Patents by Inventor Dean Emory Cameron

Dean Emory Cameron 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).

  • Reinforced elastomer panel
    Patent number: 6375122
    Abstract: A reinforced elastomer panel (100) has a first rigid member (104) with an edge (116) attached to a first end of an elastomer panel (114). The first rigid member (104) has a removable plate (106) that provides access to a cavity (108). Attached to the first rigid member (104) is a reinforcing member (102) that extends through the elastomer panel (114). A second ridge member (118) has an edge attached to a second end of the elastomer panel (114).
    Type: Grant
    Filed: August 17, 1998
    Date of Patent: April 23, 2002
    Assignee: The Boeing Company
    Inventors: Dean Emory Cameron, Paul Francis Geders, Michael Watson Geiger, Dennis Allan Roberts, Robert Henry Wille
  • Reinforced elastomer panel
    Patent number: 6027074
    Abstract: A reinforced elastomer panel (100) has a first rigid member (104) with an edge (116) attached to a first end of an elastomer panel (114). The first rigid member (104) has a removable plate (106) that provides access to a cavity (108). Attached to the first rigid member (104) is a reinforcing member (102) that extends through the elastomer panel (114). A second rigid member (118) has an edge attached to a second end of the elastomer panel (114).
    Type: Grant
    Filed: February 27, 1997
    Date of Patent: February 22, 2000
    Assignee: McDonnell Douglas
    Inventors: Dean Emory Cameron, Paul Francis Geders, Michael Watson Geiger, Dennis Allan Roberts, Robert Henry Wille
  • Fairing for an expandable bay
    Patent number: 5947417
    Abstract: A fairing (100) for an expandable bay of an has a ramp (108). A front linkage bar (102) has a first end pivotally connected to a finger (106) of the ramp (108) and a second end pivotally connected to the aircraft. A mating panel (112) is next to an interior edge (132) of the ramp (108) and pivotally connected to the ramp (108). An exterior elastomer panel (124) is connected between an exterior edge (126) of the ramp (108) and the aircraft.
    Type: Grant
    Filed: July 25, 1997
    Date of Patent: September 7, 1999
    Assignee: McDonnell Douglas
    Inventor: Dean Emory Cameron