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    FOUR-AXIS MECHANICAL CONTROLLER
    2.
    发明申请
    FOUR-AXIS MECHANICAL CONTROLLER 有权

    公开(公告)号：US20220326727A1

    公开(公告)日：2022-10-13

    申请号：US17715316

    申请日：2022-04-07

    申请人： Skyryse, Inc.

    发明人： David Anthony Cowling ,  David James Manzanares ,  Gonzalo Javier Rey

    IPC分类号： G05G9/047 ,  G05G5/03

    摘要： A mechanical controller provides four-axis control of a vehicle's position and movement. For example, the controller provides control of a vehicle's operations through a lateral axis, longitudinal axis, directional axis, and a grip axis (e.g., operating a thumbwheel of the mechanical controller that provides additional control inputs to the vehicle). The mechanical controller can provide independent force feel mechanisms in each of the lateral, longitudinal, and directional axes of movement. Additionally, the mechanical controller may provide a redundant force feel mechanism (e.g., for increased safety). For example, redundant springs and dampers may be incorporated in each axis's force feel mechanism. The mechanical controller may include a plunger and spring assembly to provide a force feel mechanism in the lateral and longitudinal axes. In addition to this spring force, surfaces of a contact region between the plunger and a plunger actuating plate may be shaped to produce force feel characteristics.

    UNPLANNED LANDING SITE SELECTION FOR AIRCRAFT
    3.
    发明申请
    UNPLANNED LANDING SITE SELECTION FOR AIRCRAFT 有权

    公开(公告)号：US20220198945A1

    公开(公告)日：2022-06-23

    申请号：US17559048

    申请日：2021-12-22

    申请人： Skyryse, Inc.

    发明人： GONZALO JAVIER REY ,  MARK DANIEL GRODEN

    IPC分类号： G08G5/00 ,  G08G5/02

    摘要： A landing site selection system selects landing sites for unplanned landings for small aircraft. The landing site selection system may generate a landing site database comprising parameters for landing sites. The landing sites may be any location where an aircraft may potentially land. The landing site selection system may monitor aircraft conditions and determine that an unplanned landing may be desirable. The landing site selection system may select potential landing sites based on the aircraft conditions and the landing site parameters. The landing site selection system may display landing site parameters for the selected landing sites to a pilot to allow the pilot to select a landing site. The landing site selection may provide navigation instructions or autonomously navigate the aircraft to the landing site.

    Electronic display console and mechanical controller configuration
    6.
    外观设计
    Electronic display console and mechanical controller configuration 有权

    公开(公告)号：USD1048996S1

    公开(公告)日：2024-10-29

    申请号：US29897478

    申请日：2023-07-14

    申请人： Skyryse, Inc.

    设计人： Mark Daniel Groden ,  Justin Mark Ryan ,  Zeke Robert Markshausen ,  Daniel James Stillion

    摘要： FIG. 1 is a front and left perspective view of a first embodiment of an electronic display console and mechanical controller configuration in a vehicle cockpit environment;
    FIG. 2 is a rear and right perspective view thereof;
    FIG. 3 is a top and front perspective view of the electronic display console and mechanical controller configuration of FIGS. 1 and 2;
    FIG. 4 is a front view thereof;
    FIG. 5 is a rear view thereof;
    FIG. 6 is a right view thereof;
    FIG. 7 is a left view thereof;
    FIG. 8 is a top view thereof;
    FIG. 9 is a bottom view thereof;
    FIG. 10 is a top and front perspective view of a second embodiment of an electronic display console and mechanical controller configuration;
    FIG. 11 is a front view thereof;
    FIG. 12 is a rear view thereof;
    FIG. 13 is a left view thereof;
    FIG. 14 is a right view thereof;
    FIG. 15 is a top view thereof;
    FIG. 16 is a bottom view thereof;
    FIG. 17 is a top and front perspective view of a third embodiment of an electronic display console and mechanical controller configuration;
    FIG. 18 is a front view thereof;
    FIG. 19 is a rear view thereof;
    FIG. 20 is a right view thereof;
    FIG. 21 is a left view thereof;
    FIG. 22 is a top view thereof;
    FIG. 23 is a bottom view thereof;
    FIG. 24 is a top and front perspective view of a fourth embodiment of an electronic display console and mechanical controller configuration;
    FIG. 25 is a front view thereof;
    FIG. 26 is a rear view thereof;
    FIG. 27 is a left view thereof;
    FIG. 28 is a right view thereof;
    FIG. 29 is a top view thereof;
    FIG. 30 is a bottom view thereof;
    FIG. 31 is a top and front perspective view of a fifth embodiment of an electronic display console and mechanical controller configuration;
    FIG. 32 is a front view thereof;
    FIG. 33 is a rear view thereof;
    FIG. 34 is a right view thereof;
    FIG. 35 is a left view thereof;
    FIG. 36 is a top view thereof;
    FIG. 37 is a bottom view thereof;
    FIG. 38 is a top and front perspective view of a sixth embodiment of an electronic display console and mechanical controller configuration;
    FIG. 39 is a front view thereof;
    FIG. 40 is a rear view thereof;
    FIG. 41 is a left view thereof;
    FIG. 42 is a right view thereof;
    FIG. 43 is a top view thereof; and,
    FIG. 44 is a bottom view thereof.
    The broken lines in the drawings are included for the purpose of illustrating portions of the electronic display console and mechanical controller configuration that form no part of the claimed design.

