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公开(公告)号：US20240300660A1
公开(公告)日：2024-09-12
申请号：US18667566
申请日：2024-05-17
Applicant: Joby Aero, Inc.
Inventor： JoeBen Bevirt , Alex Stoll , Martin van der Geest , Scott MacAfee , Jason Ryan
CPC classification number: B64D27/24 , B60L58/22 , B60L2200/10 , B64C29/0033 , B64D2221/00
Abstract: A vertical takeoff and landing aircraft includes a starboard wing, a port wing, first and second tilt rotors coupled to the port and starboard wings respectively, and first and second batteries. A pair of control surfaces are arranged on a first side of the mid-sagittal plane of the aircraft, the pair comprising a first and a second control surface. A first flight actuator is electrically connected to the first battery and a second flight actuator is electrically connected to the second battery. The first and second flight actuators are mechanically connected to the first and second control surfaces respectively.
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公开(公告)号：US12012206B2
公开(公告)日：2024-06-18
申请号：US18227310
申请日：2023-07-28
Applicant: Joby Aero, Inc.
Inventor： Gregor Veble Mikic , Alex Stoll , JoeBen Bevirt
Abstract: The aircraft can include: an airframe, a tilt mechanism, a payload housing, and can optionally include an impact attenuator, a set of ground support members (e.g., struts), a set of power sources, and a set of control elements. The airframe can include: a set of rotors and a set of support members. By utilizing a larger rotor blade area (and/or larger rotor disc area) and adjusting the blade pitch and RPM, the rotors can augment the lift generated by the aerodynamic profile of the aircraft in the forward flight mode in addition to providing forward thrust. Variants generating lift with the rotors can reduce or eliminate additional control surfaces (e.g., wing flaps, ailerons, ruddervators, elevators, rudder, etc.) on the aircraft since the thrust and motor torque is controllable (thereby indirectly controlling lift) at each rotor, thereby enabling pitch, yaw, and/or roll control during forward flight.
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23.发明公开公开(公告)号：US20230351912A1
公开(公告)日：2023-11-02
申请号：US18213264
申请日：2023-06-23
Applicant: Joby Aero, Inc.
Inventor： Gregor Veble Mikic , JoeBen Bevirt , Alex Stoll , Jeremy Bain
Abstract: A method and system for modeling aerodynamic interactions in complex eVTOL configurations for realtime flight simulations and hardware testing which includes decomposing the aircraft into aerodynamic subcomponents, wherein the interactions between these components are handled by flow simulations of the surrounding fluid, which may be Euler flow CFD simulations. A computer generated simulation can be used to analyze the fluid flow and pressures, the forces delivered by an aircraft into the fluid and the forces onto the aircraft from the fluid, to determine the position and attitude of the aircraft, and other aspects. The system may be used as a flight simulator for pilot training in a realtime environment. The system may be used to support component testing using an interface to those components, such as flight electronics and actuators, to test the components in high fidelity simulations of actual flight demands on those components. The system may also be used to support design analysis in non-realtime to run numerous simulations on different designs and to provide comparative output.
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公开(公告)号：US20230322362A1
公开(公告)日：2023-10-12
申请号：US18121001
申请日：2023-03-14
Applicant: Joby Aero, Inc.
Inventor： Gregor Veble Mikic , JoeBen Bevirt , Jeremy Bain , Alex Stoll
CPC classification number: B64C13/16 , G05D1/102 , B64C29/0033
Abstract: A method for the control of a vertical take-off and landing (VTOL) aircraft which reduces the acoustic profile of the rotary airfoil in hover for VTOL applications. The rotary airfoil incurs an efficiency penalty in order to improve the acoustic performance during hover. The aircraft operates the rotary airfoils of the propeller during hover in the hover angle of attack range, and the aircraft operates the rotary airfoils during forward flight in the forward angle of attack range.
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公开(公告)号：US11721236B2
公开(公告)日：2023-08-08
申请号：US17079514
申请日：2020-10-25
Applicant: Joby Aero, Inc.
Inventor： Gregor Veble Mikic , JoeBen Bevirt , Alex Stoll , Jeremy Bain
Abstract: A method and system for modeling aerodynamic interactions in complex eVTOL configurations for realtime flight simulations and hardware testing which includes decomposing the aircraft into aerodynamic subcomponents, wherein the interactions between these components are handled by flow simulations of the surrounding fluid, which may be Euler flow CFD simulations. The system may be used as a flight simulator for pilot training in a realtime environment. The system may be used to support component testing using an interface to those components, such as flight electronics and actuators, to test the components in high fidelity simulations of actual flight demands on those components. The system may also be used to support design analysis in non-realtime to run numerous simulations on different designs and to provide comparative output.
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Patent Agency Ranking
26.发明授权公开(公告)号：US11613370B2
公开(公告)日：2023-03-28
申请号：US17388262
申请日：2021-07-29
Applicant: JOBY AERO, INC.
Inventor： Joeben Bevirt , Alex Stoll
Abstract: An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle may have deployment mechanisms which deploy electric motor driven propellers from a forward facing to a vertical orientation. The wing mounted rotor assemblies may have split nacelles, wherein a forward portion of the nacelle deploys along with the electric motor and the propeller.
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27.发明授权公开(公告)号：US11565607B2
公开(公告)日：2023-01-31
申请号：US17348193
申请日：2021-06-15
Applicant: Joby Aero, Inc.
Inventor： Gregor Veble Mikic , JoeBen Bevirt , Robert Gulliver Lynn , Alex Stoll
IPC: H01M8/04 , B60L58/33 , B64D27/24 , B64C29/00 , H01M8/04701 , H01M8/04029 , H01M8/04119 , H01M8/04014 , B64D33/02
Abstract: A high efficiency hydrogen fuel system for an aircraft at high altitude which utilizes compressors to compress air to a sufficiently high pressure for the fuel cell. Liquid hydrogen is compressed and then utilized in heat exchangers to cool the compressed air, maintaining the air at a temperature low enough for the fuel cell. The hydrogen is also used to cool the fuel cell as it is also depressurized prior to its entry in the fuel cell cycle. A water condensation system allows for water removal from the airstream to reduce impacts to the atmosphere. The hydrogen fuel system may be used with VTOL aircraft, which may allow them to fly at higher elevations. The hydrogen fuel system may be used with other subsonic and supersonic aircraft, such as with asymmetric wing aircraft.
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公开(公告)号：US11560221B2
公开(公告)日：2023-01-24
申请号：US17389020
申请日：2021-07-29
Applicant: Joby Aero, Inc.
Inventor： JoeBen Bevirt , Alex Stoll
Abstract: An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes. The aerial vehicle uses deployment mechanisms to deploy rotor assemblies up and away from their stowed configuration locations.
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公开(公告)号：US20220204174A1
公开(公告)日：2022-06-30
申请号：US17694567
申请日：2022-03-14
Applicant: Joby Aero, Inc.
Inventor： JoeBen Bevirt , Alex Stoll
Abstract: An aerial vehicle of a box wing design adapted for vertical takeoff and landing using mounted thrust producing elements. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses one or more thrust producing elements on both of the right and the left sides. The aerial vehicle may have one or more front thrust producing elements and one or more rear thrust producing elements on both of the right and the left sides of a main vehicle body.
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公开(公告)号：US11312485B2
公开(公告)日：2022-04-26
申请号：US16833516
申请日：2020-03-28
Applicant: Joby Aero, Inc.
Inventor： JoeBen Bevirt , Alex Stoll
Abstract: An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.
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