Patents by Inventor Ozan Ates

Ozan Ates 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).

  • AIRCRAFT THROTTLE QUADRANT ASSEMBLY WITH INTEGRATED VISUAL INDICATOR FEATURE
    Publication number: 20250187740
    Abstract: A throttle quadrant system for an aircraft includes: a first throttle handle to control a first engine of the aircraft, the first throttle handle having a first activatable visual indicator integrated therein; a second throttle handle to control a second engine of the aircraft, the second throttle handle comprising a second activatable visual indicator integrated therein; and at least one controller to control activation and operation of the first activatable visual indicator and the second activatable visual indicator. The at least one controller responds to first engine data related to operating status of the first engine to selectively activate the first activatable visual indicator. The at least one controller also responds to second engine data related to operating status of the second engine to selectively activate the second activatable visual indicator.
    Type: Application
    Filed: February 21, 2025
    Publication date: June 12, 2025
    Applicant: Gulfstream Aerospace Corporation
    Inventors: Jeffrey Hausmann, Gary Freeman, Michael Knight, Ozan Ates, Kristin Medin, Jim Jordan, Scott Bohanan
  • Aircraft throttle quadrant assembly with integrated visual indicator feature
    Patent number: 12258138
    Abstract: A throttle quadrant system for an aircraft includes: a first throttle handle to control a first engine of the aircraft, the first throttle handle having a first activatable visual indicator integrated therein; a second throttle handle to control a second engine of the aircraft, the second throttle handle comprising a second activatable visual indicator integrated therein; and at least one controller to control activation and operation of the first activatable visual indicator and the second activatable visual indicator. The at least one controller responds to first engine data related to operating status of the first engine to selectively activate the first activatable visual indicator. The at least one controller also responds to second engine data related to operating status of the second engine to selectively activate the second activatable visual indicator.
    Type: Grant
    Filed: June 8, 2022
    Date of Patent: March 25, 2025
    Assignee: GULFSTREAM AEROSPACE CORPORATION
    Inventors: Jeffrey Hausmann, Gary Freeman, Michael Knight, Ozan Ates, Kristin Medin, Jim Jordan, Scott Bohanan
  • AIRCRAFT THROTTLE QUADRANT ASSEMBLY WITH INTEGRATED VISUAL INDICATOR FEATURE
    Publication number: 20230399117
    Abstract: A throttle quadrant system for an aircraft includes: a first throttle handle to control a first engine of the aircraft, the first throttle handle having a first activatable visual indicator integrated therein; a second throttle handle to control a second engine of the aircraft, the second throttle handle comprising a second activatable visual indicator integrated therein; and at least one controller to control activation and operation of the first activatable visual indicator and the second activatable visual indicator. The at least one controller responds to first engine data related to operating status of the first engine to selectively activate the first activatable visual indicator. The at least one controller also responds to second engine data related to operating status of the second engine to selectively activate the second activatable visual indicator.
    Type: Application
    Filed: June 8, 2022
    Publication date: December 14, 2023
    Applicant: Gulfstream Aerospace Corporation
    Inventors: Jeffrey Hausmann, Gary Freeman, Michael Knight, Ozan Ates, Kristin Medin, Jim Jordan, Scott Bohanan
  • Aircraft flight guidance panels with integrated standby displays
    Patent number: 11091274
    Abstract: A flight guidance panel includes a housing, a first flight guidance display, a second flight guidance display, a standby display, and a controller. The housing defines a first longitudinal side and a second longitudinal side. The first flight guidance display is disposed in the first longitudinal side of the housing and the second flight guidance display is disposed in the second longitudinal side of the housing. The standby display is disposed between the first flight guidance display and the second flight guidance display. The controller is configured for generating at least one functional panel indicating flight parameters on the first flight guidance display and on the second flight guidance display. The controller is further configured for generating standby flight information for presentation on the standby display.
    Type: Grant
    Filed: May 11, 2018
    Date of Patent: August 17, 2021
    Assignee: Gulfstream Aerospace Corporation
    Inventors: Scott Bohanan, Jeffrey Good, Jim Jordan, Ozan Ates, Kristin Medin
  • AIRCRAFT FLIGHT GUIDANCE PANELS WITH INTEGRATED STANDBY DISPLAYS
    Publication number: 20190344903
    Abstract: A flight guidance panel includes a housing, a first flight guidance display, a second flight guidance display, a standby display, and a controller. The housing defines a first longitudinal side and a second longitudinal side. The first flight guidance display is disposed in the first longitudinal side of the housing and the second flight guidance display is disposed in the second longitudinal side of the housing. The standby display is disposed between the first flight guidance display and the second flight guidance display. The controller is configured for generating at least one functional panel indicating flight parameters on the first flight guidance display and on the second flight guidance display. The controller is further configured for generating standby flight information for presentation on the standby display.
    Type: Application
    Filed: May 11, 2018
    Publication date: November 14, 2019
    Inventors: Scott Bohanan, Jeffrey Good, Jim Jordan, Ozan Ates, Kristin Medin