Pedal for an aircraft

USD1111962SActive Publication Date: 2026-02-10AEROJONES AVIATION TECH
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Patent Information

Application Number
US29/923547
Authority / Receiving Office
US · United States
Patent Type
Designs(United States)
Current Assignee / Owner
Filing Date
2023-12-29
Publication Date
2026-02-10
Estimated Expiration
2041-02-10

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Description

[0001] FIG. 1 is a front, right-side, and top perspective view of a pedal for an aircraft showing our new design;

[0002] FIG. 2 is a rear, right-side, and bottom perspective view thereof;

[0003] FIG. 3 is a front elevational view thereof;

[0004] FIG. 4 is a left rear elevational view thereof;

[0005] FIG. 5 is a left side elevational view thereof;

[0006] FIG. 6 is a right-side elevational view thereof;

[0007] FIG. 7 is a top plan view thereof;

[0008] FIG. 8 is a bottom plan view thereof; and,

[0009] FIG. 9 is a front elevational view thereof, shown in a condition of use.

[0010] The dashed broken lines depict portions of the pedal for an aircraft that form no part of the claimed design. The dashed broken lines in FIG. 9 showing a cockpit depict environmental structure that forms no part of the claimed design.

Claims

The ornamental design for a pedal for an aircraft as shown and described.

Citation Information

Patent Citations

  • Above-the-floor rudder and brake control system

    US20170174324A1

  • Rudder control pedal assembly with linear pedal travel path

    US20190384345A1

  • Pedal cartridge

    US20240140591A1

  • Adjustable assembly for aircraft rudder, brake and nose landing gear steering control

    US4848708A

  • Brake rudder pedal system for light aircraft

    US5725184A