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公开(公告)号:US10011197B2
公开(公告)日:2018-07-03
申请号:US15643997
申请日:2017-07-07
申请人: AMI INDUSTRIES, INC.
CPC分类号: B60N2/23 , B60N2/0296 , B60N2/0875 , B64D11/0639 , B64D11/064 , B64D11/0696 , F16H21/02 , F16H37/14
摘要: Systems and methods are disclosed herein for an aircraft seat with a dual-function linear actuator. The linear actuator may activate a first adjustable feature by moving in a first direction, and the linear actuator may activate a second adjustable feature by moving in a second direction. The linear actuator may include a decoupling mechanism. The decoupling mechanism may decouple the first adjustable feature and the second adjustable feature from the linear actuator in response to loss of power to the linear actuator.
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公开(公告)号:US20180170552A1
公开(公告)日:2018-06-21
申请号:US15382239
申请日:2016-12-16
申请人: AMI Industries, Inc.
发明人: Jacob W. Kirkley , Chad R. Pacheco
IPC分类号: B64D11/06
CPC分类号: B64D11/0698 , B64D11/064 , B64D11/0647 , B64D11/0691
摘要: A collapsible backrest may include a cover and a back panel retained within a first compartment of the cover. A base panel flexibly coupled to the back panel and retained within a second compartment of the cover with the central panel and the base panel defining a notch. A central panel may be flexibly coupled to the base panel and retained within a third compartment of the cover. An end panel may also be flexibly coupled to the central panel and retained within a fourth compartment of the cover. The central panel and the end panel define a cavity. The base panel, the central panel, and the end panel form a triangular support structure in a deployed position. The base panel, the central panel, and the end panel may also be arranged end-to-end and substantially parallel to the back panel in a stowed position.
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公开(公告)号:US20180155033A1
公开(公告)日:2018-06-07
申请号:US15368234
申请日:2016-12-02
申请人: AMI Industries, Inc.
发明人: Chad R. Pacheco
IPC分类号: B64D11/06
CPC分类号: B64D11/064 , B60N2/504 , B60N2/995 , B64D11/0641 , B64D11/0643 , B64D11/0691
摘要: A suspension recline system for a stowable seat may comprise a suspension member comprising a first end configured to be coupled to a seat back of the stowable seat, and a second end configured to be coupled to a legrest for the stowable seat, wherein the suspension recline system is moveable between a stowed position and a deployed position. The stowable seat may recline in response to the suspension recline system being moved to the deployed position. An end of the suspension member may be configured to be inserted into a slot disposed in the legrest, in the deployed position.
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公开(公告)号:US09908441B2
公开(公告)日:2018-03-06
申请号:US15586624
申请日:2017-05-04
申请人: AMI Industries, Inc.
CPC分类号: B60N2/0224 , B60N2/0232 , B60N2/0296 , B60N2/2209 , B60N2/929 , B60N2/933 , B64D11/06395 , B64D11/064 , B64D11/0696 , F16K31/52 , H02K7/06 , H02K7/108 , H02K7/14
摘要: A seat actuation control system is disclosed. The seat actuation control system may permit multiple functions to be controlled by a single actuator. For example, a seat floor tracking function, and a seat pan track and swivel function may be individually controlled by a single actuator, such as a rotary actuator.
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公开(公告)号:US09873510B2
公开(公告)日:2018-01-23
申请号:US15083532
申请日:2016-03-29
申请人: AMI Industries, Inc.
发明人: Keith M. Ferguson
IPC分类号: B64D11/06
CPC分类号: B64D11/0698 , B64D11/062 , B64D11/064 , B64D11/0691
摘要: A contoured stowable seat is provided. The contoured stowable seat may comprise a housing, a seat pan, a contoured backrest, and a deployment lever. The contoured stowable seat may be configured to be in a stowed position and a deployed position. In response to the seat pan being in the deployed position, the deployment lever may contact the contoured backrest, causing the contoured backrest to deploy and form into a contoured shape. The contoured stowable seat may also further comprise a tension cord and a headrest. The contoured backrest may also further comprise a cushion located on the outer surface of the contoured backrest.
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公开(公告)号:US09585480B2
公开(公告)日:2017-03-07
申请号:US14273984
申请日:2014-05-09
申请人: AMI INDUSTRIES, INC.
CPC分类号: A47C1/03294 , A47C1/032 , A47C3/00 , B60N2/2209 , B64D11/064
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。
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公开(公告)号:US20160229539A1
公开(公告)日:2016-08-11
申请号:US14618052
申请日:2015-02-10
申请人: AMI INDUSTRIES, INC.
