Vertical takeoff and landing aircraft
Patent Information
- Application Number
- US29/910049
- 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 USD1053782-D00000_ABST
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 FIG. 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
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Vertical take-off and landing vehicle with increased cruise efficiency
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Method of Flying an Electric Vertical Take-Off And Landing Aircraft
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Tiltwing multicopter with foldable and non-foldable propellers
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Vertical take-off and landing aircraft
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