Swivel Locking System
    1.
    发明公开

    公开(公告)号:US20240253530A1

    公开(公告)日:2024-08-01

    申请号:US18633079

    申请日:2024-04-11

    CPC classification number: B60N2/08 B60N2/14

    Abstract: A swivel locking system for preventing swiveling of a seat frame includes a locking pin and a series of pulleys along with a housing attached to a swivel plate. The locking pin is located in the housing and is biased to be extended downwardly through an aperture in the swivel plate and retracted from the aperture via a cable. The seat frame is able to be swiveled when the locking pin is retracted from the aperture, thereby unlocking the seat frame from a bottom support.

    SWIVEL LOCKING MECHANISM FOR AIRCRAFT SEAT

    公开(公告)号:US20250108922A1

    公开(公告)日:2025-04-03

    申请号:US18480140

    申请日:2023-10-03

    Abstract: An aircraft seat includes a base frame; a seat frame rotatably connected to a top side of the base frame, wherein the seat frame is configured to rotate about a vertical axis; an internal gear plate fixedly connected to the base frame, wherein the internal gear plate includes gear teeth arranged around an opening; a guide plate fixedly connected to a bottom side of the seat frame, wherein the guide plate includes a first guide wall and a second guide wall; and a cart attached to the guide plate between the first guide wall and the second guide wall, wherein the cart includes pawl teeth configured to mesh with the gear teeth, wherein the cart is movable along the guide plate to mesh the pawl teeth with a portion of the gear teeth.

    LEG REST EXTENSION MECHANISM AND METHOD FOR OPERATING THE LEG REST EXTENSION MECHANISM

    公开(公告)号:US20250064213A1

    公开(公告)日:2025-02-27

    申请号:US18238365

    申请日:2023-08-25

    Abstract: In an embodiment a leg rest includes a mounting fixture, an extension frame and a deployment and stowage mechanism configured to deploy the leg rest from or stow the leg rest to a seat, wherein the extension frame is movably connected to the mounting fixture so that the extension frame moves relative to the mounting fixture when the deployment and stowage mechanism moves the leg rest relative to the seat.

    CABLE TENSIONING SYSTEM, MOUNTING PLATE ASSEMBLY, RETRACTION CAM, DAMPER SYSTEM AND METHOD FOR OPERATING A SYSTEM

    公开(公告)号:US20250151913A1

    公开(公告)日:2025-05-15

    申请号:US19021391

    申请日:2025-01-15

    Abstract: Embodiments provides a cable tensioning system comprising a mounting plate assembly with a mounting plate and a retraction cam mounted to the mounting plate and configured to pivot about a primary axis, wherein the retraction cam comprises a cam body and a spur body having a cable sheave groove, wherein the mounting plate assembly is fixedly secured to a mounting fixture of a leg rest of a seat, and wherein the cable sheave groove is configured to receive a cable fixed to extension frame of the leg rest, the extension frame being movable relative to the mounting fixture.

    SWIVEL INDICATING MECHANISM FOR AIRCRAFT SEAT

    公开(公告)号:US20250042553A1

    公开(公告)日:2025-02-06

    申请号:US18364363

    申请日:2023-08-02

    Abstract: An aircraft seat includes a base frame; a seat frame rotatably connected to a top side of the base frame, wherein the seat frame is configured to rotate about a vertical axis; a slot plate connected to the top side of the base frame, wherein the slot plate has a slot in a top surface of the slot plate; and a pin mount connected to a bottom side of the seat frame, wherein the pin mount has a pin that protrudes downward, wherein the pin is configured to protrude into the slot when the seat frame is rotated into a first orientation relative to the base frame.

    Device for Adjusting Tension in a Cable
    6.
    发明公开

    公开(公告)号:US20240240695A1

    公开(公告)日:2024-07-18

    申请号:US18410832

    申请日:2024-01-11

    CPC classification number: F16G11/12

    Abstract: A cable tensioner for adjusting the tension in various cables. It may be used with a variety of cables including those that have flexible members routed through bendable sheaths. The cable tensioner includes a worm gear arrangement located within a housing, where the worm gear takes the form of a worm screw engaged with a spur gear. The spur gear may then be engaged with teeth on a movable sleeve. The end of a cable is secured within the sleeve and the tension in the cable can be adjusted by moving the sleeve via the worm gear.

    Seat Central Control Arm with Tensioning

    公开(公告)号:US20250042550A1

    公开(公告)日:2025-02-06

    申请号:US18362815

    申请日:2023-07-31

    Abstract: A system and method for a central control arm with tensioning for a lateral tracking and swivel system in a seat are provided. The control system includes a central control arm body, where the central control arm body has one or more attachment points and a cable interface feature, one or more paddle arms, and one or more adjustment mechanisms attached to the central control arm body, where each adjustment mechanism of the one or more adjustment mechanisms is aligned longitudinally along the central control arm body with a respective attachment point of the one or more attachment points, where each adjustment mechanism of the one or more adjustment mechanisms has a set screw that impinges on a face of a paddle arm of the one or more paddle arms.

    Seat Positioning System
    9.
    发明公开

    公开(公告)号:US20240239245A1

    公开(公告)日:2024-07-18

    申请号:US18410826

    申请日:2024-01-11

    CPC classification number: B60N2/07 B60N2/0812 B60N2/0881

    Abstract: A system for positioning a seat and locking it into a desired position. The system may include a seat mounted to a plurality of movable track members that allow an occupant to position a seat. The track members may be locked in place with one or more spring biased locking mechanisms that selectively engage the track members to keep the seat fixed in a desired position. The locking members may be engaged or disengaged using a series of cables. In one embodiment, a master cable is run to a handle on the side of the seat, which can be manipulated by an occupant to selectively engage and disengage the locking mechanisms.

    Mechanical Logic-Gate Pivot Tube
    10.
    发明申请

    公开(公告)号:US20250058879A1

    公开(公告)日:2025-02-20

    申请号:US18790238

    申请日:2024-07-31

    Abstract: A mechanical logic gate system for an aircraft seat which includes a flywheel operatively connected to a pivot tube and control cables. The control cables attach to swivel locking and tracking mechanisms which enable swiveling and tracking of the aircraft seat. Spring pin plungers are configured to extend into the flywheel for locking it in place. When both spring pin plungers are retracted from the flywheel via control cables, the aircraft seat is disabled from swiveling.

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