Patents by Inventor Kawthar Kasim

Kawthar Kasim 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: 11781814
    Abstract: A tapered groove width heat pipe is disclosed, including a tube having an internal surface, a first end, a second end, and a central axis. A plurality of groove walls on the internal surface define a plurality of trapezoidal grooves. Each groove wall has a proximal width closest to the central axis and a distal width furthest from the central axis, the proximal width of a portion of each groove wall tapering gradually between the first end and the second end.
    Type: Grant
    Filed: March 16, 2020
    Date of Patent: October 10, 2023
    Assignee: The Boeing Company
    Inventor: Kawthar Kasim
  • Patent number: 11174036
    Abstract: An example method for installing optical sensors for a fuel level measurement system includes mounting a plurality of fittings through a wall of a fuel tank, positioning a plurality of optical sensors within the plurality of fittings and a respective optical sensor includes a first pressure sensing end inserted through the fitting and internally into the fuel tank and a second end extending externally from the fuel tank, and mounting an optical fiber bundle external to the fuel tank. The optical fiber bundle has an optical fiber connected to each of the plurality of optical sensors for guiding light to each of the plurality of optical sensors.
    Type: Grant
    Filed: August 27, 2019
    Date of Patent: November 16, 2021
    Assignee: The Boeing Company
    Inventors: Michael Carralero, Paul Truzzi, Kawthar Kasim
  • Publication number: 20210285729
    Abstract: A tapered groove width heat pipe is disclosed, including a tube having an internal surface, a first end, a second end, and a central axis. A plurality of groove walls on the internal surface define a plurality of trapezoidal grooves. Each groove wall has a proximal width closest to the central axis and a distal width furthest from the central axis, the proximal width of a portion of each groove wall tapering gradually between the first end and the second end.
    Type: Application
    Filed: March 16, 2020
    Publication date: September 16, 2021
    Applicant: The Boeing Company
    Inventor: Kawthar Kasim
  • Patent number: 10648846
    Abstract: An example fuel quantity indicating system includes a fuel tank, optical sensors mounted inside the fuel tank that each include a sensor chip and a diaphragm that deflects when ambient pressure differs from a reference pressure of the sensor chip, an optical fiber bundle that has an optical fiber connected to each of the optical sensors for guiding light to each of the optical sensors, and a processor connected to the optical fiber bundle for receiving outputs of the optical sensors indicative of respective pressures, and for determining a fuel level measurement of the fuel tank based on the outputs of the optical sensors.
    Type: Grant
    Filed: October 10, 2018
    Date of Patent: May 12, 2020
    Assignee: The Boeing Company
    Inventors: Michael A. Carralero, Kawthar Kasim, Paul Scott Truzzi
  • Publication number: 20190382125
    Abstract: An example system includes a fuel tank, fittings mounted through a wall of the fuel tank, and optical sensors positioned within the fittings. A respective optical sensor includes a first pressure sensing end inserted through a fitting and internally into the fuel tank and a second end extending externally from the fuel tank. The system also includes an optical fiber bundle mounted external to the fuel tank, and having an optical fiber connected to each of the plurality of optical sensors for guiding light to each of the plurality of optical sensors.
    Type: Application
    Filed: August 27, 2019
    Publication date: December 19, 2019
    Inventors: Michael Carralero, Paul Truzzi, Kawthar Kasim
  • Patent number: 10435170
    Abstract: An example system includes a fuel tank, fittings mounted through a wall of the fuel tank, and optical sensors positioned within the fittings. A respective optical sensor includes a first pressure sensing end inserted through a fitting and internally into the fuel tank and a second end extending externally from the fuel tank. The system also includes an optical fiber bundle mounted external to the fuel tank, and having an optical fiber connected to each of the plurality of optical sensors for guiding light to each of the plurality of optical sensors.
    Type: Grant
    Filed: December 8, 2016
    Date of Patent: October 8, 2019
    Assignee: The Boeing Company
    Inventors: Michael Carralero, Paul Truzzi, Kawthar Kasim
  • Publication number: 20190049280
    Abstract: An example fuel quantity indicating system includes a fuel tank, optical sensors mounted inside the fuel tank that each include a sensor chip and a diaphragm that deflects when ambient pressure differs from a reference pressure of the sensor chip, an optical fiber bundle that has an optical fiber connected to each of the optical sensors for guiding light to each of the optical sensors, and a processor connected to the optical fiber bundle for receiving outputs of the optical sensors indicative of respective pressures, and for determining a fuel level measurement of the fuel tank based on the outputs of the optical sensors.
    Type: Application
    Filed: October 10, 2018
    Publication date: February 14, 2019
    Inventors: Michael A. Carralero, Kawthar Kasim, Paul Scott Truzzi
  • Patent number: 10126158
    Abstract: An example fuel quantity indicating system includes a fuel tank, optical sensors mounted inside the fuel tank that each include a sensor chip and a diaphragm that deflects when ambient pressure differs from a reference pressure of the sensor chip, an optical fiber bundle that has an optical fiber connected to each of the optical sensors for guiding light to each of the optical sensors, and a processor connected to the optical fiber bundle for receiving outputs of the optical sensors indicative of respective pressures, and for determining a fuel level measurement of the fuel tank based on the outputs of the optical sensors.
    Type: Grant
    Filed: August 22, 2016
    Date of Patent: November 13, 2018
    Assignee: The Boeing Company
    Inventors: Michael A. Carralero, Kawthar Kasim, Paul Scott Truzzi
  • Publication number: 20180164140
    Abstract: An example system includes a fuel tank, fittings mounted through a wall of the fuel tank, and optical sensors positioned within the fittings. A respective optical sensor includes a first pressure sensing end inserted through a fitting and internally into the fuel tank and a second end extending externally from the fuel tank. The system also includes an optical fiber bundle mounted external to the fuel tank, and having an optical fiber connected to each of the plurality of optical sensors for guiding light to each of the plurality of optical sensors.
    Type: Application
    Filed: December 8, 2016
    Publication date: June 14, 2018
    Inventors: Michael Carralero, Paul Truzzi, Kawthar Kasim
  • Publication number: 20180052029
    Abstract: An example fuel quantity indicating system includes a fuel tank, optical sensors mounted inside the fuel tank that each include a sensor chip and a diaphragm that deflects when ambient pressure differs from a reference pressure of the sensor chip, an optical fiber bundle that has an optical fiber connected to each of the optical sensors for guiding light to each of the optical sensors, and a processor connected to the optical fiber bundle for receiving outputs of the optical sensors indicative of respective pressures, and for determining a fuel level measurement of the fuel tank based on the outputs of the optical sensors.
    Type: Application
    Filed: August 22, 2016
    Publication date: February 22, 2018
    Inventors: Michael A. Carralero, Kawthar Kasim, Paul Scott Truzzi