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    Aircraft
    1.
    外观设计
    Aircraft 有权

    公开(公告)号：USD1042301S1

    公开(公告)日：2024-09-17

    申请号：US29813763

    申请日：2021-11-01

    Applicant: JetZero, Inc.

    Designer： Mark Allan Page ,  Blaine Knight Rawdon

    Abstract: FIG. 1 is a perspective view of an aircraft showing the new design;
    FIG. 2 is a front view thereof;
    FIG. 3 is a rear view thereof;
    FIG. 4 is a side view thereof;
    FIG. 5 is a second side view thereof;
    FIG. 6 is a top view thereof; and,
    FIG. 7 is a bottom view thereof.
    The broken lines in the figures show portions of the aircraft that form no part of the claimed design.

    Aircraft component with structural foam
    4.
    发明授权
    Aircraft component with structural foam 有权

    公开(公告)号：US12187425B1

    公开(公告)日：2025-01-07

    申请号：US18417424

    申请日：2024-01-19

    Applicant: JetZero, Inc.

    Inventor： Blaine Knight Rawdon

    IPC: B64C3/26 ,  B64C3/20 ,  B64C3/24

    Abstract: An aircraft component including a structural foam having a predetermined shape, an outer flange located near a first end of the structural foam, an inner flange located near a second end of the structural foam, a web skin encapsulating the inner flange and at least a portion of the structural foam wherein the structural foam is affixed to the web skin, wherein the aircraft component comprises a portion of a blended wing body aircraft (BWB), the BWB having no demarcation between a wing and a main body of the BWB.

    SYSTEMS AND METHODS FOR CONTROLLING LANDING GEAR OF AN AIRCRAFT
    7.
    发明公开
    SYSTEMS AND METHODS FOR CONTROLLING LANDING GEAR OF AN AIRCRAFT 审中-公开

    公开(公告)号：US20240002041A1

    公开(公告)日：2024-01-04

    申请号：US18210289

    申请日：2023-06-15

    Applicant: JETZERO, INC.

    Inventor： Blaine Knight Rawdon

    IPC: B64C25/26 ,  F15B1/02 ,  F15B15/18 ,  B64C25/00

    CPC classification number: B64C25/26 ,  F15B1/02 ,  F15B15/18 ,  B64C25/001 ,  F15B2211/30 ,  B64C2039/105

    Abstract: Aspects relate to systems and methods for controlling landing gear of an aircraft. An exemplary system includes a nose gear located at a nose of the aircraft, where the nose gear includes a nose piston configured to allow for displacement of a nose wheel relative the aircraft, a main gear located aft of the nose gear, where the main gear includes a main piston configured to allow for displacement of a main wheel relative the aircraft, a hydraulic circuit in fluidic communication with each of the nose piston and the main piston, and a compliant element in fluidic communication with the hydraulic circuit and configured to provide a compliant response at one or both of the nose piston and the main piston.

    Systems and methods for folding wings on an aircraft
    8.
    发明授权
    Systems and methods for folding wings on an aircraft 有权

    公开(公告)号：US12162602B2

    公开(公告)日：2024-12-10

    申请号：US18090173

    申请日：2022-12-28

    Applicant: JetZero, Inc.

    Inventor： Blaine Knight Rawdon

    IPC: B64C3/56 ,  B64C13/40 ,  B64C13/50 ,  B64C39/10

    Abstract: Aspects relate to systems and methods for folding wings on an aircraft. An exemplary system includes a blended wing body, where the blended wing body includes a main body and at least a wing, a hinge located on the at least a wing and configured to allow folding of the at least a wing, an actuation system configured to fold the at least a wing, and a controller configured to control the at least an actuation system.

    COMMERCIAL AIRCRAFT FOR LONG DISTANCE TRAVEL
    9.
    发明申请
    COMMERCIAL AIRCRAFT FOR LONG DISTANCE TRAVEL 有权

    公开(公告)号：US20240391586A1

    公开(公告)日：2024-11-28

    申请号：US18201923

    申请日：2023-05-25

    Applicant: JETZERO, INC.

    Inventor： John Charles Vassberg ,  Blaine Knight Rawdon

    IPC: B64C39/10 ,  B64D27/20 ,  B64D37/04

    Abstract: A commercial aircraft for long distance air travel, the commercial aircraft comprising, a blended wing body aircraft having a main body, a transition and wings with no clear demarcation between the wings and the main body along a leading edge of the commercial aircraft, a passenger cabin, the passenger cabin located within the main body and having a single aisle passenger capacity, at least a propulsor, the at least a propulsor attached to a portion of the main body and configured to propel the blended wing body aircraft through air, and a fuel storage having a fuel capacity, the fuel capacity configured for long range flight, wherein the commercial aircraft is configured for long-range flight.

    Long range freighter aircraft
    10.
    发明授权
    Long range freighter aircraft 有权

    公开(公告)号：US12139256B1

    公开(公告)日：2024-11-12

    申请号：US18243229

    申请日：2023-09-07

    Applicant: JETZERO, INC.

    Inventor： Mark Allan Page ,  Blaine Knight Rawdon ,  John Charles Vassberg

    IPC: B64C39/10 ,  B64C1/22 ,  B64C25/18 ,  B64D9/00 ,  B64D11/00

    Abstract: A freighter aircraft for long-distance travel, the freighter aircraft comprising a blended wing body having a main body, a transition, and wings with no clear demarcation between the wings and the main body along a leading edge of the freighter aircraft, at least a propulsor, the at least a propulsor attached to a portion of the main body and configured to propel the freighter aircraft through air, a fuel storage located within the blended wing body, the fuel storage having a fuel capacity wherein the fuel capacity is configured for long-range flight, and a cargo bay located within the main body; the cargo bay configured to have a freighter capacity, wherein freighter aircraft is a long-range aircraft, the freighter aircraft including a ton-miles per sortie between 135,000 and 450,000.

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