Patents by Inventor Kevin Richard Housen

Kevin Richard Housen 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: 11247784
    Abstract: Gas-flammability sensing systems and methods may be used to determine the flammability of gas mixtures in measurement volumes such as a fuel tank (e.g., an aircraft fuel tank). Gas-flammability sensing systems include a test cell structured to receive a gas sample, a heater in thermal communication with the test cell, and a gas meter configured to measure a physical property of the gas sample within the test cell related to the combustion state of the gas sample. The heater is configured to heat the gas sample to an elevated temperature less than the autoignition temperature of the gas sample. Methods of determining the flammability of a gas sample include collecting the gas sample, heating the gas sample to the elevated temperature, measuring the physical property of the gas sample after heating, and determining the flammability of a gas sample based upon the measured physical property.
    Type: Grant
    Filed: January 10, 2020
    Date of Patent: February 15, 2022
    Assignee: The Boeing Company
    Inventors: Eddie Kwon, Jason Scott Damazo, Philipp Andreas Boettcher, William J. Sweet, Kevin Richard Housen
  • Publication number: 20200148380
    Abstract: Gas-flammability sensing systems and methods may be used to determine the flammability of gas mixtures in measurement volumes such as a fuel tank (e.g., an aircraft fuel tank). Gas-flammability sensing systems include a test cell structured to receive a gas sample, a heater in thermal communication with the test cell, and a gas meter configured to measure a physical property of the gas sample within the test cell related to the combustion state of the gas sample. The heater is configured to heat the gas sample to an elevated temperature less than the autoignition temperature of the gas sample. Methods of determining the flammability of a gas sample include collecting the gas sample, heating the gas sample to the elevated temperature, measuring the physical property of the gas sample after heating, and determining the flammability of a gas sample based upon the measured physical property.
    Type: Application
    Filed: January 10, 2020
    Publication date: May 14, 2020
    Inventors: Eddie Kwon, Jason Scott Damazo, Philipp Andreas Boettcher, William J. Sweet, Kevin Richard Housen
  • Patent number: 10532822
    Abstract: Gas-flammability sensing systems and methods may be used to determine the flammability of gas mixtures in measurement volumes such as a fuel tank (e.g., an aircraft fuel tank). Gas-flammability sensing systems include a test cell structured to receive a gas sample, a heater in thermal communication with the test cell, and a gas meter configured to measure a physical property of the gas sample within the test cell related to the combustion state of the gas sample. The heater is configured to heat the gas sample to an elevated temperature less than the autoignition temperature of the gas sample. Methods of determining the flammability of a gas sample include collecting the gas sample, heating the gas sample to the elevated temperature, measuring the physical property of the gas sample after heating, and determining the flammability of a gas sample based upon the measured physical property.
    Type: Grant
    Filed: January 25, 2017
    Date of Patent: January 14, 2020
    Assignee: The Boeing Company
    Inventors: Eddie Kwon, Jason Scott Damazo, Philipp Andreas Boettcher, William J. Sweet, Kevin Richard Housen
  • Patent number: 10215674
    Abstract: A method and apparatus for measuring a dynamic tensile stress and/or tensile strain response of a material such as an elastic material and/or a ductile material. The apparatus may include a striker bar, a stretcher bar, and a drive assembly configured to propel the striker bar toward the stretcher bar. The apparatus may further include a stationary specimen mount and a movable specimen mount that receive a test sample. The striker bar and the stretcher bar of the apparatus may provide a continuous stress on the test sample and an accurate tensile stress/strain measurement.
    Type: Grant
    Filed: July 15, 2016
    Date of Patent: February 26, 2019
    Assignee: THE BOEING COMPANY
    Inventors: William J. Sweet, Kevin Richard Housen, Arthur C. Day, Jason Scott Damazo
  • Publication number: 20180208324
    Abstract: Gas-flammability sensing systems and methods may be used to determine the flammability of gas mixtures in measurement volumes such as a fuel tank (e.g., an aircraft fuel tank). Gas-flammability sensing systems include a test cell structured to receive a gas sample, a heater in thermal communication with the test cell, and a gas meter configured to measure a physical property of the gas sample within the test cell related to the combustion state of the gas sample. The heater is configured to heat the gas sample to an elevated temperature less than the autoignition temperature of the gas sample. Methods of determining the flammability of a gas sample include collecting the gas sample, heating the gas sample to the elevated temperature, measuring the physical property of the gas sample after heating, and determining the flammability of a gas sample based upon the measured physical property.
    Type: Application
    Filed: January 25, 2017
    Publication date: July 26, 2018
    Inventors: Eddie Kwon, Jason Scott Damazo, Philipp Andreas Boettcher, William J. Sweet, Kevin Richard Housen
  • Publication number: 20180017475
    Abstract: A method and apparatus for measuring a dynamic tensile stress and/or tensile strain response of a material such as an elastic material and/or a ductile material. The apparatus may include a striker bar, a stretcher bar, and a drive assembly configured to propel the striker bar toward the stretcher bar. The apparatus may further include a stationary specimen mount and a movable specimen mount that receive a test sample. The striker bar and the stretcher bar of the apparatus may provide a continuous stress on the test sample and an accurate tensile stress/strain measurement.
    Type: Application
    Filed: July 15, 2016
    Publication date: January 18, 2018
    Inventors: William J. SWEET, Kevin Richard HOUSEN, Arthur C. DAY, Jason Scott DAMAZO
  • Patent number: 9354203
    Abstract: A method and apparatus for testing a test object. A stress wave is generated in a fluid within a cavity in a structure. The stress wave is directed through the fluid within the cavity into the test object.
    Type: Grant
    Filed: February 8, 2013
    Date of Patent: May 31, 2016
    Assignee: THE BOEING COMPANY
    Inventors: William J. Sweet, Kevin Richard Housen, Richard Henry Bossi
  • Patent number: 7945388
    Abstract: An impact test system for collecting hail storm data comprises a vehicle, a video recorder, a container, a plurality of dynamic force sensors, an atmospheric instrument system, a mounting fixture, and a data processing system. The plurality of dynamic force sensors is capable of detecting force generated by an impact of an object. The plurality of markers is capable of being used to determine an orientation of an incoming object. The mounting fixture is capable of holding a test specimen. The data processing system is capable of collecting data from the plurality of dynamic force sensors, the atmospheric instrument system, and the video recorder.
    Type: Grant
    Filed: June 25, 2008
    Date of Patent: May 17, 2011
    Assignee: The Boeing Company
    Inventors: Kevin Richard Housen, Nikhil Kanuru Rao, William John Koch, IV
  • Publication number: 20090326822
    Abstract: An impact test system for collecting hail storm data comprises a vehicle, a video recorder, a container, a plurality of dynamic force sensors, an atmospheric instrument system, a mounting fixture, and a data processing system. The plurality of dynamic force sensors is capable of detecting force generated by an impact of an object. The plurality of markers is capable of being used to determine an orientation of an incoming object. The mounting fixture is capable of holding a test specimen. The data processing system is capable of collecting data from the plurality of dynamic force sensors, the atmospheric instrument system, and the video recorder.
    Type: Application
    Filed: June 25, 2008
    Publication date: December 31, 2009
    Inventors: Kevin Richard Housen, Nikhil Kanuru Rao, William John Koch, IV