Patents by Inventor Brian Curtis Hale

Brian Curtis Hale 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: 10974846
    Abstract: A detection system for detecting failure in a primary load path of a flight control actuator and annunciating engagement in a secondary load path of the flight control actuator. The failure in the primary load path causes axial movement in a secondary rod of the secondary load path. The detection system includes a secondary mounting assembly that guides axial movement of the secondary rod; and a sensor that electronically detects relative axial displacement between the secondary rod and the secondary mounting assembly upon a primary load path failure and annunciates transition to engagement in the secondary load path.
    Type: Grant
    Filed: December 7, 2017
    Date of Patent: April 13, 2021
    Assignee: Parker-Hannifin Corporation
    Inventors: Brian Curtis Hale, Abbas M. Charafeddine
  • Publication number: 20180162550
    Abstract: A detection system for detecting failure in a primary load path of a flight control actuator and annunciating engagement in a secondary load path of the flight control actuator. The failure in the primary load path causes axial movement in a secondary rod of the secondary load path. The detection system includes a secondary mounting assembly that guides axial movement of the secondary rod; and a sensor that electronically detects relative axial displacement between the secondary rod and the secondary mounting assembly upon a primary load path failure and annunciates transition to engagement in the secondary load path.
    Type: Application
    Filed: December 7, 2017
    Publication date: June 14, 2018
    Inventors: Brian Curtis Hale, Abbas M. Charafeddine
  • Patent number: 8985510
    Abstract: A stabilizer actuator has a first end for connecting to an aircraft support structure and a second end for connecting to a stabilizer. The actuator includes a primary load path for transmittal of loads acting on the stabilizer to the aircraft support structure, and a secondary load path for transmittal of loads acting on the stabilizer to the aircraft support structure upon failure of the primary load path. The secondary load path includes a tie rod extending along a longitudinal axis, a load path locking mechanism coupled to the tie rod, a lock housing having a central bore for receiving the locking mechanism, and at least one radially movable segment that, upon failure of the primary load path, moves radially to lock the tie rod to the lock housing against axial and/or radial movement.
    Type: Grant
    Filed: November 15, 2012
    Date of Patent: March 24, 2015
    Assignee: Parker-Hannifin Corporation
    Inventor: Brian Curtis Hale