Patents by Inventor Daniel William Hyatt

Daniel William Hyatt 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: 9975650
    Abstract: A lifting tool 100 form part of a lifting apparatus associated with an aircraft handler 10 for applying a lifting load to an undercarriage of an aircraft. The lifting apparatus comprise a pair of opposed lifting tools 100 which engage end portions of an undercarriage wheel axle 300 for lifting. Each lifting tool 100 has a body 101 with a cavity 103 therein filled with a plurality of axially displaceable closely packed pins 105 which permit insertion of a portion of the axle or adaptor means into the cavity, and other pins, in use, surrounding said portion provide support and transfer the lift load to the surrounding body 101.
    Type: Grant
    Filed: July 17, 2015
    Date of Patent: May 22, 2018
    Assignee: CURTISS-WRIGHT FLOW CONTROL (UK) LIMITED
    Inventor: Daniel William Hyatt
  • Patent number: 9428283
    Abstract: A lifting tool 100 form part of a lifting apparatus associated with an aircraft handler 10 for applying a lifting load to an undercarriage of an aircraft. The lifting apparatus comprise a pair of opposed lifting tools 100 which engage end portions of an undercarriage wheel axle 300 for lifting. Each lifting tool 100 has a body 101 with a cavity 103 therein filled with a plurality of axially displaceable closely packed pins 105 which permit insertion of a portion of the axle or adaptor means into the cavity, and other pins, in use, surrounding said portion provide support and transfer the lift load to the surrounding body 101.
    Type: Grant
    Filed: November 19, 2004
    Date of Patent: August 30, 2016
    Assignee: Curtiss-Wright Flow Control (UK) Limited
    Inventor: Daniel William Hyatt
  • Publication number: 20150321771
    Abstract: A lifting tool 100 form part of a lifting apparatus associated with an aircraft handler 10 for applying a lifting load to an undercarriage of an aircraft. The lifting apparatus comprise a pair of opposed lifting tools 100 which engage end portions of an undercarriage wheel axle 300 for lifting. Each lifting tool 100 has a body 101 with a cavity 103 therein filled with a plurality of axially displaceable closely packed pins 105 which permit insertion of a portion of the axle or adaptor means into the cavity, and other pins, in use, surrounding said portion provide support and transfer the lift load to the surrounding body 101.
    Type: Application
    Filed: July 17, 2015
    Publication date: November 12, 2015
    Inventor: Daniel William Hyatt