VERTICAL ADJUSTMENT SYSTEM FOR AN AIRCRAFT SEAT

    公开(公告)号:US20220340284A1

    公开(公告)日:2022-10-27

    申请号:US17338037

    申请日:2021-06-03

    IPC分类号: B64D11/06

    摘要: A vertical adjustment system for an aircraft seat is disclosed. The vertical adjustment system may include an actuation assembly. The actuation assembly may include an actuator configured to provide a vertical height adjustment for the aircraft seat. The actuation assembly may include a release mechanism configured to couple to a rotatory portion of the swivel plate. The actuation assembly may include a plurality of vertical stabilizer rods coupled to a portion of the tracking plate. The actuation assembly may include a pillow block assembly. The pillow block assembly may include a plurality of pillow blocks coupled to a portion of the swivel plate. The pillow block assembly may include a plurality of rollers coupled to a portion of the plurality of pillow blocks. The plurality of rollers may be configured to provide stability along the vertical stabilizer rods when the actuator provides the vertical height adjustment.

    Interlinked plinth attachment system for aircraft seats

    公开(公告)号:US11548645B2

    公开(公告)日:2023-01-10

    申请号:US16545447

    申请日:2019-08-20

    发明人: Michael L. Oleson

    IPC分类号: B64D11/06 A47C7/00 A47C3/18

    摘要: A plinth attachment system for attachment to at least one track includes: a first plate having a first side configured for mounting to a longitudinally extending track, and a first mounting feature for mounting a first structure; and a second plate having a first side configured for mounting to the track, and a second mounting feature for mounting a second structure. When mounted on the track, at least one interlinking feature of the first side of the first plate and at least one interlinking feature of the first side of the second plate interlock at the track, and, the first mounting feature and second mounting feature are aligned at essentially equivalent longitudinal positions.

    Three-place berthing aircraft divan

    公开(公告)号:US11059589B2

    公开(公告)日:2021-07-13

    申请号:US16054036

    申请日:2018-08-03

    IPC分类号: B64D11/06 B64D11/00

    摘要: A three-place aircraft divan configured to be installed side-facing in an aircraft and track between an upright sitting position and a berth position. Seat bottom and backrest portions of the divan are movably supported on a static frame and track together. The divan includes inflatable passenger restraints at each seat place and a leg flail prevention device at one end of the frame triggered to actuate in response to an event sensed by a mechanical crash sensor. The inboard leg arrangement of the divan accommodates the installation of two containers for containing high-capacity life rafts under the seat bottom frame, among other equipment.

    Aircraft seat with occupant weight sensing mechanism to adjust tilt-recline force

    公开(公告)号:US10259584B2

    公开(公告)日:2019-04-16

    申请号:US15337912

    申请日:2016-10-28

    摘要: In a preferred embodiment, a tilt-recline force adjusting apparatus for an aircraft passenger seat configured for a tilt-recline positioning includes a first spring having a first axis to urge a seat back into an upright position, the first spring arranged to compress as the seat is manually reclined, a helper spring having a second axis parallel to the first axis, the helper spring arranged to assist or counteract the first spring, an adjustment mechanism coupled to the helper spring to increase or decrease a force exerted by the helper spring to assist or counteract the first spring, and a weight sensing mechanism coupled to the adjustment mechanism and operable to actuate the adjustment mechanism in direct proportion to a weight of a seated passenger, whereby the force exerted on the aircraft seat to urge the seat back into an upright position is greater for a heavier seated passenger.

    SELF SUPPORTING BERTHING PLATFORM SYSTEM FOR AIRCRAFT SEATS

    公开(公告)号:US20240017834A1

    公开(公告)日:2024-01-18

    申请号:US18072140

    申请日:2022-11-30

    IPC分类号: B64D11/06

    CPC分类号: B64D11/0648

    摘要: A self-supporting berthing platform system is disclosed. The system may include a plurality of articulated panels including a first panel coupled to a second panel via at least one hinge assembly. The plurality of articulated panels may be configured to pivot between at least one of an upright position and a berth position. The system may include a hinge reinforcement assembly including a first reinforcement member and a second reinforcement member. The hinge reinforcement assembly may further include a flange. The system may include a panel reinforcement assembly including a first panel reinforcement member coupled to the first panel and a portion of at least one seatback frame and a second panel reinforcement member sub-assembly coupled to the second panel. The second panel reinforcement member sub-assembly may include at least one panel leg and at least one support block.

