Patents by Inventor Ernest Coleman

Ernest Coleman 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: 8024079
    Abstract: A computer implemented method, apparatus, and computer usable program product for symmetric and anti-symmetric control of aircraft flight control surfaces to reduce wing-body loads. Commands are sent to symmetrically deploy outboard control surfaces to shift wing air-loads inboard based on airplane state and speed brake deployment. Surface rate retraction on a wing with peak loads is limited to reduce maximum loads due to wheel checkback accompanied by utilization of opposite wing control surfaces to retain roll characteristics. Airloads are shifted inboard on a swept wing to move the center of pressure forward, thereby reducing the tail load required to perform a positive gravity maneuver. In a negative gravity maneuver, speed brakes are retracted, thereby reducing the positive tail load and reducing the aft body design loads. High gain feedback commands are filtered from wing structural modes above one hertz by a set of linear and non-linear filters.
    Type: Grant
    Filed: May 20, 2008
    Date of Patent: September 20, 2011
    Assignee: The Boeing Company
    Inventors: Kioumars Najmabadi, William F. Shivitz, Edward Ernest Coleman, John Koon-hung Ho, Richard D. Johnson, William F. Carver, David W. Grubb, Robert James McIntosh
  • Publication number: 20090292405
    Abstract: A computer implemented method, apparatus, and computer usable program product for symmetric and anti-symmetric control of aircraft flight control surfaces to reduce wing-body loads. Commands are sent to symmetrically deploy outboard control surfaces to shift wing air-loads inboard based on airplane state and speed brake deployment. Surface rate retraction on a wing with peak loads is limited to reduce maximum loads due to wheel checkback accompanied by utilization of opposite wing control surfaces to retain roll characteristics. Airloads are shifted inboard on a swept wing to move the center of pressure forward, thereby reducing the tail load required to perform a positive gravity maneuver. In a negative gravity maneuver, speed brakes are retracted, thereby reducing the positive tail load and reducing the aft body design loads. High gain feedback commands are filtered from wing structural modes above one hertz by a set of linear and non-linear filters.
    Type: Application
    Filed: May 20, 2008
    Publication date: November 26, 2009
    Inventors: Kioumars Najmabadi, William F. Shivitz, Edward Ernest Coleman, John Koon-hung Ho, Richard D. Johnson, William F. Carver, David W. Grubb, Robert James McIntosh
  • Publication number: 20060143971
    Abstract: A fishing lure assembly and the method of making a unique fill composition that causes attractant scent compounds to be dispensed from the fishing lure assembly. The fishing lure assembly has a body that can retain a volume of fill composition. The fill composition contains an ion exchange material and attractant scent compounds that are ionically bonded together. When the fishing lure is submersed in water, the fill composition is exposed to a controlled flow of water. In an ion exchange reaction, ions contained within the water bond to the ion exchange material and thus free the previously bonded attractant scent compounds. The freed attractant scent compounds flow out of the lure assembly with the passing water.
    Type: Application
    Filed: December 31, 2004
    Publication date: July 6, 2006
    Inventors: Gregory Mitchell, Ernest Coleman