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1. 发明授权

US12018726B2 Electro-mechanical actuator with integrated fail-operational mechanism 有权
公开(公告)号：US12018726B2
公开(公告)日：2024-06-25
申请号：US18143911
申请日：2023-05-05
申请人： Skyryse, Inc.
发明人： David James Manzanares , Nozar George Sadeghi , Gonzalo Javier Rey , David Evan Edwards
IPC分类号： F16H25/20 , F16D55/224 , F16D65/18 , F16H25/22 , F16H25/24 , F16D66/00 , F16D121/24 , F16D125/40
CPC分类号： F16D65/18 , F16D55/224 , F16H25/2015 , F16H25/205 , F16H25/2204 , F16H25/2454 , F16D2066/003 , F16D2121/24 , F16D2125/40 , F16H2025/2081
摘要： Some embodiments relate to an electro-mechanical actuator that includes a screw, structurally segregated (split) housings, first and second nuts coupled to the screw, a sensor assembly, a plurality of motors, and a controller. The first nut is coupled to a first mounting point, and the second nut is coupled to a second mounting point. The sensor assembly may generate signals indicative of (e.g., relative) positions of left and right units of the actuator or positions of the first nut and the second nut on the screw. The controller controls the motors based on the signals generated by the sensor assembly. The motors may rotate each nut about a screw axis of the screw. This rotation results in one or both nuts moving along the screw. Movement between the first nut and the second nut along the screw adjusts a distance between the first mounting point and the second mounting point.

2. 发明申请

US20220326727A1 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.

3. 发明申请

US20220198945A1 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.

4. 发明申请

US20210132634A1 SYSTEM AND METHOD FOR SITUATIONAL AWARENESS, VEHICLE CONTROL, AND/OR CONTINGENCY PLANNING 有权
公开(公告)号：US20210132634A1
公开(公告)日：2021-05-06
申请号：US17146699
申请日：2021-01-12
申请人： Skyryse, Inc.
发明人： Mark Groden , Mitch Adler , Jonathan Reeves , Nur Harell , Christopher Ward
IPC分类号： G05D1/10 , G05D1/00 , G08G5/02 , B64D25/00 , G08G5/00 , B64C13/16 , B64C27/57 , B64D17/80 , B64D19/02
摘要： A method, preferably including: sampling inputs, determining aircraft conditions, and/or acting based on the aircraft conditions. A method, preferably including: sampling inputs, determining input reliability, determining guidance, and/or controlling aircraft operation. A method, preferably including: operating the vehicle, planning for contingencies, detecting undesired flight conditions, and/or reacting to undesired flight conditions. A system, preferably an aircraft such as a rotorcraft, configured to implement the method.

5. 发明申请

US20180217599A1 VEHICLE SYSTEM AND METHOD FOR PROVIDING SERVICES 审中-公开
公开(公告)号：US20180217599A1
公开(公告)日：2018-08-02
申请号：US15934162
申请日：2018-03-23
申请人： SkyRyse, Inc.
发明人： Mark Groden , Mitch Adler , Nur Harell
IPC分类号： G05D1/00 , G08G5/00 , G05D1/02 , B64F5/60 , B64D45/00
CPC分类号： G05D1/0088 , A61G3/001 , A61G2220/10 , B64C39/024 , B64C2201/024 , B64C2201/141 , B64C2201/146 , B64D45/00 , B64D45/04 , B64D45/08 , B64D2045/0085 , B64F1/18 , B64F5/60 , G05D1/0202 , G05D1/0676 , G06F19/00 , G06K9/00771 , G06Q10/047 , G06Q10/0832 , G06Q50/22 , G06Q50/30 , G07C5/008 , G08B7/06 , G08G5/0013 , G08G5/003 , G08G5/0034 , G08G5/0056 , G08G5/0091 , G08G5/0095 , G16H15/00 , G16H40/20
摘要： A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.

6. 发明授权

US09849044B1 Vehicle system and method for providing services 有权
公开(公告)号：US09849044B1
公开(公告)日：2017-12-26
申请号：US15643205
申请日：2017-07-06
申请人： SkyRyse Inc.
发明人： Mark Groden , Mitch Adler , Nur Harell
IPC分类号： G06F19/00 , A61G3/00 , G08G5/00 , B64F1/18 , G05D1/00 , B64D45/08 , B64F5/60 , G07C5/00 , G08B7/06
CPC分类号： G05D1/0088 , A61G3/001 , A61G2220/10 , B64D45/00 , B64D45/08 , B64D2045/0085 , B64F1/18 , B64F5/60 , G05D1/0202 , G06F19/00 , G06K9/00771 , G06Q10/047 , G06Q10/0832 , G06Q50/22 , G06Q50/30 , G07C5/008 , G08B7/06 , G08G5/0013 , G08G5/003 , G08G5/0034 , G08G5/0056 , G08G5/0091 , G08G5/0095 , G16H15/00 , G16H40/20
摘要： A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.

7. 外观设计

USD1049991S1 Mechanical controller 有权
公开(公告)号：USD1049991S1
公开(公告)日：2024-11-05
申请号：US29897475
申请日：2023-07-14
申请人： Skyryse, Inc.
设计人： Mark Daniel Groden , Justin Mark Ryan , Zeke Robert Markshausen
摘要： FIG. 1 is a top and front perspective view of a mechanical controller;
FIG. 2 is a front view thereof;
FIG. 3 is a rear view thereof;
FIG. 4 is a left view thereof;
FIG. 5 is a right view thereof;
FIG. 6 is a top view thereof; and,
FIG. 7 is a bottom view thereof.
The broken lines in the drawings are included for the purpose of illustrating portions of the mechanical controller that form no part of the claimed design.

8. 外观设计

USD1048996S1 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.

9. 发明公开

US20240326986A1 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.

10. 发明公开

US20240069890A1 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.

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