Patents by Inventor Michael J. McNulty

Michael J. McNulty 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: 7083383
    Abstract: A trim tab assembly for a helicopter rotor blade includes a plurality of metal panels that are secured to the trailing edge of a composite material helicopter blade. Each of the metal panels can be bent relative to the rotor blade to tune the aerodynamic properties of the rotor blade.
    Type: Grant
    Filed: April 26, 2004
    Date of Patent: August 1, 2006
    Assignee: The Boeing Company
    Inventors: Robert T. Loftus, Michael J. McNulty, Keith B. Smith
  • Patent number: 6698409
    Abstract: Engine speed data N and engine fueling data MFDES are processed by a strategy (22) that multiplies (28) fueling transient data MFDES TRANSIENT and speed-based modifier data EGR_N_TRANS_MULT to develop speed-based fueling transient data. The speed-based fueling transient data is then processed according to a function (32) that correlates values of a fueling transient modifier with values of speed-based fueling transient data to develop exhaust gas recirculation modifier data. The exhaust gas recirculation modifier data and basic exhaust gas recirculation data are multiplied (34) to develop modified exhaust gas recirculation data, and exhaust gas is recirculated in accordance with the modified exhaust gas recirculation data. Using engine speed as a determinant of the extent to which the basic EGR rate should be modified during a fueling transient enables better control over certain exhaust emissions over certain speed ranges.
    Type: Grant
    Filed: December 9, 2002
    Date of Patent: March 2, 2004
    Assignee: International Engine Intellectual Property Company, LLC
    Inventors: Michael P. Kennedy, Michael J. McNulty, James T. Beaucaire, David V. Rodgers
  • Patent number: 6427445
    Abstract: A variable nozzle turbocharger (12) creates engine boost. Boost is controlled by controlling the position of vanes within turbocharger. A processor develops a control signal (29) for controlling vane position. The processor develops a value for desired boost and processes that value with a value. corresponding to the amount of boost being created by the turbocharger to generate error data (48A) defining error between the amount of boost being created by the turbocharger and the desired boost, and the processor develops a component of the control signal by P-LI-D processing (62) of the error data. Other components of the control signal are a feed-forward value from a look-up table (34) and a value from an overspeed protection function (60).
    Type: Grant
    Filed: February 5, 2001
    Date of Patent: August 6, 2002
    Assignee: International Engine Intellectual Property Company, L.L.C.
    Inventors: Emad S. Isaac, John E. Bernhardt, Michael J. McNulty
  • Publication number: 20020029772
    Abstract: A variable nozzle turbocharger (12) creates engine boost. Boost is controlled by controlling the position of vanes within turbocharger. A processor develops a control signal (29) for controlling vane position. The processor develops a value for desired boost and processes that value with a value corresponding to the amount of boost being created by the turbocharger to generate error data (48A) defining error between the amount of boost being created by the turbocharger and the desired boost, and the processor develops a component of the control signal by P-LI-D processing (62) of the error data. Other components of the control signal are a feed-forward value from a look-up table (34) and a value from an overspeed protection function (60).
    Type: Application
    Filed: February 5, 2001
    Publication date: March 14, 2002
    Inventors: Emad S. Isaac, John E. Bernhardt, Michael J. McNulty