 2022
    Publication date: May 18, 2023
    Inventors: Scott William Weber, Sam Khounsombath, Trey Marcus Siemens, Richard Lee Gaines
  • Compressor temperature control system and method
    Patent number: 11370550
    Abstract: A compressor temperature control system and method for an aircraft air cycle machine is presented. The system prevents overheating of the compressor using a low limit valve positioned between a turbine outlet and a bleed air source. The low limit valve directs the air to an air cycle machine, or bypasses the machine, in regards at least in part to the air temperature measured in the cabin supply duct.
    Type: Grant
    Filed: October 8, 2020
    Date of Patent: June 28, 2022
    Inventors: Scott William Weber, Clinton Lee Thompson
  • COMPRESSOR TEMPERATURE CONTROL SYSTEM AND METHOD
    Publication number: 20210024219
    Abstract: A compressor temperature control system and method for an aircraft air cycle machine is presented. The system prevents overheating of the compressor using a low limit valve positioned between a turbine outlet and a bleed air source. The low limit valve directs the air to an air cycle machine, or bypasses the machine, in regards at least in part to the air temperature measured in the cabin supply duct.
    Type: Application
    Filed: October 8, 2020
    Publication date: January 28, 2021
    Inventors: Scott William WEBER, Clinton Lee THOMPSON
  • Compressor temperature control system and method
    Patent number: 10829226
    Abstract: A compressor temperature control system and method for an aircraft air cycle machine is presented. The system prevents overheating of the compressor using a low limit valve positioned between a turbine outlet and a bleed air source. The low limit valve directs the air to an air cycle machine, or bypasses the machine, in regards at least in part to the air temperature measured in the cabin supply duct.
    Type: Grant
    Filed: May 15, 2017
    Date of Patent: November 10, 2020
    Assignee: Textron Innovations, Inc.
    Inventors: Scott William Weber, Clinton Lee Thompson
  • COMPRESSOR TEMPERATURE CONTROL SYSTEM AND METHOD
    Publication number: 20170341757
    Abstract: A compressor temperature control system and method for an aircraft air cycle machine is presented. The system prevents overheating of the compressor using a low limit valve positioned between a turbine outlet and a bleed air source. The low limit valve directs the air to an air cycle machine, or bypasses the machine, in regards at least in part to the air temperature measured in the cabin supply duct.
    Type: Application
    Filed: May 15, 2017
    Publication date: November 30, 2017
    Inventors: Scott William WEBER, Clinton Lee THOMPSON