Structure for aircraft

USD1091432SActive Publication Date: 2025-09-02THE BOEING CO

Patent Information

Application Number
US29/864158
Authority / Receiving Office
US · United States
Patent Type
Designs(United States)
Current Assignee / Owner
Filing Date
2022-05-11
Publication Date
2025-09-02
Estimated Expiration
2040-09-02

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  • Figure USD1091432-D00000_ABST
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Description

[0001] FIG. 1 is a front perspective view of a structure for aircraft;

[0002] FIG. 2 is a front elevation view of the structure for aircraft;

[0003] FIG. 3 is a rear elevation view of the structure for aircraft;

[0004] FIG. 4 is a right side view of the structure for aircraft;

[0005] FIG. 5 is a left side view of the structure for aircraft;

[0006] FIG. 6 is a top view of the structure for aircraft; and,

[0007] FIG. 7 is a bottom view of the structure for aircraft.

[0008] The broken lines shown in the drawings are for the purpose of illustrating portions of the structure for aircraft that form no part of the claimed design. The structure for aircraft is shown with a symbolic break in its length. The appearance of any portion of the article between the break lines, as well as the break lines themselves, form no part of the claimed design.

Claims

The ornamental design for an structure for aircraft as shown and described.

Citation Information

Patent Citations

  • Composite control surfaces for aircraft

    EP2842867A1

  • Wing element having a mobile element

    EP3670331A1

  • Robot-deployed assembly tool and method for installing fasteners in aircraft structures

    US20080155807A1

  • Composite structures having integrated stiffeners and method of making the same

    US20110315824A1

  • Torsion box skin stiffened with non parallel stringers

    US20120193473A1

Cited By

  • Wing for aeroplane

    USD1137086S