Patents by Inventor Kate Boudreau

Kate Boudreau 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: 11442040
    Abstract: A shear wave inspection tool has a housing with a rotatable top removably fixable over a fastener hole in a structure. An aperture is positioned through the rotatable top and operable to couple an ultrasonic transducer such that when rotatable top is rotated, the ultrasonic transducer transmits a shear wave into the structure around the fastener hole inspecting the fastener hole for an anomaly. A shear wave inspection system includes the inspection tool, an ultrasonic transducer, an ultrasonic data instrument operable to acquire data from the ultrasonic transducer, the nature of the received data indicates the presence of an anomaly in the fastener hole. A method for detecting anomalies in a fastener hole includes removably fixing the inspection tool over a fastener hole and rotating the rotatable top such that the ultrasonic transducer transmits a shear wave in a controlled sweep around the fastener hole.
    Type: Grant
    Filed: February 7, 2020
    Date of Patent: September 13, 2022
    Assignee: The Boeing Company
    Inventors: Kareem Shehab, Kate Boudreau Summers, Paul Stanley Rutherford
  • Publication number: 20210247362
    Abstract: A shear wave inspection tool has a housing with a rotatable top removably fixable over a fastener hole in a structure. An aperture is positioned through the rotatable top and operable to couple an ultrasonic transducer such that when rotatable top is rotated, the ultrasonic transducer transmits a shear wave into the structure around the fastener hole inspecting the fastener hole for an anomaly. A shear wave inspection system includes the inspection tool, an ultrasonic transducer, an ultrasonic data instrument operable to acquire data from the ultrasonic transducer, the nature of the received data indicates the presence of an anomaly in the fastener hole. A method for detecting anomalies in a fastener hole includes removably fixing the inspection tool over a fastener hole and rotating the rotatable top such that the ultrasonic transducer transmits a shear wave in a controlled sweep around the fastener hole.
    Type: Application
    Filed: February 7, 2020
    Publication date: August 12, 2021
    Applicant: The Boeing Company
    Inventors: Kareem Shehab, Kate Boudreau Summers, Paul Stanley Rutherford
  • Patent number: 9778230
    Abstract: An ultrasound scanning assembly is configured to inspect a structure, such as a composite winglet of an aircraft. The ultrasound scanning assembly may include an outer ultrasound probe configured to be positioned on an outer surface of the structure. The outer ultrasound probe may include a phased array transducer having a plurality of transducer elements. An inner ultrasound probe may be configured to be positioned within the structure opposite from the outer surface. The inner ultrasound probe may include a single element transducer configured to receive ultrasound signals transmitted by the phased array transducer.
    Type: Grant
    Filed: April 30, 2015
    Date of Patent: October 3, 2017
    Assignee: The Boeing Company
    Inventors: Kate Boudreau, Justin D. Serrill, Fred D. Young
  • Publication number: 20170227504
    Abstract: In accordance with one or more aspects of the present disclosure, an apparatus for inspecting a part having a non-linear cross section includes a stationary sensor element including at least one phased array sensing unit, each of the at least one phased array sensing unit having a shape that is geometrically complimentary to the non-linear cross section of the part, and a support for the part having the non-linear cross section, the support comprising a drive assembly configured to move the part relative to the stationary sensor element, through an inspection beam emitted from the at least one phased array sensing unit.
    Type: Application
    Filed: February 4, 2016
    Publication date: August 10, 2017
    Inventors: Kate BOUDREAU, Fred D. YOUNG, Joseph TAYLOR
  • Publication number: 20160320348
    Abstract: An ultrasound scanning assembly is configured to inspect a structure, such as a composite winglet of an aircraft. The ultrasound scanning assembly may include an outer ultrasound probe configured to be positioned on an outer surface of the structure. The outer ultrasound probe may include a phased array transducer having a plurality of transducer elements. An inner ultrasound probe may be configured to be positioned within the structure opposite from the outer surface. The inner ultrasound probe may include a single element transducer configured to receive ultrasound signals transmitted by the phased array transducer.
    Type: Application
    Filed: April 30, 2015
    Publication date: November 3, 2016
    Applicant: THE BOEING COMPANY
    Inventors: Kate Boudreau, Justin D. Serrill, Fred D. Young