公开(公告)号：US20250058878A1

公开(公告)日：2025-02-20

申请号：US18449124

申请日：2023-08-14

Applicant: Textron Aviation, Inc.

Inventor： Matthew William Reese ,  Jason Michael Decker ,  Adam Ryan Payton

IPC: B64D11/06 ,  B64D11/00

Abstract: A system for storage includes a drawer configured to open with a push, a drawer base, and a seat. A drawer face of the drawer is free of a handle. The drawer opens in a first direction along two or more slides. The drawer base is under the drawer, the drawer being coupled to the drawer base. The seat is over the drawer. The seat faces perpendicular to the first direction.

公开(公告)号：US20250074599A1

公开(公告)日：2025-03-06

申请号：US18461927

申请日：2023-09-06

Applicant: Textron Aviation, Inc.

Inventor： Matthew William Reese

IPC: B64D11/06

Abstract: A passenger seat comprising a first armrest assembly; a second armrest assembly, the second armrest assembly comprising: a side panel comprising an armrest portion and a side portion, the side panel comprising a first magnet secured on an interior side of the side panel; an interior compartment disposed within the side panel; and an access panel in a removably attached position to the side panel, the access panel comprising a second magnet secured on an interior side of the access panel, the first magnet being aligned with the second magnet when the access panel is in the removably attached position.

公开(公告)号：US20250033776A1

公开(公告)日：2025-01-30

申请号：US18360547

申请日：2023-07-27

Applicant: Textron Aviation, Inc.

Inventor： Joshua Lawrence Bell ,  Matthew William Reese

IPC: B64D11/06 ,  B64C19/00

Abstract: An embodiment seat control system includes a control board having a processing unit, wherein the processing unit has one or more processors and one or more memories, and a mainboard. The processing unit is communicatively attached to the mainboard and mainboard has a plurality of receptacles and mainboard includes one or more communication buses between at least one of the plurality of receptacles and the processing unit. The system further has one or more system modules, where each module of the one or more system modules is configured to be connected to a respective receptacle of the plurality of receptacles, where each module of the one or more system modules implements a functional capability of a seat, and where the one or more system modules are nondestructively removeable from the mainboard.

公开(公告)号：USD1044336S1

公开(公告)日：2024-10-01

申请号：US29812503

申请日：2021-10-21

Applicant: Textron Aviation Inc.

Designer： Barry John Ward ,  Matthew William Reese ,  Jason Michael Decker ,  Matthew Allen Paul ,  Wallis Augusta Mead

Abstract: FIG. 1 is a perspective view of a fold over seat mat showing our new design in a closed configuration;
FIG. 2 is a front view of the fold over seat mat of FIG. 1 in a closed configuration;
FIG. 3 is a right view of the fold over seat mat of FIG. 1 in a closed configuration;
FIG. 4 is a left view of the fold over seat mat of FIG. 1 in a closed configuration;
FIG. 5 is a top view of the fold over seat mat of FIG. 1 in a closed configuration;
FIG. 6 is a perspective view of the fold over seat mat of FIG. 1 in an open configuration;
FIG. 7 is a front view of the fold over seat mat of FIG. 1 in an open configuration;
FIG. 8 is a right view of the fold over seat mat of FIG. 1 in an open configuration;
FIG. 9 is a left view of the fold over seat mat of FIG. 1 in an open configuration; and,
FIG. 10 is a top view of the fold over seat mat of FIG. 1 in an open configuration.
In FIGS. 1-10, broken lines indicate environmental structure that forms no part of the claimed design.

公开(公告)号：USD1069434S1

公开(公告)日：2025-04-08

申请号：US29910693

申请日：2023-08-23

Applicant: Textron Aviation Inc.

Designer： Allan Dale Schrag ,  Torin Alexander De Joy ,  Lydia P. Pierce ,  Matthew William Reese ,  Adam Brickman ,  John Hladik

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.

公开(公告)号：USD1043189S1

公开(公告)日：2024-09-24

申请号：US29812252

申请日：2021-10-20

Applicant: Textron Aviation Inc.

Designer： Jason Michael Decker ,  Matthew William Reese ,  Barry John Ward ,  Matthew Allen Paul ,  Wallis Augusta Mead

Abstract: FIG. 1 is a perspective view of a fold over seat matting set showing our new design in an closed configuration;
FIG. 2 is a front view of the fold over seat matting set of FIG. 1 in an open configuration;
FIG. 3 is a left view of the fold over seat matting set of FIG. 1 in an open configuration;
FIG. 4 is a right view of the fold over seat matting set of FIG. 1 in an open configuration;
FIG. 5 is a top view of the fold over seat matting set of FIG. 1 in an open configuration;
FIG. 6 is a perspective view of the fold over seat matting set of FIG. 1 in a closed configuration;
FIG. 7 is a front view of the fold over seat matting set of FIG. 1 in a closed configuration;
FIG. 8 is a left view of the fold over seat matting set of FIG. 1 in a closed configuration;
FIG. 9 is a right view of the fold over seat matting set of FIG. 1 in a closed configuration; and,
FIG. 10 is a top view of the fold over seat matting set of FIG. 1 in a closed configuration.
In FIGS. 1-10, broken lines indicate environmental structure that forms no part of the claimed design.

公开(公告)号：US20230115357A1

公开(公告)日：2023-04-13

申请号：US18045553

申请日：2022-10-11

Applicant: Textron Aviation Inc.

Inventor： Barry John Ward ,  Matthew William Reese ,  Jason Michael Decker ,  Matthew Allen Paul

IPC: B64D11/06

Abstract: A foldable vehicle seat includes a seat base having a seat support frame, a seat back extending from the seat base, and a foldable section connected to the seat back. The folded section has a folded and unfolded configuration, and comprises a hinge mechanism with a pivot point, a first support, a second support, and a top surface configured to store luggage thereon. The first support is connected to the hinge mechanism and is rotatable about the pivot point. Likewise, the second support is connected to the hinge mechanism and is rotatable about the pivot point. The first and second supports contain first and second magnets, respectively, which are configured to retain the foldable section in the folded configuration.