Vertical takeoff and landing (VTOL) vehicle

USD1115657SActive Publication Date: 2026-03-03EVE UAM LLC
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Patent Information

Authority / Receiving Office
US · United States
Patent Type
Designs(United States)
Current Assignee / Owner
Filing Date
2022-07-15
Publication Date
2026-03-03

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Description

[0001] FIGS. 1-7 show a first embodiment of our new and original design for a vertical takeoff and landing (VTOL) vehicle, wherein

[0002] FIG. 1 is a front perspective view thereof,

[0003] FIG. 2 is a front elevation view thereof;

[0004] FIG. 3 is a rear elevation view thereof;

[0005] FIG. 4 is a top plan view thereof;

[0006] FIG. 5 is a bottom plan view thereof; and

[0007] FIG. 6 is a right side elevation view thereof, and

[0008] FIG. 7 is a left side elevation view thereof; and wherein

[0009] FIGS. 8-14 show a second embodiment of our new and original design for a vertical takeoff and landing (VTOL) vehicle, wherein

[0010] FIG. 8 is a front perspective view thereof,

[0011] FIG. 9 is a front elevation view thereof;

[0012] FIG. 10 is a rear elevation view thereof;

[0013] FIG. 11 is a top plan view thereof;

[0014] FIG. 12 is a bottom plan view thereof; and

[0015] FIG. 13 is a right side elevation view thereof, and

[0016] FIG. 14 is a left side elevation view thereof; and wherein

[0017] FIGS. 15-21 show a third embodiment of our new and original design for a vertical takeoff and landing (VTOL) vehicle, wherein

[0018] FIG. 15 is a front perspective view thereof,

[0019] FIG. 16 is a front elevation view thereof;

[0020] FIG. 17 is a rear elevation view thereof;

[0021] FIG. 18 is a top plan view thereof;

[0022] FIG. 19 is a bottom plan view thereof; and

[0023] FIG. 20 is a right side elevation view thereof, and

[0024] FIG. 21 is a left side elevation view thereof; and wherein

[0025] FIGS. 22-28 show a fourth embodiment of our new and original design for an vertical takeoff and landing (VTOL) vehicle, wherein

[0026] FIG. 22 is a front perspective view thereof,

[0027] FIG. 23 is a front elevation view thereof;

[0028] FIG. 24 is a rear elevation view thereof;

[0029] FIG. 25 is a top plan view thereof;

[0030] FIG. 26 is a bottom plan view thereof; and

[0031] FIG. 27 is a right side elevation view thereof; and,

[0032] FIG. 28 is a left side elevation view thereof.

[0033] The dashed lines in the FIGURES depict elements that are in the environment of the claimed design but do not form a part of the claimed design.

Claims

The ornamental design for a “vertical takeoff and landing (VTOL) vehicle”, as shown and described.

Citation Information

Patent Citations

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    CN308764576S

  • Systems and methods for lifter motor cooling in eVTOL aircraft

    US11613350B1

  • Systems and methods for propeller blade retention

    US12122504B1

  • Fault-tolerant multi-processor systems and methods for an aircraft

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  • Systems, methods, and mechanical designs for inverters for eVTOL aircraft

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