Patents by Inventor Brian D. Simpson

Brian D. Simpson 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: 9230549
    Abstract: A multi-modal communications system integrates multiple different communications channels and modalities into a single user interface that enables operators to monitor and respond to multiple audio and text communications.
    Type: Grant
    Filed: May 18, 2011
    Date of Patent: January 5, 2016
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Dianne K. Popik, Victor S Finomore, Jr., Brian D Simpson, Douglas S. Brungart
  • Publication number: 20100084111
    Abstract: A liquid to liquid heat exchanger for a marine engine cooling system disposes a tube bundle within a non-metallic shell, provides a thermostat within an integral portion of the shell, uses bolts that both push and pull respective end caps when rotated, and in one embodiment provides an integral deaeration reservoir to remove entrained gases from a liquid of a closed cooling system.
    Type: Application
    Filed: July 11, 2006
    Publication date: April 8, 2010
    Inventors: Matthew W. Jaeger, Brian D. Simpson, Ritchie C. Griffin
  • Patent number: 7482951
    Abstract: An auditory attitude indicator for aircraft that includes an audio source providing an audible signal, a? stereo headset with a left side and a right side, an aircraft avionics system that provides at least aircraft pitch data and roll data to an audio processor unit. The audio processor unit includes at least one lookup table of coefficients corresponding to a plurality of possible aircraft pitch and roll orientations and at least two selectable multipoint finite impulse response filters. The first selectable multipoint finite impulse response filter having a first coefficient selected by the audio processing unit from the lookup table based upon the aircraft pitch data and roll data for varying the audible signal to the stereo headset left side. The second selectable multipoint impulse response filter for varying the audible signal to the stereo headset right side having a second coefficient selected by the audio processing unit from the lookup table based upon the aircraft pitch data and roll data.
    Type: Grant
    Filed: September 25, 2006
    Date of Patent: January 27, 2009
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Douglas S. Brungart, Brian D. Simpson
  • Patent number: 7341039
    Abstract: A lubrication system for an in-line engine which has a piston symmetry plane that is tilted relative to a vertical plane is provided with an oil pan and windage tray that facilitates the transfer of oil from a rotating crankshaft to the oil pan without excessive aeration. In addition, it facilitates the removal of entrained air from liquid oil as it passes from the crankshaft to a pool of oil collected in an oil pan. A windage tray is provided with a louver structure and a louver opening structure that assists this passage of oil droplets without undue aeration being caused.
    Type: Grant
    Filed: May 12, 2006
    Date of Patent: March 11, 2008
    Assignee: Brunswick Corporation
    Inventors: Wayne M. Jaszewski, Joshua K. English, George E. Phillips, Brian D. Simpson
  • Patent number: 6652337
    Abstract: The present invention provides a relationship between the exhaust passages and coolant passages of the exhaust manifold and exhaust elbow which serves to maintain the joint of the exhaust passage at a higher temperature than would be possible with known exhaust manifolds and exhaust elbows. By providing a space between surfaces of a raised exhaust portion of the components and surfaces of the raised coolant portions of the exhaust system, leakage from the coolant conduits to the exhaust cavities is avoided. The space provided between exhaust portions of the manifold and elbow and coolant portions of the manifold and elbow, near the joint between these components, provides the two advantages of maintaining a higher exhaust connection between the manifold and elbow and also preventing coolant leakage from flowing from the coolant passages to the exhaust passages of the exhaust system.
    Type: Grant
    Filed: March 15, 2002
    Date of Patent: November 25, 2003
    Assignee: Brunswick Corporation
    Inventors: Andrew K. Logan, Christopher J. Luckett, Matthew W. Jaeger, Brian D. Simpson
  • Patent number: 6412595
    Abstract: A muffler is provided for a marine propulsion system in which an initial portion causes a downward flow of exhaust gas and entrained water from an exhaust manifold. The transition section directs the exhaust gas toward an egress section which extends upwardly from the transition section. The various sections of the exhaust path can be configured to form one or more loops which define one or more water collection regions.
    Type: Grant
    Filed: July 26, 2000
    Date of Patent: July 2, 2002
    Assignee: Brunswick Corporation
    Inventors: James M. Horak, Brian D. Simpson
  • Patent number: 5964662
    Abstract: A coupling device is provided with two flanges and a resilient annular member disposed between facing surfaces of the flanges. The resilient annular member is provided with a central opening through which a metallic spring is disposed to exert a resistive force against compression of the resilient annular member between the two flanges. The device is particularly well suited for use in a marine propulsion system because of the propulsive force exerted on the shaft system by the propeller. In one particularly preferred arrangement, each of the two flanges is provided with three holes, and the resilient annular member is provided with six holes. The two flanges are offset rotationally to place each of the holes of one flange in alignment with an interstitial space between the holes of the other flange.
    Type: Grant
    Filed: December 11, 1997
    Date of Patent: October 12, 1999
    Assignee: Brunswick Corporation
    Inventors: James M. Horak, Brian D. Simpson
  • Patent number: 5832903
    Abstract: A fuel supply system for a marine propulsion system having an electronically controlled fuel injection system eliminates the need for a vapor separator. The system pumps an excessive amount of fuel through a plumbed fuel supply loop and cools recirculated fuel to cool all the components in the plumbed fuel supply loop, i.e. a continuous duty, constant displacement fuel pump; a pressure regulator; and a water separating fuel filter. Recirculated fuel flows from the pressure regulator to the water separating fuel filter as does make-up fuel from a fuel tank. The fuel stream from the water separating fuel filter flows to the low-pressure side of the fuel pump, which pumps the fuel through the plumb fuel supply loop. A fuel injection portion of the fuel flows to the engine for combustion, while the remaining portion of the fuel is recirculated. The recirculated portion of the fuel is cooled, preferably using a water-cooled heat exchanger.
    Type: Grant
    Filed: June 2, 1997
    Date of Patent: November 10, 1998
    Assignee: Brunswick Corp.
    Inventors: Brian R. White, Vince E. Notareschi, Grant W. Hines, Brian D. Simpson, Timothy M. Baer, Matthew W. Jaeger, Daniel E. Clarkson, James Michael Horak