Patents by Inventor Daniel Shetzer

Daniel Shetzer 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).

  • Actuation system for a translating variable area fan nozzle
    Patent number: 9777671
    Abstract: A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating thrust reverser sleeve with a trailing edge. The thrust reverser sleeve is movably disposed aft of the nacelle's aft edge and is movable between a forward position and an aft position. A translating fan nozzle having a forward edge is movably disposed behind the trailing edge, and is movable between a stowed position and a deployed position. An upstream bypass flow exit is defined between the trailing edge and the forward edge when the fan nozzle is in the deployed position. An extendable actuation system is configured to move the fan nozzle between the stowed position and the deployed position.
    Type: Grant
    Filed: February 18, 2013
    Date of Patent: October 3, 2017
    Assignee: ROHR, INC.
    Inventors: Jihad I. Ramlaoui, Geoffrey Pinto, Daniel Shetzer, Daniel M. Amkraut, Andrew Robert Hawksworth, John Harvey, Alan K. Evans, Vikram Chandarana, Roger Moorhouse
  • ACTUATION SYSTEM FOR A TRANSLATING VARIABLE AREA FAN NOZZLE
    Publication number: 20160169158
    Abstract: A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating thrust reverser sleeve with a trailing edge. The thrust reverser sleeve is movably disposed aft of the nacelle's aft edge and is movable between a forward position and an aft position. A translating fan nozzle having a forward edge is movably disposed behind the trailing edge, and is movable between a stowed position and a deployed position. An upstream bypass flow exit is defined between the trailing edge and the forward edge when the fan nozzle is in the deployed position. An extendable actuation system is configured to move the fan nozzle between the stowed position and the deployed position.
    Type: Application
    Filed: February 18, 2013
    Publication date: June 16, 2016
    Applicants: Goodrich Actuation Systems Limited, Rohr, Inc.
    Inventors: Jihad I. Ramlaoui, Geoffrey Pinto, Daniel Shetzer, Daniel M. Amkraut, Andrew Robert Hawksworth, John Harvey, Alan K. Evans, Vikram Chandarana, Roger Moorehouse
  • Actuation system for a translating variable area fan nozzle
    Patent number: 8511062
    Abstract: A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating thrust reverser sleeve with a trailing edge. The thrust reverser sleeve is movably disposed aft of the nacelle's aft edge and is movable between a forward position and an aft position. A translating fan nozzle having a forward edge is movably disposed behind the trailing edge, and is movable between a stowed position and a deployed position. An upstream bypass flow exit is defined between the trailing edge and the forward edge when the fan nozzle is in the deployed position. An extendable actuation system is configured to move the fan nozzle between the stowed position and the deployed position.
    Type: Grant
    Filed: June 16, 2009
    Date of Patent: August 20, 2013
    Assignees: Rohr, Inc., Goodrich Actuation Systems Limited
    Inventors: Jihad I. Ramlaoui, Geoffrey Pinto, Daniel Shetzer, Daniel M. Amkraut, Andrew Robert Hawksworth, John Harvey, Alan K. Evans, Vikram Chandarana, Roger Moorhouse
  • ACTUATION SYSTEM FOR A TRANSLATING VARIABLE AREA FAN NOZZLE
    Publication number: 20100229528
    Abstract: A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating thrust reverser sleeve with a trailing edge. The thrust reverser sleeve is movably disposed aft of the nacelle's aft edge and is movable between a forward position and an aft position. A translating fan nozzle having a forward edge is movably disposed behind the trailing edge, and is movable between a stowed position and a deployed position. An upstream bypass flow exit is defined between the trailing edge and the forward edge when the fan nozzle is in the deployed position. An extendable actuation system is configured to move the fan nozzle between the stowed position and the deployed position.
    Type: Application
    Filed: June 16, 2009
    Publication date: September 16, 2010
    Applicants: Rohr, Inc.
    Inventors: Jihad I. Ramlaoui, Geoffrey Pinto, Daniel Shetzer, Daniel M. Amkraut, Andrew Robert Hawksworth, John Harvey, Alan K. Evans, Vikram Chandarana, Roger Moorhouse