Vertical takeoff and landing aircraft

USD1053783SActive Publication Date: 2024-12-10AIBOT US IP INC
View PDF 13 Cites 0 Cited by

Patent Information

Application Number
US29/910050
Authority / Receiving Office
US · United States
Patent Type
Designs(United States)
Current Assignee / Owner
Filing Date
2023-08-15
Publication Date
2024-12-10
Estimated Expiration
2039-12-10

Smart Images

  • Figure USD1053783-D00000_ABST
    Figure USD1053783-D00000_ABST
Patent Text Reader
Need to check novelty before this filing date? Find Prior Art

Description

[0001] FIG. 1 is a front, left side perspective view of a vertical takeoff and landing aircraft showing our new design with wings of the vertical takeoff and landing aircraft in a first configuration, wherein the front, right side perspective view is a mirror image of the front, left side perspective view except for the door on a left side;

[0002] FIG. 2 is a rear, left side perspective view of the vertical takeoff and landing aircraft illustrated in FIG. 1, wherein the rear, right side perspective view is a mirror image of the rear, left side perspective view except for the door on the left side;

[0003] FIG. 3 is a front elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 1;

[0004] FIG. 4 is a rear elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 1;

[0005] FIG. 5 is a left side elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 1;

[0006] FIG. 6 is a right side elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 1;

[0007] FIG. 7 is a top elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 1;

[0008] FIG. 8 is a bottom elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 1;

[0009] FIG. 9 is a front, left side perspective view of the vertical takeoff and landing aircraft of FIGS. 1-8 with the wings of the vertical takeoff and landing aircraft in a second configuration, wherein the front, right side perspective view is a mirror image of the front, left side perspective view except for the door on the left side;

[0010] FIG. 10 is a rear, left side perspective view of the vertical takeoff and landing aircraft illustrated in FIG. 9, wherein the rear, right side perspective view is a mirror image of the rear, left side perspective view except for the door on the left side;

[0011] FIG. 11 is a front elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 9;

[0012] FIG. 12 is a rear elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 9;

[0013] FIG. 13 is a left side elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 9;

[0014] FIG. 14 is a right side elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 9;

[0015] FIG. 15 is a front, left side perspective view of the vertical takeoff and landing aircraft of FIGS. 1-14 with the wings of the vertical takeoff and landing aircraft in a transition configuration between the first configuration and the second configuration of the vertical takeoff and landing aircraft, in which the wings transition together;

[0016] FIG. 16 is a front elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 15;

[0017] FIG. 17 is a rear elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 15;

[0018] FIG. 18 is a left side elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 15;

[0019] FIG. 19 is a right side elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 15;

[0020] FIG. 20 is a front, left side perspective view of the vertical takeoff and landing aircraft of FIGS. 1-14 with the wings of the vertical takeoff and landing aircraft in a transition configuration between the first configuration and the second configuration of the vertical takeoff and landing aircraft, in which the wings transition separately;

[0021] FIG. 21 is a front elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 20;

[0022] FIG. 22 is a rear elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 20;

[0023] FIG. 23 is a left side elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 20; and,

[0024] FIG. 24 is a right side elevation view of the vertical takeoff and landing aircraft illustrated in FIG. 20.

[0025] The short-short-long broken lines are for the purpose of illustrating portions of the vertical takeoff and landing vehicle in which line impressions are caused by surface contours. The dash-dash-dash broken lines showing portions of the propellers are for the purpose of illustrating portions of the vertical takeoff and landing vehicle and forms no part of the claimed design.

Claims

The ornamental design for a vertical takeoff and landing aircraft, as shown and described.

Citation Information

Patent Citations

  • Tri-rotor aircraft capable of vertical takeoff and landing and transitioning to forward flight

    US10071801B2

  • Vertical take-off and landing vehicle with increased cruise efficiency

    US20160244158A1

  • Method of Flying an Electric Vertical Take-Off And Landing Aircraft

    US20230048620A1

  • Tiltwing multicopter with foldable and non-foldable propellers

    US9975631B1

  • Vertical take-off and landing aircraft

    USD799402S