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    Floor system for a fuselage airframe of an aircraft
    1.
    发明授权
    Floor system for a fuselage airframe of an aircraft 有权
    飞机机身机身的地板系统

    公开(公告)号：US08074928B2

    公开(公告)日：2011-12-13

    申请号：US12842769

    申请日：2010-07-23

    申请人： Cord Haack ,  Markus Schumacher ,  Andrew Muin ,  Ian Scoley

    发明人： Cord Haack ,  Markus Schumacher ,  Andrew Muin ,  Ian Scoley

    IPC分类号： B64C1/18

    CPC分类号： B64C1/18 ,  B64D11/0696 ,  Y02T50/46

    摘要： A floor system for a fuselage section of an aircraft is provided. The floor system has an essentially self-supporting design and is substantially mechanically separate from the fuselage section as primary structure. Consequent to the free or self-supporting design of the floor system in the fuselage cell, the layout of the floor system along an aircraft axis can be matched to customer specifications in a simple manner without reference to structural boundary conditions of the fuselage structure. A floor surface for the floor system is formed from a number of floor elements which can be fitted with functional elements, wherein filling of empty spaces or cavities can be achieved with a number of floor equalization elements. As the floor elements have a relatively large support or fixing surface the loads induced by the functional elements are introduced into the floor system distributed over a large area such that the structural components thereof can be of a structurally lighter and thus weight-saving size.

    摘要翻译： 提供飞机机身部分的地面系统。 地板系统具有基本上自支撑的设计，并且基本上机械地与作为主结构的机身部分分离。 由于机身单元中的地板系统的自由或自支撑设计，沿着飞行器轴线的地板系统的布局可以以简单的方式与客户规格相匹配，而不参考机身结构的结构边界条件。 用于地板系统的地板表面由许多可装配有功能元件的地板元件形成，其中可以利用多个地板均衡元件来实现空的空间或空腔的填充。 由于地板元件具有相对较大的支撑或固定表面，所以由功能元件引起的载荷被引入到分布在大面积上的地板系统中，使得其结构部件可以具有结构上较轻且因此减轻重量的尺寸。

    FLOOR SYSTEM FOR A FUSELAGE AIRFRAME OF AN AIRCRAFT
    2.
    发明申请
    FLOOR SYSTEM FOR A FUSELAGE AIRFRAME OF AN AIRCRAFT 有权
    飞机空调机的地板系统

    公开(公告)号：US20110011978A1

    公开(公告)日：2011-01-20

    申请号：US12842769

    申请日：2010-07-23

    申请人： Cord Haack ,  Markus Schumacher ,  Andrew Muin ,  Ian Scoley

    发明人： Cord Haack ,  Markus Schumacher ,  Andrew Muin ,  Ian Scoley

    IPC分类号： B64C1/18

    CPC分类号： B64C1/18 ,  B64D11/0696 ,  Y02T50/46

    摘要： A floor system for a fuselage section of an aircraft is provided. The floor system has an essentially self-supporting design and is substantially mechanically separate from the fuselage section as primary structure. Consequent to the free or self-supporting design of the floor system in the fuselage cell, the layout of the floor system along an aircraft axis can be matched to customer specifications in a simple manner without reference to structural boundary conditions of the fuselage structure. A floor surface for the floor system is formed from a number of floor elements which can be fitted with functional elements, wherein filling of empty spaces or cavities can be achieved with a number of floor equalisation elements. As the floor elements have a relatively large support or fixing surface the loads induced by the functional elements are introduced into the floor system distributed over a large area such that the structural components thereof can be of a structurally lighter and thus weight-saving size.

    摘要翻译： 提供飞机机身部分的地面系统。 地板系统具有基本上自支撑的设计，并且基本上机械地与作为主结构的机身部分分离。 由于机身单元中的地板系统的自由或自支撑设计，沿着飞行器轴线的地板系统的布局可以以简单的方式与客户规格相匹配，而不参考机身结构的结构边界条件。 用于地板系统的地板表面由许多可装配有功能元件的地板元件形成，其中可以利用多个地板均衡元件来实现空的空间或空腔的填充。 由于地板元件具有相对较大的支撑或固定表面，所以由功能元件引起的载荷被引入到分布在大面积上的地板系统中，使得其结构部件可以具有结构上较轻且因此减轻重量的尺寸。

    Luggage Retention Device and Seat with Such a Luggage Retention Device
    5.
    发明申请
    Luggage Retention Device and Seat with Such a Luggage Retention Device 审中-公开
    具有行李保持装置的行李保持装置和座椅

