Patents by Inventor Jason W. Mazanec

Jason W. Mazanec 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: 8911203
    Abstract: A turbofan engine comprises an engine case. A gaspath extends through the engine case. A fan has a circumferential array of fan blades. A fan case encircles the fan blades radially outboard of the engine case. A plurality of fan case vanes extend aftward and outward from the engine case to the fan case. A forward frame comprises a plurality of vanes radially across the gaspath. A torque box couples the fan case vanes to the forward frame. A transmission couples a shaft to a fan shaft to drive the fan. A fan bearing assembly couples a stationary forward hub structure to the fan shaft.
    Type: Grant
    Filed: June 15, 2012
    Date of Patent: December 16, 2014
    Assignee: United Technologies Corporation
    Inventors: Gregory E. Reinhardt, Karl D. Blume, John P. Tirone, III, John C. Ditomasso, Enzo DiBenedetto, Jason W. Mazanec
  • Publication number: 20140301829
    Abstract: A turbofan engine comprises an engine case. A gaspath extends through the engine case. A fan has a circumferential array of fan blades. A fan case encircles the fan blades radially outboard of the engine case. A plurality of fan case vanes extend outward from the engine case to the fan case. A front frame assembly includes a plurality of vanes extending radially across the gaspath. A transmission couples a shaft to a fan shaft to drive the fan. A bearing assembly couples the shaft to the front frame assembly. A bearing support extends aftward and radially inward from the front frame assembly to the bearing assembly.
    Type: Application
    Filed: August 19, 2013
    Publication date: October 9, 2014
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Gregory E. Reinhardt, Enzo DiBenedetto, Jason W. Mazanec
  • Patent number: 8511987
    Abstract: A turbofan engine comprises an engine case. A gaspath extends through the engine case. A fan has a circumferential array of fan blades. A fan case encircles the fan blades radially outboard of the engine case. A plurality of fan case vanes extend outward from the engine case to the fan case. A front frame assembly includes a plurality of vanes extending radially across the gaspath. A transmission couples a shaft to a fan shaft to drive the fan. A bearing assembly couples the shaft to the front frame assembly. A bearing support extends aftward and radially inward from the front frame assembly to the bearing assembly.
    Type: Grant
    Filed: June 15, 2012
    Date of Patent: August 20, 2013
    Assignee: United Technologies Corporation
    Inventors: Gregory E. Reinhardt, Enzo DiBenedetto, Jason W. Mazanec
  • Patent number: 8439637
    Abstract: An assembly includes a first tapered roller bearing and a second tapered roller bearing and a bellows spring. The bellows spring is disposed adjacent the first tapered roller bearing and the second tapered roller bearing.
    Type: Grant
    Filed: November 20, 2009
    Date of Patent: May 14, 2013
    Assignee: United Technologies Corporation
    Inventors: Enzo DiBenedetto, Jason W. Mazanec
  • Publication number: 20120257960
    Abstract: A turbofan engine comprises an engine case. A gaspath extends through the engine case. A fan has a circumferential array of fan blades. A fan case encircles the fan blades radially outboard of the engine case. A plurality of fan case vanes extend outward from the engine case to the fan case. A front frame assembly includes a plurality of vanes extending radially across the gaspath. A transmission couples a shaft to a fan shaft to drive the fan. A bearing assembly couples the shaft to the front frame assembly. A bearing support extends aftward and radially inward from the front frame assembly to the bearing assembly.
    Type: Application
    Filed: June 15, 2012
    Publication date: October 11, 2012
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Gregory E. Reinhardt, Enzo DiBenedetto, Jason W. Mazanec
  • Publication number: 20120251306
    Abstract: A turbofan engine comprises an engine case. A gaspath extends through the engine case. A fan has a circumferential array of fan blades. A fan case encircles the fan blades radially outboard of the engine case. A plurality of fan case vanes extend aftward and outward from the engine case to the fan case. A forward frame comprises a plurality of vanes radially across the gaspath. A torque box couples the fan case vanes to the forward frame. A transmission couples a shaft to a fan shaft to drive the fan. A fan bearing assembly couples a stationary forward hub structure to the fan shaft.
    Type: Application
    Filed: June 15, 2012
    Publication date: October 4, 2012
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Gregory E. Reinhardt, Karl D. Blume, John P. Tirone, III, John C. Ditomasso, Enzo DiBenedetto, Jason W. Mazanec
  • Publication number: 20110123326
    Abstract: An assembly includes a first tapered roller bearing and a second tapered roller bearing and a bellows spring. The bellows spring is disposed adjacent the first tapered roller bearing and the second tapered roller bearing.
    Type: Application
    Filed: November 20, 2009
    Publication date: May 26, 2011
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Enzo DiBenedetto, Jason W. Mazanec