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公开(公告)号：US20250064213A1
公开(公告)日：2025-02-27
申请号：US18238365
申请日：2023-08-25
Applicant: Textron Aviation, Inc.
Inventor： Blake David Raybern
IPC: A47C7/50
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.
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公开(公告)号：US20240253530A1
公开(公告)日：2024-08-01
申请号：US18633079
申请日：2024-04-11
Applicant: Textron Aviation Inc.
Inventor： Blake David Raybern
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.
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公开(公告)号：US20250042553A1
公开(公告)日：2025-02-06
申请号：US18364363
申请日：2023-08-02
Applicant: Textron Aviation, Inc.
Inventor： Blake David Raybern
IPC: B64D11/06
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.
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公开(公告)号：US20240240695A1
公开(公告)日：2024-07-18
申请号：US18410832
申请日：2024-01-11
Applicant: Textron Aviation Inc.
Inventor： Blake David Raybern
IPC: F16G11/12
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.
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Patent Agency Ranking
公开(公告)号：US20250066021A1
公开(公告)日：2025-02-27
申请号：US18238347
申请日：2023-08-25
Applicant: Textron Aviation, Inc.
Inventor： Blake David Raybern
IPC: B64D11/06
Abstract: A life vest container, a method for assembling a life vest container and a method for removing a life vest from a life vest container are disclosed. In an embodiment a leg rest includes linkages of a deployment and stowage mechanism, the linkages of the deployment and stowage mechanism being connectable to a seat, a mounting fixture connected to the linkages and a container secured to the mounting fixture, the container being configured to store a life vest.
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公开(公告)号：US20250042550A1
公开(公告)日：2025-02-06
申请号：US18362815
申请日：2023-07-31
Applicant: Textron Aviation, Inc.
Inventor： Blake David Raybern
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.
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公开(公告)号：US20240239245A1
公开(公告)日：2024-07-18
申请号：US18410826
申请日：2024-01-11
Applicant: Textron Aviation Inc.
Inventor： Blake David Raybern
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.
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公开(公告)号：US20250058879A1
公开(公告)日：2025-02-20
申请号：US18790238
申请日：2024-07-31
Applicant: Textron Aviation Inc.
Inventor： Blake David Raybern
IPC: B64D11/06
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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公开(公告)号：US20240255017A1
公开(公告)日：2024-08-01
申请号：US18633073
申请日：2024-04-11
Applicant: Textron Aviation Inc.
Inventor： Blake David Raybern
CPC classification number: F16C1/106 , B60N2/929 , B64D11/064
Abstract: A cable tension triggering mechanism. It may be used with a variety of cables including those that have flexible members routed through bendable sheaths. The triggering mechanism includes a rotatable hub mounted to a swiveling plate. When the hub rotates around its pivot point, it increases the tension forces in cables thereby causing the cables to pull on locking mechanisms. The hub rotates when the plate is rotated and a stub extending from the plate presses against an end of the hub to cause the hub to rotate.
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