CPC分类号: B60N2/23 , B60N2/0296 , B60N2/0875 , B64D11/0639 , B64D11/064 , B64D11/0696 , F16H21/02 , F16H37/14
摘要: Systems and methods are disclosed herein for an aircraft seat with a dual-function linear actuator. The linear actuator may activate a first adjustable feature by moving in a first direction, and the linear actuator may activate a second adjustable feature by moving in a second direction. The linear actuator may include a decoupling mechanism. The decoupling mechanism may decouple the first adjustable feature and the second adjustable feature from the linear actuator in response to loss of power to the linear actuator.
摘要翻译: 本文公开了具有双功能线性致动器的飞机座椅的系统和方法。 线性致动器可以通过沿第一方向移动来激活第一可调特征,并且线性致动器可以通过沿第二方向移动来激活第二可调特征。 线性致动器可以包括去耦机构。 解耦机构可以响应于线性致动器的功率损失,将第一可调特征和第二可调特征与线性致动器分离。
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公开(公告)号:US09388615B2
公开(公告)日:2016-07-12
申请号:US14282432
申请日:2014-05-20
申请人: AMI INDUSTRIES, INC.
CPC分类号: E05D7/12 , A47C7/58 , B64D11/064 , E05D1/02 , E05D7/00 , E05D11/00 , E05Y2800/342 , Y10T16/5253
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。
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公开(公告)号:US08998323B2
公开(公告)日:2015-04-07
申请号:US13571084
申请日:2012-08-09
申请人: Martin S. Day , Chad R. Pacheco , Donald R. Pinkal
发明人: Martin S. Day , Chad R. Pacheco , Donald R. Pinkal
IPC分类号: B60N2/427
CPC分类号: B60N2/427 , B60N2/42736 , B64D11/0696 , Y02T50/46
摘要: A track-mounted aircraft seat has seat track locking pins that are capable of moving independently to remain engaged with the seat track assembly in a warped-floor condition. The seat track locking pins are actuated by means of a pair of torque tubes that rotate independently about a common pilot shaft. A control link, which is operated by the user, acts on a pair of bell cranks each of which acts on one of the torque tubes. The control link is attached to the bell cranks by means of a spherical joint. Because the torque tubes rotate independently and because the spherical joint allows the bell cranks also to move independently, in the event of a warped-floor condition, rotation of one torque tube caused by the skewed seat track will not cause the other torque tube to release its track locking pin.
摘要翻译: 轨道安装的飞机座椅具有座椅轨道锁定销,其能够独立地移动以在翘曲地板状态下保持与座椅轨道组件接合。 座椅轨道锁定销通过一对扭矩管来致动,该扭矩管围绕公共导向轴独立地旋转。 由用户操作的控制链路作用在一对钟形曲柄上,每个钟形曲柄作用在一个扭矩管上。 控制连杆通过球形接头连接到钟形曲柄上。 因为扭矩管独立地旋转,并且由于球形接头允许钟形曲柄也可以独立地移动,所以在扭曲的地板状况的情况下,由倾斜的座椅轨道引起的一个扭矩管的旋转将不会导致另一个扭矩管释放 其轨道锁定销。
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公开(公告)号:US20120199695A1
公开(公告)日:2012-08-09
申请号:US13348207
申请日:2012-01-11
IPC分类号: B64D11/06
CPC分类号: B64D11/0691
摘要: A self-stowing jumpseat consists of a seat frame that is deployed by pulling the seat frame out of a pocket formed in the edge of a bulkhead. Once the seat frame has been deployed and locked in position, the seat pan is folded down to enable a user to be seated. The seat pan is spring-loaded to fold up, so that when the user vacates the seat, the seat pan automatically folds up into the closed configuration. As it does so, an interlock lever attached to the seat pan trips the seat frame locks from their locked to their unlocked positions. The seat frame has a retraction mechanism that urges the seat into the pocket. Accordingly, as soon as the seat pan interlock lever releases the seat frame locks, the retraction mechanism causes the folded seat frame to move into the stowed position within the bulkhead.
摘要翻译: 自动收起的跳伞由一个座椅框架组成,座椅框架通过将座椅框架从形成在隔板边缘的口袋中拉出而展开。 一旦座椅框架已经部署并被锁定就位,座椅底板被向下折叠以使使用者能够就位。 座垫被弹簧加载以折叠,使得当使用者离开座椅时,座椅底板自动折叠成闭合构型。 如此,附接到座盘的联锁杆将座椅框架锁从锁定位置解锁到解锁位置。 座椅框架具有将座椅推入口袋的缩回机构。 因此,一旦座盘互锁杆释放座椅框架锁,缩回机构就使得折叠的座椅框架移动到舱壁内的收起位置。
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