    REDUNDANCY SYSTEMS FOR FLY-BY-WIRE VEHICLES
    7.
    发明公开
    REDUNDANCY SYSTEMS FOR FLY-BY-WIRE VEHICLES 审中-公开

    公开(公告)号：US20240326986A1

    公开(公告)日：2024-10-03

    申请号：US18597818

    申请日：2024-03-06

    申请人： Skyryse, Inc.

    发明人： Gonzalo Javier Rey ,  David James Manzanares ,  Sylvain Alarie ,  Deon Esterhuizen

    IPC分类号： B64C13/50

    CPC分类号： B64C13/505 ,  B64C13/503

    摘要： A universal vehicle control router for fly-by-wire aircraft may include multiple vehicle control computers, such as flight control computers. Each flight control computer may be part of an independent channel that provides instructions to multiple actuators to control multiple vehicle components. Each channel is a distinct pathway capable of delivering a system function, such as moving an actuator. Each flight control computer may include a fully analyzable and testable voter (FAT voter). In the event of a failure to one of the flight control computers, the FAT voters may cause the failing flight control computer to be ignored or shut off power. Each flight control computer may comprise a backup battery. In the event of a power disruption from the primary power source, such as a generator and primary battery, the backup battery may power the flight control computer and all actuators.

    SOFTWARE UPDATE SYSTEM FOR AERIAL VEHICLES
    8.
    发明公开
    SOFTWARE UPDATE SYSTEM FOR AERIAL VEHICLES 审中-公开

    公开(公告)号：US20240069890A1

    公开(公告)日：2024-02-29

    申请号：US18239652

    申请日：2023-08-29

    申请人： Skyryse, Inc.

    发明人： Mark Daniel Groden ,  Gonzalo Javier Rey

    IPC分类号： G06F8/65

    CPC分类号： G06F8/65

    摘要： A software update system is disclosed for managing a remote software updating process for aerial vehicles. Responsive to receiving an indication from a companion application that an update for a display or a Flight Control Computer (FCC) is available for installation, the software update system may determine if a set of requirements are met by retrieving information associated with the aircraft from the sensors of the aircraft. The software update system may determine whether the aircraft is suitable for performing the installation of the update by checking a set of requirements and retrieving information from the sensors of the aircraft. The software update system may further determine if the update is for a display or an FCC and perform a different remote update process for each type of update correspondingly.

    Vehicle control and interface system
    9.
    发明授权
    Vehicle control and interface system 有权

    公开(公告)号：US11874674B2

    公开(公告)日：2024-01-16

    申请号：US17370415

    申请日：2021-07-08

    申请人： Skyryse, Inc.

    发明人： Mark Groden ,  Gonzalo Javier Rey ,  Christopher Camilo Cole ,  Christopher Ryan Smith

    IPC分类号： G05D1/10 ,  G05D1/00

    CPC分类号： G05D1/101 ,  G05D1/0016 ,  G05D1/0088

    摘要： A system and a method are disclosed for a vehicle control and interface system configured to facilitate control of different vehicles through universal mechanisms. The vehicle control and interface system can be integrated with different types of vehicles (e.g., rotorcraft, fixed-wing aircraft, motor vehicles, watercraft, etc.) in order to facilitate operation of the different vehicles using universal vehicle control inputs. In particular, the vehicle control and interface system converts universal vehicle control inputs describing a requested trajectory of a vehicle received from one or more universal vehicle control interfaces into commands for specific actuators of the vehicle configured to adjust a current trajectory of the vehicle to the requested trajectory. In order to convert the universal vehicle control inputs to actuator commands the vehicle control and interface system processes the universal vehicle control inputs using a universal vehicle control router.