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    Aircraft landing gear
    2.
    外观设计
    Aircraft landing gear 有权

    公开(公告)号：USD987546S1

    公开(公告)日：2023-05-30

    申请号：US29675588

    申请日：2019-01-03

    Applicant: Bell Helicopter Textron Inc.

    Designer： Steven Loveland ,  Allen Brittain ,  Paul Charles Griffiths

    Abstract: FIG. 1 is a bottom perspective view of the aircraft landing gear.
    FIG. 2 is a front elevational view of the landing gear of FIG. 1.
    FIG. 3 is a rear elevational view of the landing gear of FIG. 1.
    FIG. 4 is a left side elevational view of the landing gear of FIG. 1.
    FIG. 5 is a right side elevational view of the landing gear of FIG. 1.
    FIG. 6 is a top plan view of the landing gear of FIG. 1.
    FIG. 7 is a bottom plan view of the landing gear of FIG. 1; and,
    FIG. 8 is a top perspective view of the aircraft landing gear shown in an environment of use.
    The broken lines shown in FIGS. 1-7 illustrate portions of the aircraft landing gear that form no part of the claimed design; the additional broken lines shown in FIG. 8 are for purposes of illustrating environmental subject matter only and forms no part thereof. The right side not shown is understood to be a mirror image of the left side shown in FIGS. 1-8.

    Aircraft landing-gear step
    5.
    外观设计
    Aircraft landing-gear step 有权

    公开(公告)号：USD1009762S1

    公开(公告)日：2024-01-02

    申请号：US29675592

    申请日：2019-01-03

    Applicant: Bell Helicopter Textron Inc.

    Designer： Paul Charles Griffiths ,  Steven Loveland ,  Allen Brittain

    Abstract: FIG. 1 a bottom perspective view of the aircraft landing-gear step.
    FIG. 2 is a front elevational view of the landing-gear step as configured in FIG. 1.
    FIG. 3 is a rear elevational view of the landing-gear step as configured in FIG. 1.
    FIG. 4 is a left side elevational view of the landing-gear step as configured in FIG. 1.
    FIG. 5 is a right side elevational view of the landing-gear step as configured in FIG. 1.
    FIG. 6 is a top plan view of the landing-gear step as configured in FIG. 1.
    FIG. 7 is a bottom plan view of the landing-gear step as configured in FIG. 1.
    FIG. 8 is a top perspective view of the aircraft landing-gear step shown in an environment of use.
    FIG. 9 is an oblique view of the left landing-gear step, the door being configured in a closed position.
    FIG. 10 is a front elevational view of the landing-gear step as configured in FIG. 9.
    FIG. 11 is a rear elevational view of the landing-gear step as configured in FIG. 9.
    FIG. 12 is a left side elevational view of the landing-gear step as configured FIG. 9.
    FIG. 13 is a right side elevational view of the landing-gear step as configured in FIG. 9.
    FIG. 14 is a top plan view of the landing-gear step as configured in FIG. 9.
    FIG. 15 is a bottom plan view of the landing-gear step as configured in FIG. 9; and,
    FIG. 16 is an oblique view of the landing-gear step as configured in FIG. 9.
    The broken lines shown in FIGS. 1-7 and 9-15 illustrate portions of the aircraft landing-gear step that form no part of the claimed design; the additional broken lines shown in FIGS. 8 and 16 are for purposes of illustrating environmental subject matter only and forms no part thereof. The right side not shown is understood to be a mirror image of the left side shown in FIGS. 1-8 and 9-16.

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