Aircraft
Patent Information
- Application Number
- US29/920426
- Authority / Receiving Office
- US · United States
- Patent Type
- Designs(United States)
- Current Assignee / Owner
- Filing Date
- 2023-12-11
- Publication Date
- 2026-02-03
- Estimated Expiration
- 2041-02-03
Smart Images

Figure USD1110923-D00000_ABST
Description
[0001] FIG. 1 is a front perspective view of an aircraft with the rotor nacelles facing forward;
[0002] FIG. 2 is a front elevational view of the aircraft in FIG. 1
[0003] FIG. 3 is a rear elevational view thereof;
[0004] FIG. 4 is a right side view thereof;
[0005] FIG. 5 is a left side view thereof;
[0006] FIG. 6 is a top view thereof;
[0007] FIG. 7 is a bottom view thereof;
[0008] FIG. 8 is a front perspective view of the aircraft in FIG. 1 with the rotor nacelles facing upward;
[0009] FIG. 9 is a front elevational view of the aircraft in FIG. 8;
[0010] FIG. 10 is a rear elevational view thereof;
[0011] FIG. 11 is a right side view thereof;
[0012] FIG. 12 is a left side view thereof;
[0013] FIG. 13 is a top view thereof; and,
[0014] FIG. 14 is a bottom view thereof.
[0015] The figures include broken, solid and dash-dot-dash lines. The areas within the solid lines and inside the dash-dot-dash lines form the claimed design. The dash-dot-dash lines illustrate an unclaimed boundary of the claimed design. The broken lines shown in the figures are included for the purpose of illustrating portions of the aircraft and form no part of the claimed design.
Claims
The ornamental design for an aircraft, substantially as shown and described.
Citation Information
Patent Citations
Outboard centrifugal force bearing with inboard blade fold axis in a folding rotor blade assembly
US10640205B2
Systems and methods for redundant control of active fuses for battery pack safety
US11710957B1
Electric power system architecture and fault tolerant VTOL aircraft using same
US12006048B2
Integrated wingtip extensions for jet transport aircraft and other types of aircraft
US20070018049A1
Frangible fasteners with flexible connectors for unmanned aircraft, and associated systems and methods
US20190003511A1