    公开(公告)号：US20070152480A1

    公开(公告)日：2007-07-05

    申请号：US11618303

    申请日：2006-12-29

    申请人： Andrew Muin ,  Markus Schumacher

    发明人： Andrew Muin ,  Markus Schumacher

    IPC分类号： A47C7/62

    CPC分类号： B64D11/0636 ,  B64D11/003 ,  B64D11/064

    摘要： A luggage retention device may be affixed underneath a seat area of a passenger seat and includes an upper element and a lower element which may be made of flexible materials. The upper element in the region of a backrest of the passenger seat is spaced apart from the lower element to form a raised part, and in the region of a front edge of a seat area contacts the lower element to form a part of the luggage retention device, the part being arranged so as to be lying substantially flat.

    摘要翻译： 行李保持装置可以固定在乘客座椅的座位区域的下面，并且包括可由柔性材料制成的上部元件和下部元件。 乘客座椅的靠背区域中的上部元件与下部元件间隔开以形成凸起部分，并且在座位区域的前边缘的区域中接触下部元件以形成行李保持件的一部分 装置，该部分被布置成基本平坦。

    Downwards folding seat
    6.
    发明申请
    Downwards folding seat 有权
    向下折叠座椅

    公开(公告)号：US20090127911A1

    公开(公告)日：2009-05-21

    申请号：US12319969

    申请日：2009-01-14

    申请人： Markus Schumacher ,  Andrew Muin

    发明人： Markus Schumacher ,  Andrew Muin

    IPC分类号： B60N2/46

    CPC分类号： B64D11/064 ,  B60N2/3047 ,  B60N2/753 ,  B64D11/06 ,  B64D11/0646

    摘要： A folding seat for an aircraft has a backrest, a seat area and an armrest. The seat area is pivotable. When the seat area is pivoted, the armrest is pivotable downwards, the seat area and the armrest being coupled by at least one coupling element in the form of a bevel gear.

    摘要翻译： 用于飞机的折叠座椅具有靠背，座椅区域和扶手。 座椅区域是可枢转的。 当座椅区域枢转时，扶手可向下枢转，座椅区域和扶手通过锥齿轮形式的至少一个联接元件联接。

    Seat backrest for the crew rest compartment of an aircraft
    7.
    发明授权
    Seat backrest for the crew rest compartment of an aircraft 有权
    飞机的乘员休息室的座椅靠背

    公开(公告)号：US07490906B2

    公开(公告)日：2009-02-17

    申请号：US11135129

    申请日：2005-05-23

    申请人： Markus Schumacher ,  Andrew Muin

    发明人： Markus Schumacher ,  Andrew Muin

    IPC分类号： B60N2/02 ,  B60N2/46

    CPC分类号： A47C1/023 ,  A47C7/407 ,  B64D11/0691

    摘要： To save space it is often not possible to provide a comfortable seat beside a bed, for example for a second flightdeck crew. Normally, sitting on a bed is not comfortable for extended periods of time. The present invention states a backrest arrangement which can be changed from a foldaway position to a seating position. The backrest arrangement can be hinged to a wall. In foldaway position, the distance between a lower region of the backrest and the essentially vertical surface is shorter than in the seating position. In this way the backrest arrangement can for example be attached to a wall beside a bed; in the seating position the backrest arrangement provides a comfortable and safe seat.

    摘要翻译： 为了节省空间，通常不可能在床旁边提供舒适的座位，例如在第二个飞行甲板上。 通常坐在床上长时间不舒服。 本发明提出了一种可以从折叠位置改变到就座位置的靠背装置。 靠背装置可以铰接到墙上。 在折叠位置，靠背的下部区域和基本上垂直的表面之间的距离比在就座位置短。 以这种方式，靠背装置可以例如附接到床旁边的墙壁; 在座位位置，靠背装置提供舒适和安全的座椅。

    Seating group of passenger seats especially for an aircraft cabin
    8.
    发明授权
    Seating group of passenger seats especially for an aircraft cabin 失效
    乘客座椅座椅组，特别适用于飞机机舱

    公开(公告)号：US5829836A

    公开(公告)日：1998-11-03

    申请号：US714206

    申请日：1996-09-16

    申请人： Markus Schumacher ,  Andrew Muin

    发明人： Markus Schumacher ,  Andrew Muin

    IPC分类号： B60N2/06 ,  B64D11/06 ,  A47C15/00

    CPC分类号： B60N2/06 ,  B64D11/0693

    摘要： Seating groups for passengers, for example in an aircraft cabin, are equipped with several seats having seat components supported on a support base on which the seat components, especially the seat sections are laterally slideable to make the seats wider when a passenger sits on a seat or narrower when a passenger is not sitting on a seat. The seat widening or narrowing is accomplished in several ways, for example, with the aid of a grooved shaft that operates as a spindle when turned by tilting a seat component, or by springs that vault upwardly when not loaded and spread when a passenger sits on a seat supported by the springs. The grooved shaft can be operated for example by an armrest or a seat section.

