Patents by Inventor L. Porter Davis

L. Porter Davis 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: 6415674
    Abstract: A gear drive having a third order damper operating with the antibacklash gear so as to lower the impact of the antibacklash gear at high torques to reduce gear wear while maintaining good contact with the antibacklash gear at lower torques to maintain high accuracy and bandwidth.
    Type: Grant
    Filed: April 28, 2000
    Date of Patent: July 9, 2002
    Assignee: Honeywell International Inc.
    Inventors: L. Porter Davis, Christopher J. Heiberg, Jack H. Jacobs
  • Patent number: 6003849
    Abstract: A vibration damping and isolation apparatus including a passive damping mechanism and an active enhancement mechanism. The passive damping mechanism operates to dissipate vibratory and shock forces applied to the vibration damping and isolation apparatus. The passive damping mechanism includes first and second spaced damping elements. A first resilient structure connects the first damping element to the second damping element to define a primary fluid chamber between the first and second damping elements. The passive damping mechanism further includes a second resilient structure that defines a secondary fluid chamber which is in fluid communication with the primary fluid chamber via a fluid flow orifice. A fluid fills the primary fluid chamber, the secondary fluid chamber and the fluid flow orifice.
    Type: Grant
    Filed: March 4, 1997
    Date of Patent: December 21, 1999
    Assignee: Honeywell Inc.
    Inventors: L. Porter Davis, T. Tupper Hyde
  • Patent number: 4848525
    Abstract: A dual mode vibration isolator for reducing transmission of vibrations between a forward body and an aft body includes a mounting member positioned between the forward and aft bodies, a plurality of magnetic actuators each having an armature fixed to the forward body and a stator mounted on the mounting member, and a plurality of linear actuators pivotally connected between the aft body and the mounting member. The magnetic actuators support the forward body relative to the mounting member by magnetically supporting the armatures between paired stator cores in each stator. The magnetic actuators are controlled, preferably through local flux feedback loops, to permit the stators to vibrate relative to the armature without transmitting forces to the armatures, thus isolating the vibration of the aft body and mounting member from the forward body. The linear actuators extend and contract to reposition the forward body and mounting member relative to the aft body.
    Type: Grant
    Filed: November 2, 1987
    Date of Patent: July 18, 1989
    Assignee: The Boeing Company
    Inventors: A. Dean Jacot, Brian J. Hamilton, David C. Cunningham, L. Porter Davis