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91. 发明申请

US20090301832A1 Energy Absorber for Aircraft 失效
标题翻译：飞机能量吸收器
公开(公告)号：US20090301832A1
公开(公告)日：2009-12-10
申请号：US12223829
申请日：2007-02-08
申请人： Dirk Humfeldt , Michael Harriehausen , Jan Schröder , Martin Sperber , Michael Demary
发明人： Dirk Humfeldt , Michael Harriehausen , Jan Schröder , Martin Sperber , Michael Demary
IPC分类号： F16F7/12 , B60R19/02
CPC分类号： B64C1/062 , F16F7/123
摘要： An energy absorber for aircraft, which includes one or more energy absorber elements and a housing, whereby the energy absorber elements can absorb crash impulses by plastic deformation within the housing. Thus, the load on the primary structure and the respective inboard devices is limited, which can lead to an increased, passive safety of the passengers and a weight reduction.
摘要翻译：一种用于飞机的能量吸收器，其包括一个或多个能量吸收器元件和壳体，由此能量吸收器元件可以通过壳体内的塑性变形吸收碰撞冲击。因此，主结构和相应的内置装置上的负载受到限制，这可能导致乘客的被动安全性增加和重量减轻。

92. 发明授权

US07629068B2 Aircraft having integrated electrochemical supply system 有权
标题翻译：具有集成电化学供应系统的飞机
公开(公告)号：US07629068B2
公开(公告)日：2009-12-08
申请号：US11137231
申请日：2005-05-25
申请人： Claus Hoffjann , Hans-Georg Schuldzig , Harald Gruendel , Hans-Juergen Heinrich
发明人： Claus Hoffjann , Hans-Georg Schuldzig , Harald Gruendel , Hans-Juergen Heinrich
IPC分类号： H01M8/18
CPC分类号： B64D41/00 , B64D10/00 , B64D11/02 , B64D41/007 , B64D2041/005 , C02F1/04 , C02F1/461 , C02F2103/002 , C02F2201/009 , H01M8/00 , H01M2250/20 , Y02A20/212 , Y02T90/32 , Y02T90/36
摘要： An aircraft includes a supply system with an electrochemical reactor for generating energy, hydrogen, oxygen and clear water from grey water, a hydrocarbon containing fuel and air, so that the up to now separated systems for supply of clear water, generation of energy and generation of oxygen are combined to a combined system. The necessary redundancies may thereby secured by two or more systems of the same kind, which may be operated completely independently of each other.
摘要翻译：飞机包括具有用于从灰水，含烃燃料和空气产生能量，氢，氧和清水的电化学反应器的供应系统，使得迄今分离的用于供应清水，产生能量和产生的分离系统的氧气组合到组合系统。因此，可以通过两个或更多个相同类型的系统来确保必要的冗余，这些系统可以彼此完全独立地操作。

93. 发明申请

US20090294585A1 ASSEMBLY FOR STORING OBJECTS IN THE CABIN OF A VEHICLE 有权
标题翻译：大会在车辆仓库存储物体
公开(公告)号：US20090294585A1
公开(公告)日：2009-12-03
申请号：US12474469
申请日：2009-05-29
申请人： Karsten Schmidt , Bjoern Wandmaker
发明人： Karsten Schmidt , Bjoern Wandmaker
IPC分类号： B64C1/22 , B60R99/00
CPC分类号： B60R7/02 , B64D11/003 , B64D2231/025
摘要： The invention relates to an assembly for storing objects in the cabin of a vehicle, comprising at least one frame with attachment means, and at least one holding device for mounting the objects, wherein the frame has a contour that, at least in some regions, essentially corresponds to the interior contour of a storage container so that the frame can be arranged in the storage container and can be attached in the storage container with the use of the attachment means, and wherein the holding device can be removably stored in the frame. The assembly according to the invention can be placed in a pre-assembled state in the vehicle, thus reducing the time required for installation and maintenance, while at the same time making better use of the available space.
摘要翻译：本发明涉及一种用于将物体存储在车辆的舱内的组件，其包括至少一个具有附接装置的框架以及用于安装物体的至少一个保持装置，其中该框架具有至少在一些区域中的轮廓，基本上对应于存储容器的内部轮廓，使得框架可以布置在存储容器中并且可以使用附接装置附接到存储容器中，并且其中保持装置可以可拆卸地存储在框架中。根据本发明的组件可以放置在车辆中的预组装状态，从而减少安装和维护所需的时间，同时更好地利用可用空间。