    摘要翻译： 乘客的座位组，例如在飞机机舱中，配备有多个座位，其具有支撑在支撑基座上的座椅部件，座椅部件，特别是座椅部分可侧向滑动，座椅部件可以在乘客坐在座椅上时使座椅更宽 或者当乘客不坐在座位上时更窄。 座椅变宽或变窄是以几种方式完成的，例如借助于在通过倾斜座椅部件转动时作为主轴工作的带槽的轴，或者当乘客坐下时不加载和扩展时向上突出的弹簧 由弹簧支撑的座椅。 带槽的轴可以例如由扶手或座椅部分操作。

    Luggage compartment system especially for a passenger aircraft cabin
    9.
    发明授权
    Luggage compartment system especially for a passenger aircraft cabin 失效
    行李箱系统特别适用于客机舱

    公开(公告)号：US5820076A

    公开(公告)日：1998-10-13

    申请号：US742459

    申请日：1996-11-01

    申请人： Markus Schumacher ,  Andrew Muin

    发明人： Markus Schumacher ,  Andrew Muin

    IPC分类号： B64D11/00 ,  A47F5/08

    CPC分类号： B64D11/003

    摘要： A luggage compartment system for a passenger cabin, especially for commercial airliners, is equipped with compartment units each formed by at least two compartments interconnected or coupled through a coupling, guide and drive mechanism (13) for moving the compartments of a unit from a closed upper position to an open lower position and vice versa. Each unit has a large compartment and a small compartment, the latter is intended for smaller luggage items, including fragile items, while the larger compartment is intended for large luggage including suitcases. In the closed position the two compartments of a unit are arranged next to each other in a direction extending crosswise to a longitudinal central vertical plane (10) through the aircraft cabin. The compartments have for their bottom contoured panels that are integrated into the ceiling of the cabin in the closed compartment position. The coupling, guide and drive mechanism (13) moves both compartments of a unit either up or down, whereby the compartments in their down position are located just above the passenger seats for loading and unloading with the smaller compartment being positioned above the larger compartment. Openings in the compartments face the central plane.

    摘要翻译： 用于客舱，特别是用于商业客机的行李厢系统装备有隔室单元，每个隔间单元由至少两个互连或通过联接器，引导和驱动机构（13）联接的隔室形成，用于将单元的隔室从封闭 上部位置到打开的较低位置，反之亦然。 每个单元都有一个大的隔间和一个小隔间，后者适用于较小的行李物品，包括易碎物品，而较大的隔间用于包括行李箱的大型行李箱。 在关闭位置，单元的两个隔室沿着与通过飞机机舱的纵向中心垂直平面（10）横向延伸的方向彼此相邻布置。 隔间具有底部轮廓的面板，在封闭的隔间位置集成到机舱的天花板中。 联接器，引导和驱动机构（13）将单元的两个隔间向上或向下移动，由此在其下方位置的隔间位于乘客座椅正上方，用于装载和卸载，较小隔间位于较大隔间上方。 隔间中的开口面向中心平面。

    Telescopic stowage bin
    10.
    发明授权
    Telescopic stowage bin 有权
    伸缩式装载箱

    公开(公告)号：US07922119B2

    公开(公告)日：2011-04-12

    申请号：US11618290

    申请日：2006-12-29

    申请人： Andrew Muin ,  Markus Schumacher

    发明人： Andrew Muin ,  Markus Schumacher

    IPC分类号： B64D11/00

    CPC分类号： B64D11/003 ,  Y02T50/46

    摘要： A stowage bin arrangement for fastening a stowage bin for an aircraft, includes a stowage bin unit with a first direction of extension. The stowage bin unit may be fastened to an aircraft structure and be designed such that the stowage bin unit is capable of being telescopically extended along the first direction of extension.

    摘要翻译： 用于紧固用于飞行器的存放箱的存放箱装置包括具有第一延伸方向的装载箱单元。 装载箱单元可以被紧固到飞机结构，并且被设计成使得该装载箱单元能够沿着第一延伸方向伸缩地延伸。