Patents by Inventor Sydney Davis

Sydney 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: 12120124
    Abstract: Techniques are described for providing a built-in “app” editor for an information technology (IT) and security operations application that enables users to create, modify, and test operation of apps under development within the editor. Some IT and security operations applications enable users to extend the applications by adding connectivity to third party technologies to run custom actions. For example, a user might create a custom app to enable an IT and security operations application to connect to an external service providing information about malicious Internet Protocol (IP) addresses, to connect to a relevant cloud provider service, or to interact with a firewall or other type of computing device used in a user's computing environment. Given the broad set of technologies that can be orchestrated by an IT and security operations application, apps broadly enable users to add custom functionality to interface with virtually any technology of interest.
    Type: Grant
    Filed: January 31, 2022
    Date of Patent: October 15, 2024
    Assignee: Splunk Inc.
    Inventors: Jacob Davis, Dekel Shahaff, Jeffrey Roecks, Sydney Flak, Navya Mehta, Ian Forrest, Sydney Karimi, Elton Xue
  • Patent number: 4798085
    Abstract: A test rig for measuring wear on flexible membrane material used as seal gers on air cushion vehicles includes a pump and nozzle for producing a shallow, high speed water flow and hydraulic actuators for moving the seal fingers into the flow. The fingers are moved into and out of the flow to simulate the effect of the ship crossing waves at high speed. A fan and air plenum inflate the seal fingers in a manner similar to normal operation.
    Type: Grant
    Filed: July 29, 1982
    Date of Patent: January 17, 1989
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Alexander Malakhoff, Sydney Davis
  • Patent number: 4657101
    Abstract: The purpose of this invention is to improve the life of transversely stiffened membrane (TSM) seals. To this end the inventors have introduced a segmented glass reinforced plastic (GRP) plank into the lower stiffened lobe portion, which is positioned beneath the bag segments of the TSM seal. The segmented (GRP) planks consist of planks separated by rubber spacers and sandwiched between two sheets of rubber coated nylon fabric.
    Type: Grant
    Filed: June 13, 1985
    Date of Patent: April 14, 1987
    Assignee: U.S. Dept. of Navy
    Inventors: Sydney Davis, Alexander Malakhoff
  • Patent number: 4436312
    Abstract: A seal structure for an air cushion vessel includes an inflatable bag secured to the hull and a transversely stiffened lobe portion maintained therebeneath. The stiffened lobe portion consists of a membrane with an array of spaced, transverse stiffener members connected thereto. The colinear stiffener members are interconnected in end-to-end relationship. According to one embodiment, the end portions of the stiffener members are connected to support stays which are connected either to the bag structure or to the forward portion of the hull. The support stays may comprise cable elements or membranes which form continuations of the stiffened lobe membrane. Additional support for the stiffened lobe portion is provided in the form of a plurality of rear support elements which set the orientation and configuration of the stiffened lobe portion and limit the downward deflection of the stiffened lobe portion.
    Type: Grant
    Filed: January 29, 1982
    Date of Patent: March 13, 1984
    Inventors: Sydney Davis, Alexander Malakhoff
  • Patent number: 4333413
    Abstract: A seal structure for an air cushion vessel includes an inflatable bag secd to the hull and a transversely stiffened lobe portion maintained therebeneath. The stiffened lobe portion consists of a membrane with an array of spaced, transverse stiffener members connected thereto. The colinear stiffener members are interconnected in end-to-end relationship.Generally, the end portions of the stiffener members are connected to support stays which are connected either to the bag structure or to the forward portion of the hull. The support stays may comprise cable elements or membranes which form continuations of the stiffened lobe membrane.Additional support for the stiffened lobe portion is provided in the form of a plurality of rear support elements which set the orientation and configuration of the stiffened lobe portion and limit the downward deflection of the stiffened lobe portion.
    Type: Grant
    Filed: January 23, 1980
    Date of Patent: June 8, 1982
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Sydney Davis, Alexander Malakhoff
  • Patent number: 4285414
    Abstract: A seal structure for an air cushion vessel includes an inflatable bag secd to the hull and a plurality of juxtaposed, interconnected planer members maintained in operative position beneath the bag by a plurality of support straps. Each planer member includes a transversely reinforced shell portion and a flexible, resilient membrane secured to the longitudinal edge portions of the shell portion to form a flexible planing surface for the seal structure. The planer members may have tapered aft end portions and curved planing surfaces to provide a gradual change of the interface between the planer members and the water.
    Type: Grant
    Filed: November 30, 1979
    Date of Patent: August 25, 1981
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Alexander Malakhoff, Sydney Davis
  • Patent number: 4228753
    Abstract: An arrangement for controlling the apparent curvature of diffuser vanes of turbine fan to reduce stalling of the vanes and increase efficiency of the fan output over a wider range of flow demand. Sensors responsive to pressure on opposite sides of the vanes selectively control the discharge of pressurized fluid from the diffuser vanes to effect their apparent curvature changes. The arrangement has particular use in a ride control system for surface effect ships.
    Type: Grant
    Filed: February 27, 1979
    Date of Patent: October 21, 1980
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Sydney Davis, John M. Durkin
  • Patent number: 4141506
    Abstract: A variable flow diffuser for use in air cushion vehicles to convert the ktic energy of the moving air from the main fan into potential energy of air pressure. The conversion is accomplished by passing the air flow from the fan through a flow splitter and diverting it radially outward in all directions along a plane perpendicular to the initial direction of the air flow. The volume of air passing through the diffuser is controlled by placing control vanes around the flow splitter or by moving the flow splitter and a back plate in and out of the air channel.
    Type: Grant
    Filed: July 15, 1977
    Date of Patent: February 27, 1979
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Jerry W. Cuthbert, Sydney Davis
  • Patent number: D525660
    Type: Grant
    Filed: March 1, 2005
    Date of Patent: July 25, 2006
    Inventor: Joe Sydney Davis