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    COLLAPSIBLE COVER FOR ENGINE INLET AND METHOD FOR COVERING ENGINE INLET
    1.
    发明申请
    COLLAPSIBLE COVER FOR ENGINE INLET AND METHOD FOR COVERING ENGINE INLET 有权

    公开(公告)号：US20240417104A1

    公开(公告)日：2024-12-19

    申请号：US18817380

    申请日：2024-08-28

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Andrew Martin ,  Kristin Medin ,  Scott Bohanan

    IPC: B64F1/00 ,  A45B23/00 ,  F02C7/04

    Abstract: An engine inlet cover and a method for covering an engine inlet are provided. A method for covering an engine inlet includes providing a collapsible cover comprising a connection pin defining an axis; a frame including interconnected arms; and a web. Further, the method includes storing the collapsible cover in a stowed configuration in which the arms are aligned. Also, the method includes rotating the arms from the stowed configuration to an operating configuration in which the arms are radially spaced about the axis, enclosing the frame in the operating configuration with the web to define an interior volume, and placing the cover over the engine inlet.

    PRESET CAPTURE FOR A VEHICLE ENVIRONMENT MANAGEMENT SYSTEM
    3.
    发明申请
    PRESET CAPTURE FOR A VEHICLE ENVIRONMENT MANAGEMENT SYSTEM 有权

    公开(公告)号：US20210371106A1

    公开(公告)日：2021-12-02

    申请号：US17303392

    申请日：2021-05-27

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Stephen Spencer ,  Kristin Medin ,  Theron McDaniel ,  Preeti Menon ,  Kamen Kostov

    IPC: B64D11/00

    Abstract: An aircraft includes a passenger cabin, a plurality of settable cabin environment systems, and an aircraft environment management system. The passenger cabin has an environment. The plurality of settable cabin environment systems are in operable communication with the passenger cabin and each control an aspect of the environment based on a setting. The aircraft environment management system is in electronic communication with the plurality of settable cabin environment systems and is programmed to: receive a preset capture request from a user; store, as an environment preset, the setting as it existed for each of the plurality of settable cabin environment systems at a time of receipt of the preset capture request; receive a preset recall request for the environment preset; and recall the environment preset by adjusting the setting of each of the plurality of settable cabin environment systems according to the environment preset.

    Method and apparatus for auxiliary port function distinction
    4.
    发明授权
    Method and apparatus for auxiliary port function distinction 有权

    公开(公告)号：US11079823B1

    公开(公告)日：2021-08-03

    申请号：US16749055

    申请日：2020-01-22

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Kristin Medin ,  Timothy O'Hara ,  Dean Knight ,  Matthew Wallace ,  Kenneth Carden

    IPC: G06F1/26 ,  G06F13/20 ,  G06F3/14 ,  G06F13/42

    Abstract: The present application relates to providing auxiliary port function distinction by illuminating a first light emitting diode around a data transfer capable port wherein the first light emitting diode is illuminated in a first color, illuminating a second light emitting diode around a charge only port, receiving a first data connection request at the charge only port, illuminating the first light emitting diode a second color in response to the data connection request, receiving a second data connection request at the data transfer capable port, initiating a data connection handshake between a device connected to the data transfer capable port and a processor in response to the second data connection request, and illuminating the first light emitting diode the second color in response to the initiation of the data connection handshake.

    METHOD AND APPARATUS FOR AUXILIARY PORT FUNCTION DISTINCTION
    5.
    发明申请
    METHOD AND APPARATUS FOR AUXILIARY PORT FUNCTION DISTINCTION 有权

    公开(公告)号：US20210223840A1

    公开(公告)日：2021-07-22

    申请号：US16749055

    申请日：2020-01-22

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Kristin Medin ,  Timothy O'Hara ,  Dean Knight ,  Matthew Wallace ,  Kenneth Carden

    IPC: G06F1/26 ,  G06F13/20 ,  G06F13/42 ,  G06F3/14

    Abstract: The present application relates to providing auxiliary port function distinction by illuminating a first light emitting diode around a data transfer capable port wherein the first light emitting diode is illuminated in a first color, illuminating a second light emitting diode around a charge only port, receiving a first data connection request at the charge only port, illuminating the first light emitting diode a second color in response to the data connection request, receiving a second data connection request at the data transfer capable port, initiating a data connection handshake between a device connected to the data transfer capable port and a processor in response to the second data connection request, and illuminating the first light emitting diode the second color in response to the initiation of the data connection handshake.

    Aircraft throttle quadrant assembly with integrated visual indicator feature
    7.
    发明授权
    Aircraft throttle quadrant assembly with integrated visual indicator feature 有权

    公开(公告)号：US12258138B2

    公开(公告)日：2025-03-25

    申请号：US17806027

    申请日：2022-06-08

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Jeffrey Hausmann ,  Gary Freeman ,  Michael Knight ,  Ozan Ates ,  Kristin Medin ,  Jim Jordan ,  Scott Bohanan

    IPC: B64D31/04 ,  B64D31/14 ,  B64D45/00 ,  G05G1/015 ,  G05G1/02

    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.

    ADVANCED FLIGHT GUIDANCE PANEL WITH DISPLAY OF FUTURE WAYPOINTS AND CONSTRAINTS
    10.
    发明申请
    ADVANCED FLIGHT GUIDANCE PANEL WITH DISPLAY OF FUTURE WAYPOINTS AND CONSTRAINTS 有权

    公开(公告)号：US20210262803A1

    公开(公告)日：2021-08-26

    申请号：US16796464

    申请日：2020-02-20

    Applicant: Gulfstream Aerospace Corporation

    Inventor： Jeffrey Hausmann ,  Kristin Medin ,  Scott Bohanan ,  Jim Jordan

    IPC: G01C21/20 ,  G08G5/00 ,  G06F3/0484 ,  G06F3/0488

    Abstract: Flight control information systems, flight guidance display, and aircraft are provided. A navigational information system includes an input configured to receive a flight plan wherein the flight plan includes a first waypoint, a second waypoint, a third waypoint, and future waypoints, a user interface operative to generate a control signal in response to a user input, a display configured to display a graphical user interface, a processor operative to receive the flight plan from the input, to generate the graphical user interface to include to the first waypoint and the second waypoint and to couple the graphical user interface to the display, the processor being further operative to generate the graphical user interface in to include the first waypoint and the third waypoint in response to the control signal and to couple the graphical user interface to the display.

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