Patents by Inventor William O. Walters

William O. Walters 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: 7698769
    Abstract: An apparatus for the rapid loading, launching and retrieval of foam pellets for tube cleaning. The apparatus uses a block configuration to allow gravity feed and rapid firing of pellets into tubes. The apparatus includes a hopper feeder attachment, which is self-adjusting during pellet jams.
    Type: Grant
    Filed: March 14, 2006
    Date of Patent: April 20, 2010
    Assignee: The Boeing Company
    Inventor: William O Walters
  • Patent number: 7666263
    Abstract: An apparatus for the rapid loading, launching and retrieval of foam pellets for tube cleaning. The apparatus uses a block configuration to allow gravity feed and rapid firing of pellets into tubes. The apparatus includes a hopper feeder attachment, which is self-adjusting during pellet jams.
    Type: Grant
    Filed: August 30, 2005
    Date of Patent: February 23, 2010
    Assignee: The Boeing Company
    Inventor: William O. Walters
  • Patent number: 7644618
    Abstract: A method of inspecting a radius area of composite parts with an ultrasonic inspection system, the system includes at least one ultrasonic probe, an upper sliding surface, a lower sliding surface, an adjustable guide rail, and an adjustable encoder wheel rotatably coupled to a rotary encoder, is provided. The method includes generating a high frequency sound wave using the probe including a radius of curvature extending from a center point, the sound wave travels partially through the part, adjusting the guide rail to align the center point of the probe with a center axis of a part corner portion, sliding the part through the inspection system to inspect the corner portion using the sound wave by rotating the wheel and rotary encoder such that the arcuate distance of the part is recorded, adjusting the wheel to avoid any apertures defined within the part, and processing the sound wave information.
    Type: Grant
    Filed: October 26, 2007
    Date of Patent: January 12, 2010
    Assignee: The Boeing Company
    Inventors: Barry A. Fetzer, William O. Walters, Hien T. Bui
  • Publication number: 20090107244
    Abstract: A method of inspecting a radius area of composite parts with an ultrasonic inspection system, the system includes at least one ultrasonic probe, an upper sliding surface, a lower sliding surface, an adjustable guide rail, and an adjustable encoder wheel rotatably coupled to a rotary encoder, is provided. The method includes generating a high frequency sound wave using the probe including a radius of curvature extending from a center point, the sound wave travels partially through the part, adjusting the guide rail to align the center point of the probe with a center axis of a part corner portion, sliding the part through the inspection system to inspect the corner portion using the sound wave by rotating the wheel and rotary encoder such that the arcuate distance of the part is recorded, adjusting the wheel to avoid any apertures defined within the part, and processing the sound wave information.
    Type: Application
    Filed: October 26, 2007
    Publication date: April 30, 2009
    Inventors: Barry A. Fetzer, William O. Walters, Hien T. Bui
  • Patent number: 4339712
    Abstract: A shunt is disposed in the current path of a device, e.g. a magnetic particle machine and an input voltage from the shunt is amplified and coupled to: a peak-hold circuit for developing a digital amperage readout; and, a pulse comparator circuit operative with clock, clock gate and counter circuits for developing pulse length readout.
    Type: Grant
    Filed: May 1, 1980
    Date of Patent: July 13, 1982
    Assignee: The Boeing Company
    Inventor: William O. Walters
  • Patent number: 4331026
    Abstract: A material hardness testing apparatus is provided, for use in quality control of production materials and parts, in which a pneumatically actuated indenter probe, incorporating an LVDT displacement transducer, is coupled by an analog-to-digital converter to a microprocessor-based computer that controls the cyclic actuation of the indentor probe, and processes indenter measurement data received from the LVDT transducer. The pneumatically actuated indenter probe includes pneumatic control means for providing independently adjustable control over the rates of probe impact and retraction in order to achieve consistent hardness measurements from cycle to cycle, together with relatively rapid displacement cycling of the indenter probe. The microprocessor-based computer incorporates a recalibration processor which automatically causes the testing apparatus to branch into a recalibration routine after a predetermined period of operation.
    Type: Grant
    Filed: July 14, 1980
    Date of Patent: May 25, 1982
    Assignee: The Boeing Company
    Inventors: Bruce S. Howard, William O. Walters