Rotatable cabin attendant seat and aircraft monument arrangement with a rotatable cabin attendant seat
    11.
    发明授权
    Rotatable cabin attendant seat and aircraft monument arrangement with a rotatable cabin attendant seat 有权
    可旋转的客舱座椅和飞机纪念碑布置与可旋转的客舱座位

    公开(公告)号:US09145209B2

    公开(公告)日:2015-09-29

    申请号:US13655076

    申请日:2012-10-18

    IPC分类号: B64D11/06

    摘要: A cabin attendant seat (14) comprises a backrest element (20) and a seat element (22) which is secured to the backrest element (20). The backrest element (20) is rotatable about a rotation axis (24a, 24b) in order to move the cabin attendant seat (14) between a rest position and an operating position. A fastening device (18) for fastening the cabin attendant seat (14) to a side wall (16) of an aircraft monument (12) is constructed and sized in such a manner that it is capable of directing away a predetermined maximum force which can be introduced into the cabin attendant seat (14) during operation of the cabin attendant seat (14) via the side wall (16) of the aircraft monument (12).

    摘要翻译: 座舱服务员座椅(14)包括靠背元件(20)和固定到靠背元件(20)的座位元件(22)。 靠背元件(20)可围绕旋转轴线(24a,24b)旋转,以便在休息位置和操作位置之间移动机舱服务员座椅(14)。 用于将舱室驾驶员座椅(14)紧固到飞机纪念碑(12)的侧壁(16)的紧固装置(18)被构造和定尺寸为使得能够引导预定的最大力 通过飞机纪念碑(12)的侧壁(16)在乘务员座椅(14)的操作期间被引入驾驶室座椅(14)。

    Safety Seat Without Side Fittings
    12.
    发明申请
    Safety Seat Without Side Fittings 审中-公开
    安全座椅无侧面配件

    公开(公告)号:US20100102602A1

    公开(公告)日:2010-04-29

    申请号:US12523523

    申请日:2008-01-09

    申请人: Holger Hansen

    发明人: Holger Hansen

    摘要: A safety seat for vehicles, including a seat portion having a rear end supported against vertical support straps of a strap framework secured to a vehicle. Each of two supports laterally disposed on the seat portion as a first end secured to the set. From the first end, each support extends in an inclined path, below the seat portion, to the vertical support straps. Each support has a free end remote from the first end and suspended in a loop formed on the vertical support straps. To tensioning straps are disposed beneath the seat portion and extend along side edges thereof from a front securement and the seat portion to a connection with the vertical support straps. Each tensioning strap has a length less than the distance between the front securement and the rear end of the seat portion.

    摘要翻译: 一种用于车辆的安全座椅,包括座椅部分,该座椅部分的后端支撑在固定在车辆上的绑带框架的垂直支撑带上。 两个支撑件中的每一个作为固定到该组件上的第一端侧向设置在座椅部分上。 从第一端部,每个支撑件在座椅部分下方的倾斜路径中延伸到垂直支撑带。 每个支撑件具有远离第一端的自由端并且悬挂在形成在垂直支撑带上的环中。 张紧带被布置在座部下方并且沿其侧边缘从前固定件和座部分延伸到与垂直支撑带的连接。 每个张紧带的长度小于前部固定件和座椅部分的后端之间的距离。

    Child's seat for airplanes
    13.
    发明授权
    Child's seat for airplanes 失效
    儿童座椅的飞机

    公开(公告)号:US06474732B1

    公开(公告)日:2002-11-05

    申请号:US09633247

    申请日:2000-08-04

    申请人: Harald Merensky

    发明人: Harald Merensky

    IPC分类号: B60N232

    摘要: The child's seat for airplanes comprises a mounting adapted to be fastened to a partition wall of an airplane, and a seat fastened to the mounting such that the seat can assume two different vertical positions. In an upper takeoff and landing position, the seat is located above the head strike arc of a person seated on an airplane seat, while in a lower communicating position, assumed during the flight, the seat is at chest level of the accompanying person. Thanks to the child's seat, the number of adult passengers normally occupying passenger seats of an airplane need not be reduced.

    摘要翻译: 儿童用于飞机的座椅包括适于紧固到飞机的分隔壁上的安装件,以及固定到安装件的座椅,使得座椅可以呈现两个不同的垂直位置。 在起飞和着陆位置上,座椅位于坐在飞机座椅上的人的头部撞击弧的上方,而在飞行期间假定为较低的通信位置,座椅处于伴随人员的胸部水平。 由于孩子的座位,通常占用飞机乘客座位的成年乘客人数不需要减少。

    Variable energy attenuating apparatus
    14.
    发明授权
    Variable energy attenuating apparatus 有权
    可变能量衰减装置

    公开(公告)号:US06378939B1

    公开(公告)日:2002-04-30

    申请号:US09668156

    申请日:2000-09-25

    IPC分类号: B60N242

    摘要: An energy attenuating apparatus for use with a seat includes an elongated attenuator having a resistance to bending which varies along its length. A bending mechanism defining a nonlinear path receives the attenuator. Translation of the bending mechanism relative to the attenuator in a lengthwise direction of the attenuator produces bending of the attenuator to absorb energy applied to the energy attenuating apparatus.

