Vertical take-off and landing tilt-wing aircraft

USD1106027SActive Publication Date: 2025-12-16TRANSCEND AIR CORP
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Patent Information

Application Number
US29/867714
Authority / Receiving Office
US · United States
Patent Type
Designs(United States)
Current Assignee / Owner
Filing Date
2022-11-04
Publication Date
2025-12-16
Estimated Expiration
2040-12-16

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Description

[0001] FIG. 1 is a right rear top perspective view of a vertical take-off and landing tilt-wing aircraft with landing gear up;

[0002] FIG. 2 is a front view of the vertical take-off and landing tilt-wing aircraft with landing gear up;

[0003] FIG. 3 is a rear view of the vertical take-off and landing tilt-wing aircraft with landing gear up;

[0004] FIG. 4 is a right side view of the vertical take-off and landing tilt-wing aircraft with landing gear up;

[0005] FIG. 5 is a left side view of the vertical take-off and landing tilt-wing aircraft with landing gear up;

[0006] FIG. 6 is a top view of the vertical take-off and landing tilt-wing aircraft with landing gear up;

[0007] FIG. 7 is a bottom view of the vertical take-off and landing tilt-wing aircraft with landing gear up;

[0008] FIG. 8 is a left front bottom perspective view of the vertical take-off and landing tilt-wing aircraft with landing gear up;

[0009] FIG. 9 is a right rear top perspective view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear up;

[0010] FIG. 10 is a front view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear up;

[0011] FIG. 11 is a rear view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear up;

[0012] FIG. 12 is a right side view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear up;

[0013] FIG. 13 is a left side view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear up;

[0014] FIG. 14 is a top view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear up;

[0015] FIG. 15 is a bottom view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear up;

[0016] FIG. 16 is a left front bottom perspective view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear up;

[0017] FIG. 17 is right rear top perspective view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear down;

[0018] FIG. 18 is a front view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear down;

[0019] FIG. 19 is a rear view of the aircraft, shown in an alternate configuration of use, with landing gear down;

[0020] FIG. 20 is a right side view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear down;

[0021] FIG. 21 is a left side view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear down;

[0022] FIG. 22 is a top view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear down;

[0023] FIG. 23 is a bottom view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear down; and,

[0024] FIG. 24 is a left front bottom perspective view of the vertical take-off and landing tilt-wing aircraft, shown in an alternate configuration of use, with landing gear down.

[0025] The broken lines in the drawings depict portions of the vertical take-off and landing tilt-wing aircraft that form no part of the claim.

Claims

The ornamental design for a vertical take-off and landing tilt-wing aircraft, as shown and described.

Citation Information

Patent Citations

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  • Aircraft rotor assembly with segmented input shaft for electric motor stack and gearbox unit

    US12172770B2

  • VTOL aircraft for network system

    US12187409B2