Patents by Inventor David G. Owens

David G. Owens 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).

  • Publication number: 20240123460
    Abstract: Disclosed are methods, systems and computer program products for producing and applying a spray foam producing mixture onto a surface, and imaging a spray cone, or the applied surface, using an infrared or an optical imaging device to capture an image, and then determining, based on the captured image, if a defect that requires correction exists in the spray cone or in the applied surface; and optionally, in response to determining that a defect requiring correction exists, modifying a process parameter in producing or applying spray foam.
    Type: Application
    Filed: October 6, 2020
    Publication date: April 18, 2024
    Inventors: Devin W. Ulam, David D. Steppan, Scott M. Cloherty, Steven G. Owens, Eric C. Giles
  • Patent number: 6915687
    Abstract: A static pressure sensing probe has an aerodynamically shaped cross section, and extends laterally from an aircraft surface sufficiently so that an outer end of the probe is a short distance outside the boundary layer on the aircraft surface on which the probe is mounted. The probe has surface corrugations or ridges along the probe, and the ridges include an upstream ridge adjacent the leading edge, and a downstream ridge spaced rearwardly from the upstream ridge. The ridges cause pressure disturbances along the probe surfaces. Static pressure sensing ports are positioned on the surfaces of the probe relative to the ridges in regions of pressure disturbances caused by the ridges. The probes can be mounted on opposite sides of the aircraft and pneumatically or electrically connected to average the pressures from selected sets of ports.
    Type: Grant
    Filed: July 1, 2003
    Date of Patent: July 12, 2005
    Assignee: Rosemount Aerospace Inc.
    Inventors: Roger D. Foster, Paul F. Heine, Patrick J. Moynihan, David G. Owens
  • Patent number: 6320511
    Abstract: An ice detector for an aircraft comprises a strut and probe assembly, and it is positioned on the aircraft so that the pressure field around the ice detector causes a lower temperature region on the probe assembly compared to the aircraft. Ice will therefore form on the probe assembly before it forms on the aircraft to provide an early warning of icing conditions near freezing temperatures.
    Type: Grant
    Filed: November 28, 2000
    Date of Patent: November 20, 2001
    Assignee: Rosemount Aerospace Inc.
    Inventors: Dennis J. Cronin, Darren G. Jackson, David G. Owens
  • Patent number: 4670265
    Abstract: A method has been disclosed for treating type 1 or 2 herpes simplex virus comprising the successive steps of:(1) topically applying to the virus-affected areas of a person suffering from said virus, a topically effective amount of an anthaquinone, containing extract having an antiviral effect of type 1 or type 2 herpes simplex virus, and(2) repeating said topical application as required until the desired antiviral effect is observed.
    Type: Grant
    Filed: November 26, 1984
    Date of Patent: June 2, 1987
    Inventors: Robert J. Sydiskis, David G. Owen
  • Patent number: 4067467
    Abstract: A quick coupler device for use on tractor vehicles in which a quick attach plate is connected in place of the usual implement. Implements, equipped with complementary attachment fixtures, attach to the quick attach plate. A spring loaded latch automatically locks the implement to the quick attach plate and a projecting lug on the implement is engageable with a plate to hold the latch in an unlocked position.
    Type: Grant
    Filed: April 14, 1975
    Date of Patent: January 10, 1978
    Assignee: International Harvester Company
    Inventors: Arthur S. Datta, David G. Owens, R. Dale Moore
  • Patent number: RE39295
    Abstract: An ice detector for an aircraft comprises a strut and probe assembly, and it is positioned on the aircraft so that the pressure field around the ice detector causes a lower temperature region on the probe assembly compared to the aircraft. Ice will therefore form on the probe assembly before it forms on the aircraft to provide an early warning of icing conditions near freezing temperatures.
    Type: Grant
    Filed: September 10, 2003
    Date of Patent: September 19, 2006
    Assignee: Rosemount Aerospace, Inc.
    Inventors: Dennis J. Cronin, Darren G. Jackson, David G. Owens