    摘要翻译: 用于座椅的能量衰减装置包括具有沿其长度变化的弯曲阻力的细长衰减器。 限定非线性路径的弯曲机构接收衰减器。 在衰减器的长度方向上相对于衰减器的弯曲机构的平移产生衰减器的弯曲以吸收施加到能量衰减装置的能量。

    Aircraft bulkhead-mounted pilot seat with horizontal and vertical adjustment

    公开(公告)号:US12049321B2

    公开(公告)日:2024-07-30

    申请号:US17941674

    申请日:2022-09-09

    发明人: Chad R. Pacheco

    IPC分类号: B64D11/06 B64D25/04

    摘要: A bulkhead-mounted aircraft seat assembly configured for independent vertical and horizontal adjustment includes an aircraft seat (seatback and seat frame/cushion) for supporting a pilot, passenger, or other occupant. Parallel rails attach to the bulkhead and extend along the bulkhead (vertically or near vertically) with opposing slots set into each rail. A sled translates along the rails via paired sliding members set into the slots, each pair of sliding members connected to an axle extending through the sled. A four-bar linkage attached to the sled and to the aircraft seat; the four-bar linkage extends from a default position to allow the aircraft seat to translate along a horizontal linear rail under the seat while maintaining a stable vertical reference point above the cabin floor. The seat is independently configured for substantially vertical adjustment via a metering plate attached to the bulkhead.

    AIRCRAFT SEAT WITH NESTED ENERGY ATTENUATION GUIDE SYSTEM

    公开(公告)号:US20240124141A1

    公开(公告)日:2024-04-18

    申请号:US17966413

    申请日:2022-10-14

    IPC分类号: B64D11/06

    摘要: An aircraft seat assembly including stanchions defining elongated guide channels and elongated motion sleds nested in the guide channels and affixed to a seat bucket. An energy absorber implemented as a wire bender assembly is coupled between the stanchions and the motion sled. In use, the elongated guide channels guide motion of the motion sleds and the wire bender assemblies attenuate energy during a dynamic event exceeding a predetermined threshold load value. The elongated interface between the guide channels and motion sleds serve to transfer excessive loading to the seat frame thereby protecting the seat assembly from damage and the occupant from excessive lumbar spinal loads.

    Components for Enhancement of a Low Profile Crew Attendant Seat

    公开(公告)号:US20190233120A1

    公开(公告)日:2019-08-01

    申请号:US16375002

    申请日:2019-04-04

    发明人: Markus Spagl

    IPC分类号: B64D11/06

    摘要: A crew attendant seat assembly configured to be installed in an aircraft cabin and including a seat including a seat bottom hinged to a seatback to rotate between a stowed position and a deployed position, a spring member mountable to a static structure adjacent the and to an adjustable aperture on the hinge, the spring having two mounting positions, a harness mounted to the seat for restraining a seated passenger including a shoulder strap and a lap belt, and a storage area for retaining at least one of the lap belt and the buckle when the seat bottom is stowed, wherein at least one of the lap belt and the buckle are enclosed by the crew attendant seat assembly when the seat bottom is stowed.

    SEAT RAIL MOUNTING MEMBER
    19.
    发明申请

    公开(公告)号:US20180009535A1

    公开(公告)日:2018-01-11

    申请号:US15644090

    申请日:2017-07-07

    IPC分类号: B64D11/06 F16L3/12 H02G3/04

    摘要: An aircraft assembly with first and second seat rails for interlocking with an aircraft seat, and a systems component mounting member interlocked with those seat rails. The mounting member has a first anchor member interlocked with the first seat rail and a second anchor member interlocked with the second seat rail. The assembly includes an aircraft systems component mounted on the mounting member. Existing seat rails or tracks of the aircraft can be used for attachment of support brackets for aircraft systems components. A novel way of using existing seat rails to provide anchorage points for systems brackets for systems components is disclosed.

    Apparatus for holding a cabin attendant seat, cabin arrangement in a vehicle and vehicle having a cabin and such a cabin arrangement
    20.
    发明授权
    Apparatus for holding a cabin attendant seat, cabin arrangement in a vehicle and vehicle having a cabin and such a cabin arrangement 有权
    用于保持舱室座椅的座椅,车辆中的舱室布置以及具有舱室和车厢布置的车辆

    公开(公告)号:US09573689B2

    公开(公告)日:2017-02-21

    申请号:US14672883

    申请日:2015-03-30

    摘要: An apparatus for holding a cabin attendant seat in a cabin of a vehicle includes a base body attachable to a wall surface in the cabin, at least one holding mechanism for holding a cabin attendant seat, at least one linear movement mechanism, and at least one arresting mechanism. The at least one linear movement mechanism is attached to the base body and supports the at least one holding mechanism. The at least one linear movement mechanism is configured for laterally moving the at least one holding mechanism between at least two laterally distanced discrete positions. The at least one arresting mechanism is coupled with the at least one linear movement mechanism and is configured for arresting the at least one linear movement mechanism in the at least two discrete positions. By this apparatus a very space effective provision of a cabin attendant seat especially on a monument is given.

    摘要翻译: 一种用于将客舱座位保持在车辆的舱室中的装置包括可附接到舱室中的壁表面的基体,至少一个用于保持舱室座椅的保持机构,至少一个线性运动机构,以及至少一个 逮捕机制。 所述至少一个线性运动机构附接到所述基体并且支撑所述至少一个保持机构。 所述至少一个线性移动机构构造成用于在至少两个横向间隔离散位置之间横向移动所述至少一个保持机构。 所述至少一个止动机构与所述至少一个线性运动机构联接,并且被构造成用于在所述至少两个离散位置中止动所述至少一个线性运动机构。 通过这种装置,给出了一个非常空间有效的提供特别是在纪念碑上的客舱乘务员座位。