Patents by Inventor David A. Rathke

David A. Rathke 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: 10627304
    Abstract: A system includes a signal generator that is configured to generate a first electrical signal. The system also includes a light source configured to generate a light beam based on the first electrical signal. The light source is also configured to direct the light beam towards a structural member of an aircraft. The system also includes a photoelectric sensor configured to receive a reflected light beam and convert the reflected light beam to a second electrical signal. The reflected light beam corresponds to a portion of the light beam that is reflected from one or more optical reflectors coupled to the structural member. The system also includes circuitry configured to estimate a location of a center-of-gravity of the aircraft based on a timing difference between the first electrical signal and the second electrical signal.
    Type: Grant
    Filed: January 31, 2018
    Date of Patent: April 21, 2020
    Assignee: THE BOEING COMPANY
    Inventors: Sina S. Golshany, Martin M. Withington, Lowell B. Campbell, David A. Rathke, Tarek H. Elghoroury, Matthew W. Orr, Gnanulan Canagaratna
  • Publication number: 20190234825
    Abstract: A system includes a signal generator that is configured to generate a first electrical signal. The system also includes a light source configured to generate a light beam based on the first electrical signal. The light source is also configured to direct the light beam towards a structural member of an aircraft. The system also includes a photoelectric sensor configured to receive a reflected light beam and convert the reflected light beam to a second electrical signal. The reflected light beam corresponds to a portion of the light beam that is reflected from one or more optical reflectors coupled to the structural member. The system also includes circuitry configured to estimate a location of a center-of-gravity of the aircraft based on a timing difference between the first electrical signal and the second electrical signal.
    Type: Application
    Filed: January 31, 2018
    Publication date: August 1, 2019
    Inventors: Sina S. Golshany, Martin M. Withington, Lowell B. Campbell, David A. Rathke, Tarek H. Elghoroury, Matthew W. Orr, Gnanulan Canagaratna
  • Patent number: 10100944
    Abstract: Methods and systems for a butterfly valve including a shape memory alloy (SMA) tube trained for rotation are presently disclosed. The SMA tube has a ground end coupled to a housing and rotating end coupled to a plate. The SMA tube is configured to rotate in a first direction in response to a first temperature change of the SMA tube. When rotating in the first direction, the rotating end of the SMA tube rotates and deflects the plate to rotate in a direction that permits a medium to flow through the valve. The SMA tube is also configured to rotate in a second direction in response to a second temperature change of the SMA tube. When rotating in the second direction, the rotating end of the SMA tube rotates and deflects the plate to rotate in a direction that does not permits a medium to flow through the valve.
    Type: Grant
    Filed: August 3, 2015
    Date of Patent: October 16, 2018
    Assignee: The Boeing Company
    Inventors: Frederick T. Calkins, Pruthvish V. Patel, David A. Rathke
  • Publication number: 20170037982
    Abstract: Methods and systems for a butterfly valve including a shape memory alloy (SMA) tube trained for rotation are presently disclosed. The SMA tube has a ground end coupled to a housing and rotating end coupled to a plate. The SMA tube is configured to rotate in a first direction in response to a first temperature change of the SMA tube. When rotating in the first direction, the rotating end of the SMA tube rotates and deflects the plate to rotate in a direction that permits a medium to flow through the valve. The SMA tube is also configured to rotate in a second direction in response to a second temperature change of the SMA tube. When rotating in the second direction, the rotating end of the SMA tube rotates and deflects the plate to rotate in a direction that does not permits a medium to flow through the valve.
    Type: Application
    Filed: August 3, 2015
    Publication date: February 9, 2017
    Inventors: Frederick T. Calkins, Pruthvish V. Patel, David A. Rathke