Submersible aerial vehicle

USD1116925SActive Publication Date: 2026-03-10GUNAWARDHANA CHETANA
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Patent Information

Authority / Receiving Office
US · United States
Patent Type
Designs(United States)
Current Assignee / Owner
Filing Date
2024-06-28
Publication Date
2026-03-10

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Description

[0001] FIG. 1 is a front perspective of a submersible aerial vehicle;

[0002] FIG. 2 is a front elevation view thereof;

[0003] FIG. 3 is a rear elevation view thereof;

[0004] FIG. 4 is a right elevation view thereof;

[0005] FIG. 5 is a left elevation view thereof;

[0006] FIG. 6 is a top plan view thereof;

[0007] FIG. 7 is a bottom plan view thereof;

[0008] FIG. 8 is a front perspective view of a submersible aerial vehicle according to another embodiment;

[0009] FIG. 9 is a front elevation view of the embodiment of FIG. 8;

[0010] FIG. 10 is a rear elevation view of the embodiment of FIG. 8;

[0011] FIG. 11 is a right elevation view of the embodiment of FIG. 8;

[0012] FIG. 12 is a left elevation view of the embodiment of FIG. 8;

[0013] FIG. 13 is a top plan view of the embodiment of FIG. 8; and,

[0014] FIG. 14. is a bottom plan view of the embodiment of FIG. 8.

[0015] The broken lines are included for the purpose of illustrating environment and form no part of the claimed design.

Claims

The ornamental design of a submersible aerial vehicle as shown and described.

Citation Information

Patent Citations

  • UAV (land-based and ship-borne dual-purpose anti-submarine)

    CN308566239S

  • Foldable swan-wings aircraft

    US20110000999A1

  • Transformation method of hybrid transportation vehicle for ground and air, and hybrid transportation vehicle itself

    US20150028150A1

  • Procedure for maneuvering a hybrid aerodyne of VTOL or stol

    US20210011493A1

  • Vertical Take-Off and Landing Aircraft

    US20210078701A1