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    Multi-function credenza
    1.
    发明授权
    Multi-function credenza 有权

    公开(公告)号：US11066173B2

    公开(公告)日：2021-07-20

    申请号：US15797769

    申请日：2017-10-30

    Applicant: Textron Aviation Inc.

    Inventor： David Wayne Davis ,  Frank Joseph Rowe ,  Jason Michael Decker ,  Matthew Robert Harrell

    IPC: B64D11/06 ,  A47B83/00 ,  A47B85/04 ,  A47B85/08 ,  A47B1/05 ,  A47B13/02

    Abstract: A multi-function credenza includes at least one cabinet with a first top surface and a seat adjacent the cabinet. The seat has a convertible seat back for converting to a second top surface adjacent to the first top surface when the seat is stowed. A multi-function credenza in an aircraft cabin includes a first cabinet that has a first inboard panel and a first top surface, a second cabinet that has a second inboard panel and a second top surface, and a stowable seat located between the first cabinet and the second cabinet. A stowable seat includes a seat back that has a first side adapted for seating in a first mode and a second side adapted as a working surface in a second mode. The seat back articulates between the first mode and the second mode for deploying and stowing the seat, respectively.

    MODULAR REFRESHMENT CENTER
    4.
    发明申请
    MODULAR REFRESHMENT CENTER 有权

    公开(公告)号：US20220267007A1

    公开(公告)日：2022-08-25

    申请号：US17668215

    申请日：2022-02-09

    Applicant: Textron Aviation Inc.

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

    IPC: B64D11/04

    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 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. The module may include a locking assembly.

    ADJUSTABLE INTERIOR MOCKUP
    5.
    发明申请
    ADJUSTABLE INTERIOR MOCKUP 审中-公开

    公开(公告)号：US20180334266A1

    公开(公告)日：2018-11-22

    申请号：US16048947

    申请日：2018-07-30

    Applicant: Textron Aviation Inc.

    Inventor： David Wayne Davis ,  Todd Alan Thisius ,  Chris Trask ,  Chris Pinkerton ,  Alec Charles Willford

    IPC: B64F5/00 ,  G09B25/02

    CPC classification number: B64F5/00 ,  B64F5/10 ,  G09B25/02

    Abstract: A system and method for simulating a structure is disclosed. An adjustable interior mockup for simulating a structure has a base with a first elongated side and a second elongated side, the first elongated side being nonadjacent the second elongated side; and an adjustable frame secured to the base. The adjustable frame includes a plurality of girder members secured along the first and second elongated sides to form an arc; a plurality of brackets; a plurality of arms having a latch attached to one end; and a sheet of fabric. The girders are securely fastened along the first elongated side of the base at predetermined intervals; the brackets are secured to the girders; the arms are received by the brackets and adjustably anchored to the girders via a fastener; and the latches engage the sheet of fabric, thus pulling the fabric into a shape that resembles the structure.

    Electronically Actuated Seat Recline Release
    7.
    发明申请
    Electronically Actuated Seat Recline Release 有权

    公开(公告)号：US20250042552A1

    公开(公告)日：2025-02-06

    申请号：US18362538

    申请日：2023-07-31

    Applicant: Textron Aviation, Inc.

    Inventor： Matthew William Reese ,  David Wayne Davis ,  Joshua Lawrence Bell

    IPC: B64D11/06

    Abstract: A seat release system and device, the system including an interface assembly that provides actuation signaling, an actuation device that communicatively provides mechanical motion in response to the actuation signaling, a cable connected to the actuation device, and a recline release cylinder having a gas release button and a release lever at a first end, and having a cylinder piston arm in the recline release cylinder at a second end. The release lever is attached to a second end of the cable where the cable moves the release lever in response to the mechanical motion of the actuation device. The gas release button vents the recline release cylinder to atmosphere in response to being depressed as a result of the cable moving the release lever. The cylinder piston arm may move in the recline release cylinder in response to the gas release button being depressed.

    Side ledge for aircraft
    9.
    外观设计
    Side ledge for aircraft 有权

    公开(公告)号：USD1022845S1

    公开(公告)日：2024-04-16

    申请号：US29811182

    申请日：2021-10-12

    Applicant: Textron Aviation Inc.

    Designer： Frank Joseph Rowe ,  Matthew R. Harrell ,  David Wayne Davis ,  Sergio R. Martinez ,  Brent Todd Coppock

    Abstract: FIG. 1 is a perspective view of a side ledge for aircraft showing our new design;
    FIG. 2 is a front view of the side ledge for aircraft of FIG. 1;
    FIG. 3 is a left view of the side ledge for aircraft of FIG. 1;
    FIG. 4 is a right view of the side ledge for aircraft of FIG. 1; and,
    FIG. 5 is a top view of the side ledge for aircraft of FIG. 1.
    In FIGS. 1-5, the broken lines shown in the drawings depict portions of the side ledge for aircraft that form no part of the claimed design.

    Adjustable interior mockup
    10.
    发明授权
    Adjustable interior mockup 有权

    公开(公告)号：US11014690B2

    公开(公告)日：2021-05-25

    申请号：US16048947

    申请日：2018-07-30

    Applicant: Textron Aviation Inc.

    Inventor： David Wayne Davis ,  Todd Alan Thisius ,  Chris Trask ,  Chris Pinkerton ,  Alec Charles Willford

    IPC: B64F5/00 ,  G09B25/02 ,  B64F5/10

    Abstract: A system and method for simulating a structure is disclosed. An adjustable interior mockup for simulating a structure has a base with a first elongated side and a second elongated side, the first elongated side being nonadjacent the second elongated side; and an adjustable frame secured to the base. The adjustable frame includes a plurality of girder members secured along the first and second elongated sides to form an arc; a plurality of brackets; a plurality of arms having a latch attached to one end; and a sheet of fabric. The girders are securely fastened along the first elongated side of the base at predetermined intervals; the brackets are secured to the girders; the arms are received by the brackets and adjustably anchored to the girders via a fastener; and the latches engage the sheet of fabric, thus pulling the fabric into a shape that resembles the structure.

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