Aircraft

USD1110923SActive Publication Date: 2026-02-03TEXTRON INNOVATIONS INC
View PDF 25 Cites 0 Cited by

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
    Figure USD1110923-D00000_ABST
Patent Text Reader
Need to check novelty before this filing date? Find Prior Art

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