    INTERLINKED PLINTH ATTACHMENT SYSTEM FOR AIRCRAFT SEATS

    公开(公告)号:US20200062405A1

    公开(公告)日:2020-02-27

    申请号:US16545447

    申请日:2019-08-20

    发明人: Michael L. Oleson

    IPC分类号: B64D11/06 A47C7/00 A47C3/18

    摘要: A plinth attachment system for attachment to at least one track includes: a first plate having a first side configured for mounting to a longitudinally extending track, and a first mounting feature for mounting a first structure; and a second plate having a first side configured for mounting to the track, and a second mounting feature for mounting a second structure. When mounted on the track, at least one interlinking feature of the first side of the first plate and at least one interlinking feature of the first side of the second plate interlock at the track, and, the first mounting feature and second mounting feature are aligned at essentially equivalent longitudinal positions.

    Modular aircraft floor track adapter system
    8.
    发明授权
    Modular aircraft floor track adapter system 有权
    模块化飞机地板轨道适配器系统

    公开(公告)号:US09481467B2

    公开(公告)日:2016-11-01

    申请号:US14519756

    申请日:2014-10-21

    发明人: Michael L. Oleson

    IPC分类号: B64D11/06 B64C1/20 B64C1/18

    CPC分类号: B64D11/0696 B64C1/18 B64C1/20

    摘要: A modular floor track adapter system including a plurality of adapter plates laterally sized to span existing aircraft floor beams, each of the plurality of adapter plates shaped to interlock with an adjacent adapter plate in a side-by-side arrangement and including a series of holes for attaching seat track crown sections and panel attachment tabs for securing an aircraft floor panel thereto.

    摘要翻译: 一种模块化地板轨道适配器系统,包括横向尺寸以跨越现有飞行器地板梁的多个适配器板,所述多个适配器板中的每一个成形为并排布置并与相邻适配器板互锁,并且包括一系列孔 用于附接座椅轨道冠部分和用于将飞机底板固定到其上的面板附接突片。

    LEG RESTRAINT DEVICE FOR SIDE-FACING SEATED VEHICLE OCCUPANTS
    9.
    发明申请
    LEG RESTRAINT DEVICE FOR SIDE-FACING SEATED VEHICLE OCCUPANTS 有权
    用于侧面覆盖车辆职业的LEG限制装置

    公开(公告)号:US20150166185A1

    公开(公告)日:2015-06-18

    申请号:US14628431

    申请日:2015-02-23

    IPC分类号: B64D11/06 B64D25/04 B60N2/427

    摘要: A lower leg restraint for a side-facing passenger seat including a restraint panel configured to deploy from a first position proximate a seat to a second position forward of the seat in response to an abrupt deceleration event, an actuator arranged to push the panel from the first position to the second position, and a sensor and trigger assembly configured to signal the actuator to fire in response to the abrupt deceleration event. A side-facing aircraft passenger seat having a deployable lower leg restraint.

    摘要翻译: 一种面向侧面的乘客座椅的小腿部保护装置,包括一个约束面板,其构造成响应于突然的减速事件从座椅的靠近座椅的第一位置向第二位置展开;致动器,被布置成将面板从 第一位置到第二位置,以及传感器和触发器组件,其被配置为响应于突然减速事件而使致动器发出信号。 面向侧面的飞机乘客座椅具有可部署的小腿保护装置。

    Self supporting berthing platform system for aircraft seats

    公开(公告)号:US12116135B2

    公开(公告)日:2024-10-15

    申请号:US18072140

    申请日:2022-11-30

    IPC分类号: B64D11/06

    CPC分类号: B64D11/0641

    摘要: A self-supporting berthing platform system is disclosed. The system may include a plurality of articulated panels including a first panel coupled to a second panel via at least one hinge assembly. The plurality of articulated panels may be configured to pivot between at least one of an upright position and a berth position. The system may include a hinge reinforcement assembly including a first reinforcement member and a second reinforcement member. The hinge reinforcement assembly may further include a flange. The system may include a panel reinforcement assembly including a first panel reinforcement member coupled to the first panel and a portion of at least one seatback frame and a second panel reinforcement member sub-assembly coupled to the second panel. The second panel reinforcement member sub-assembly may include at least one panel leg and at least one support block.