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    Rubber mat for avionics box
    1.
    外观设计
    Rubber mat for avionics box 有权

    公开(公告)号：USD1013610S1

    公开(公告)日：2024-02-06

    申请号：US29811357

    申请日：2021-10-13

    Applicant: Textron Aviation Inc.

    Designer： Jason Michael Decker ,  Rebecca Rae Groninga ,  Michael Scott Robinson ,  Sidney Aloysius Mohr

    Abstract: FIG. 1 is a perspective view of the rubber mat for avionics box showing our new design;
    FIG. 2 is a front view of the rubber mat for avionics box of FIG. 1;
    FIG. 3 is a back view of the rubber mat for avionics box of FIG. 1;
    FIG. 4 is a left view of the rubber mat for avionics box of FIG. 1;
    FIG. 5 is a right view of the rubber mat for avionics box of FIG. 1;
    FIG. 6 is a top view of the rubber mat for avionics box of FIG. 1;
    FIG. 7 is a bottom view of the rubber mat for avionics box of FIG. 1; and,
    FIG. 8 is a perspective view of the rubber mat for avionics box shown in an alternate environment of use.
    In FIGS. 1-8, broken lines indicate environmental structure that forms no part of the claimed design.

    MODULAR REFRESHMENT CENTER
    2.
    发明申请
    MODULAR REFRESHMENT CENTER 审中-公开

    公开(公告)号：US20180118349A1

    公开(公告)日：2018-05-03

    申请号：US15795707

    申请日：2017-10-27

    Applicant: Textron Aviation Inc.

    Inventor： Frank Joseph Rowe ,  Michael Scott Robinson ,  Dave Wayne Davis ,  JoAnn Kimbell ,  Stephen Fagan

    IPC: B64D11/04 ,  A47B77/04 ,  A47B95/00 ,  A47B61/02

    CPC classification number: B64D11/04 ,  A47B61/02 ,  A47B77/04 ,  A47B95/008

    Abstract: A substructure in an aircraft cabin includes a drawer-insert accepting portion that defines multiple racks. Each rack may receive an exchangeable drawer insert. A module-accepting portion of the substructure defines an opening that includes a supporting surface, a back wall which extends upward and outward, and a lateral side wall. A module is provided for optionally installing in the module-accepting portion. The module has concealed areas upon installing that include: (i) a base adapted to rest on the supporting surface, (ii) a side wall adapted to abut the lateral side wall, and (iii) a rear wall adapted to abut the back wall. The module also has exposed surfaces upon installing that are adapted to match an existing profile of the drawer-insert accepting portion. The module-accepting portion is configured for stowing cargo in a first mode and for receiving the module in a second mode.

    Modular refreshment center
    6.
    发明授权
    Modular refreshment center 有权

    公开(公告)号：US11273915B2

    公开(公告)日：2022-03-15

    申请号：US15795707

    申请日：2017-10-27

    Applicant: Textron Aviation Inc.

    Inventor： Frank Joseph Rowe ,  Michael Scott Robinson ,  David Wayne Davis ,  JoAnn Kimbell ,  Stephen Fagan

    IPC: B64D11/04 ,  A47B61/02 ,  A47B77/04 ,  A47B95/00

    Abstract: A substructure in an aircraft cabin includes a drawer-insert accepting portion that defines multiple racks. Each rack may receive an exchangeable drawer insert. A module-accepting portion of the substructure defines an opening that includes a supporting surface, a back wall which extends upward and outward, and a lateral side wall. A module is provided for optionally installing in the module-accepting portion. The module has concealed areas upon installing that include: (i) a base adapted to rest on the supporting surface, (ii) a side wall adapted to abut the lateral side wall, and (iii) a rear wall adapted to abut the back wall. The module also has exposed surfaces upon installing that are adapted to match an existing profile of the drawer-insert accepting portion. The module-accepting portion is configured for stowing cargo in a first mode and for receiving the module in a second mode.

    Adaptable skylight
    7.
    发明授权
    Adaptable skylight 有权

    公开(公告)号：US10349489B2

    公开(公告)日：2019-07-09

    申请号：US15795786

    申请日：2017-10-27

    Applicant: Textron Aviation Inc.

    Inventor： Michael Scott Robinson ,  Frank Joseph Rowe ,  Todd Alan Thisius

    IPC: H05B37/02 ,  B64C1/14 ,  B64D11/00 ,  F21V14/00 ,  G02F1/133 ,  G02F1/1334 ,  F21V23/00 ,  E04D13/03 ,  F21S10/02 ,  F21Y115/10 ,  F21S11/00 ,  F21W121/00 ,  F21Y113/13

    Abstract: An adaptable skylight includes a frame facing an interior of an enclosure having an opening for allowing light to pass. An opacity-control pane adjacent the opening allows a variable amount of light to pass, and an artificial light source illuminates the frame. An aircraft skylight assembly includes a variable pane, an artificial light source for illuminating portions of the skylight assembly, and a controller configured for adjusting an amount of external light transmission through the variable pane and an amount of artificial light illumination. An internal ambiance lighting system includes the adaptable skylight having a dimmable pane for providing transmission of a variable amount of external light into an enclosure, the artificial light illuminates the frame surrounding the adaptable skylight, and the controller automatically adjusts external light transmission through the adaptable skylight and illumination of the frame based on a lighting preference.

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