Vertical take-off and landing tilt-wing aircraft
Patent Information
- Application Number
- US29/871877
- Authority / Receiving Office
- US · United States
- Patent Type
- Designs(United States)
- Current Assignee / Owner
- Filing Date
- 2023-03-01
- Publication Date
- 2024-12-24
- Estimated Expiration
- 2039-12-24
Smart Images

Figure USD1054959-D00000_ABST
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 left front bottom perspective view of the vertical take-off and landing tilt-wing aircraft with landing gear up;
[0003] FIG. 3 is a front view of the vertical take-off and landing tilt-wing aircraft with landing gear up;
[0004] FIG. 4 is a rear view of the vertical take-off and landing tilt-wing aircraft with landing gear up;
[0005] FIG. 5 is a right side view of the vertical take-off and landing tilt-wing aircraft with landing gear up;
[0006] FIG. 6 is a left side view of the vertical take-off and landing tilt-wing aircraft with landing gear up;
[0007] FIG. 7 is a top view of the vertical take-off and landing tilt-wing aircraft with landing gear up;
[0008] FIG. 8 is a bottom 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 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;
[0011] FIG. 11 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;
[0012] FIG. 12 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;
[0013] FIG. 13 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;
[0014] FIG. 14 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;
[0015] FIG. 15 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;
[0016] FIG. 16 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;
[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 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.
[0019] FIG. 19 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;
[0020] FIG. 20 is a rear 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 right 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 left side 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 top 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 bottom 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
Vertical take-off and landing (VTOL) tilt-wing passenger aircraft
US11077937B1
Electric power system architecture and fault tolerant VTOL aircraft using same
US12006048B2
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US20130099065A1
Control method for preventing differences between rotor tilt angles in a fly-by-wire tiltrotor aircraft
US20190225322A1
Tilt Rotor Aircraft Noise Reduction
US20230009101A1
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