SYSTEM AND APPARATUS FOR DECOUPLING AN ELECTRO-MECHANICAL ACTUATOR FROM A PORTION OF A LINKAGE
    91.
    发明申请
    SYSTEM AND APPARATUS FOR DECOUPLING AN ELECTRO-MECHANICAL ACTUATOR FROM A PORTION OF A LINKAGE 有权
    用于从连接部分解除机电致动器的系统和装置

    公开(公告)号:US20160052424A1

    公开(公告)日:2016-02-25

    申请号:US14467811

    申请日:2014-08-25

    IPC分类号: B60N2/04 B60N2/02 F16H21/40

    摘要: In various embodiments, a drive system with a motor rotary actuator driven linkage and an override system is provided. The override system may be a manually actuated override system that, in response to a power loss or outage, is configured to disengage one or more links of drive system 100 from the electric motor rotary actuator, allowing the disengaged link to be moved and/or repositioned. Moreover, drive system 100 and, more specifically, the override system may be configured to restore normal operation to the disengaged link in response to power being restored (i.e., by reengaging the link).

    摘要翻译: 在各种实施例中,提供具有电动机旋转致动器驱动联动装置和超控系统的驱动系统。 超控系统可以是手动启动的超控系统,其响应于功率损耗或停电被配置为将驱动系统100的一个或多个链路与电动机旋转致动器分离,允许分离链路被移动和/或 重新定位 此外,驱动系统100,更具体地,覆盖系统可以被配置为响应于恢复的功率(即,通过重新连接链路)来恢复对分离链路的正常操作。

    DEFORMABLE STOW BOX DOOR HINGE
    92.
    发明申请
    DEFORMABLE STOW BOX DOOR HINGE 有权
    可变轨道箱门铰链

    公开(公告)号:US20150337576A1

    公开(公告)日:2015-11-26

    申请号:US14282432

    申请日:2014-05-20

    IPC分类号: E05D7/00

    摘要: As described herein, a hinge system may comprise one or more a guide wire hinges. In general, the guide wire hinges may be unitary members having a generally constant diameter. A pair of guide wire hinges may be utilized to hingeably couple a stow box door to the stow box housing. The hinge system may be configured to be deformable in response to experiencing a warping.

    摘要翻译: 如本文所述,铰链系统可以包括一个或多个导丝铰链。 通常,导丝铰链可以是具有大致恒定直径的整体构件。 可以使用一对导丝铰链将收起箱门铰接地联接到收起箱壳体上。 铰链系统可以被配置为响应于经历翘曲而变​​形。

    SYSTEMS AND METHODS FOR RECLINING SEATS
    93.
    发明申请
    SYSTEMS AND METHODS FOR RECLINING SEATS 有权
    系统和方法

    公开(公告)号:US20150320216A1

    公开(公告)日:2015-11-12

    申请号:US14273984

    申请日:2014-05-09

    IPC分类号: A47C1/032 B64D11/06 A47C3/00

    摘要: Systems and methods are disclosed herein for reclining seats. A seat may have a seat back, a seat bottom, and a spine within the seat back and seat bottom. The seat bottom may be coupled to a base. The seat bottom may translate relative to the base. The seat may include a guide ramp coupled to the base. A portion of the spine may be located within the guide ramp. In response to translation of the seat bottom, the guide ramp may apply a torque on the spine, causing the seat back to recline.

    摘要翻译: 本文公开了用于倾斜座椅的系统和方法。 座椅可以在座椅靠背和座椅底部具有座椅靠背,座椅底部和脊柱。 座椅底部可以联接到基座。 座椅底部可以相对于底座平移。 座椅可以包括连接到基座的引导斜面。 脊柱的一部分可以位于引导斜坡内。 响应于座椅底部的平移,导向斜面可以在脊柱上施加扭矩,导致座椅靠背倾斜。

    Cabin attendant aircraft seat leg rest with foot support

    公开(公告)号:US12043390B2

    公开(公告)日:2024-07-23

    申请号:US17379515

    申请日:2021-07-19

    发明人: Kyler J. Marutzky

    IPC分类号: B64C11/06 B64D11/06

    摘要: A leg rest assembly is disclosed. The assembly may include a support sub-assembly configured to provide at least one of leg support or foot support. The support sub-assembly may include a panel and a support cushion. The support cushion may include a cavity defined by one or more surfaces of the support cushion. The assembly may include a translation sub-assembly configured to translate the support sub-assembly. The translation sub-assembly may include one or more translation arms. The translation sub-assembly may include one or more guide rails. The translation sub-assembly may include one or more linear bearings configured to engage with the one or more guide rails, the one or more linear bears slideable along a length of the one or more guide rails. The translation sub-assembly may include one or more translation devices configured to translate the support sub-assembly between a first position and one or more additional positions.

    AIRCRAFT SEAT WITH INTERNAL SEAT PAN RETURN SPRING MECHANISM

    公开(公告)号:US20240124142A1

    公开(公告)日:2024-04-18

    申请号:US17966283

    申请日:2022-10-14

    IPC分类号: B64D11/06

    CPC分类号: B64D11/064 B64D11/062

    摘要: An aircraft seat assembly including first and second stanchions forming interior spaces open through forward slots. A seat pan is pivotally attached to the stanchions and includes rearward extensions that extend through the forward slots and are received in the interior spaces. First and second spring mechanisms reside in the respective first and second interior spaces and are attached at opposing ends to their respective stanchion and to the seat pan. In use, rotating the seat pan toward a deployed position elongates the first and second elongation springs thereby energizing a return force of the spring mechanisms.

    AIRCRAFT SEAT WITH ENERGY ATTENUATING METERING PLATE

    公开(公告)号:US20240083582A1

    公开(公告)日:2024-03-14

    申请号:US17940873

    申请日:2022-09-08

    发明人: Chad R. Pacheco

    IPC分类号: B64D25/04 B64D11/06

    摘要: A seat base assembly for an aircraft seat includes parallel rails attached to an aircraft bulkhead, each rail including a slot extending vertically within the rail. The seat (e.g., seatback and seat frame) is attached to a sled capable of vertical translation relative to the bulkhead via slidable members that translate along the slots. The sled includes a hole for accommodating a locking pin controllable by the seat occupant. A metering plate attached to the seat base behind the sled is folded over a lateral axis into a forward and rear layer, the forward layer including holes for the locking pin wherein each hole corresponds to a desired seat height to which the seat may be adjusted by securing the locking pin through the sled hole and metering hole. In response to an impact event, the metering plate deforms to absorb impact energy and control downward deceleration of the seat.

    Multi-seat escape system and ejection seat sequencer

    公开(公告)号:US11713127B2

    公开(公告)日:2023-08-01

    申请号:US17549634

    申请日:2021-12-13

    IPC分类号: B64D25/10

    CPC分类号: B64D25/10

    摘要: An article of manufacture may include a tangible, non-transitory computer-readable storage medium having instructions stored thereon for controlling deployment of aircraft escape and ejection seat subsystems. The instructions, in response to execution by a first sequencer, cause the first sequencer to perform operations which may comprise receiving a power input, determining a seat location and a seat identity of a first ejection seat in which the first sequencer is installed, determining an ejection mode, sending a first deploy command to an escape path clearance subsystem, determining a deployment sequence for a seat rocket catapult subsystem and a plurality of ejection seat subsystems of the first ejection seat based on the seat location, the seat identity, and the ejection mode, sending a second deploy command to the seat rocket catapult subsystem, and sending a series of third deploy commands to the plurality of ejection seat subsystems.