Aero dynamic structure with fastener arrangement

USD1058473SActive Publication Date: 2025-01-21THE BOEING CO
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Patent Information

Application Number
US29/864157
Authority / Receiving Office
US · United States
Patent Type
Designs(United States)
Current Assignee / Owner
Filing Date
2022-05-11
Publication Date
2025-01-21
Estimated Expiration
2040-01-21

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Description

[0001] FIG. 1 is a front perspective view of aero dynamic structure with fastener arrangement;

[0002] FIG. 2 is a front elevation view of the aero dynamic structure with fastener arrangement;

[0003] FIG. 3 is a rear elevation view;

[0004] FIG. 4 is a right side view of the aero dynamic structure with fastener arrangement;

[0005] FIG. 5 is a left side view of the aero dynamic structure with fastener arrangement; and

[0006] FIG. 6 is a top view of the aero dynamic structure with fastener arrangement; and,

[0007] FIG. 7 is a bottom view of the aero dynamic structure with fastener arrangement.

[0008] The broken lines illustrate portions of the aero dynamic structure with fastener arrangement that form no part of the claimed design. The broken away symbols in the drawings indicate the appearance of any portion of the article between the break lines forms no part of the claimed design.

Claims

The ornamental design for aero dynamic structure with fastener arrangement as shown and described.

Citation Information

Patent Citations

  • Composite control surfaces for aircraft

    EP2842867A1

  • Wing element having a mobile element

    EP3670331A1

  • Torsion box skin stiffened with non parallel stringers

    US20120193473A1

  • Isogrid stiffening elements

    US20180117873A1

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

    US20080155807A1

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