94. 发明申请

US20090291625A1 Air System 有权
标题翻译：空气系统
公开(公告)号：US20090291625A1
公开(公告)日：2009-11-26
申请号：US11795778
申请日：2006-01-24
申请人： Frank Klimpel , Torge Pfafferott
发明人： Frank Klimpel , Torge Pfafferott
IPC分类号： B64D13/02 , F25B29/00
CPC分类号： B64D13/02 , B64D13/06 , B64D2013/0618 , B64D2013/0644 , B64D2013/0688 , Y02T50/56
摘要： An air system for pressurizing and air conditioning a cockpit and cabin space of a plane comprises a compressor (3) for compressing an air mass flow, wherein the air mass flow to be compressed is extracted through a ram air duct (13, 14) from the environment of the plane and supplied through a heat exchanger (15, 18) to at least one zone (10A-D) to be pressurized and air conditioned.
摘要翻译：用于对飞机的驾驶舱和客舱空间进行加压和空调的空气系统包括用于压缩空气质量流的压缩机（3），其中待压缩的空气质量流量通过冲压空气管道（13,14）从平面的环境并通过热交换器（15,18）供应到至少一个区域（10A-D），以被加压和空调。

95. 发明申请

US20090289146A1 INTEGRATED ACOUSTIC DECOUPLING IN A HABITATION MODULE 有权
标题翻译：在一个居住模块中集成的声学解体
公开(公告)号：US20090289146A1
公开(公告)日：2009-11-26
申请号：US12466516
申请日：2009-05-15
申请人： Tobias Gauggel , Martin Geldien , Markus Klingseis , Christian Wesselink
发明人： Tobias Gauggel , Martin Geldien , Markus Klingseis , Christian Wesselink
IPC分类号： B64D11/00 , B64C1/40 , B64D11/06 , B64D11/04
CPC分类号： B64D11/00 , B64C1/40 , B64D2011/0046 , B64D2011/0076
摘要： According to an exemplary embodiment of the invention, a combined habitation module for the crew of an aircraft is provided, which habitation module comprises two monument units that are separated from each other by a gap such that acoustic decoupling of the two monument units from each other is provided. In this way noise propagation within the habitation module may be prevented to a large extent.
摘要翻译：根据本发明的示例性实施例，提供了一种用于飞机机组人员的组合居住模块，该居住模块包括两个纪念碑单元，这两个纪念碑单元通过间隙彼此分开，使得两个纪念碑单元彼此的声学解耦被提供。以这种方式，可以在很大程度上防止居住模块内的噪声传播。

96. 发明申请

US20090283641A1 AIRCRAFT WITH CONNECTION ELEMENT FOR CONNECTING A CONDUIT SYSTEM TO COOLING AGGREGATES IN AIRCRAFT CABINS 有权
标题翻译：具有连接元件的连接元件用于冷却航空仓库中的集合体的飞机
公开(公告)号：US20090283641A1
公开(公告)日：2009-11-19
申请号：US12472221
申请日：2009-05-26
申请人： Theo DE BUHR
发明人： Theo DE BUHR
IPC分类号： B64C1/00
CPC分类号： B64D11/04 , F16L41/00 , Y02T50/46
摘要： The invention relates to an aircraft with a connection element for connecting at least one first conduit element or the like positioned in a supply chamber of an aircraft with at least one second conduit element positioned in a cabin chamber of the aircraft, wherein supply chamber and cabin chamber are separated from each other by means of a separation element, substantially comprising a connection part comprising fastening elements for fastening the first and second conduit element.Known connection elements have the disadvantage that there occur sealing problems due to the fastening of the fastening element at the outside of the connection part at the end facing the cabin chamber. A further disadvantage is that the connection elements protrude into the cabin chamber and form stumble edges there.In that at least the fastening element for the fastening the conduit element of the cabin chamber is provided within the connection part, there may be realised a compact structural shape which does not protrude from the separating element into the cabin chamber, and which may in addition be reliably sealed.
摘要翻译：本发明涉及一种具有连接元件的飞行器，该连接元件用于连接位于飞行器的供应室中的至少一个第一导管元件等，其中至少一个第二导管元件定位在飞机的舱室中，其中供应室和舱室室通过分离元件彼此分离，基本上包括连接部分，该连接部分包括用于紧固第一和第二导管元件的紧固元件。已知的连接元件具有这样的缺点，即由于紧固元件在面向机舱的端部处的连接部分的外部处的紧固而出现密封问题。另一个缺点是连接元件突出到舱室中并在那里形成绊倒边缘。因为至少用于紧固舱室的管道元件的紧固元件设置在连接部分内，所以可以实现紧凑的结构形状，其不会从分离元件突出到舱室中，并且可以另外可靠密封。

97. 发明申请

US20090272853A1 Lift-Augmenting Flap, in Particular for Leading Edge Flap, for an Aerodynamically Effective Wing 有权
标题翻译：升降翼，特别是前缘翼片，用于空气动力学有效的翼
公开(公告)号：US20090272853A1
公开(公告)日：2009-11-05
申请号：US11922068
申请日：2006-06-14
申请人： Morten Raudszus , Bernhard Schlipf , Luc Andreani , Xavier Hue , Mark Heintjes
发明人： Morten Raudszus , Bernhard Schlipf , Luc Andreani , Xavier Hue , Mark Heintjes
IPC分类号： B64C3/50 , B64C9/22
CPC分类号： B64C3/50 , Y02T50/14
摘要： A lift-augmenting leading edge flap for a carrying wing of an aircraft, wherein the flap comprises an essentially rigid main body which makes a transition from the first side to the second side of the wing the flap being adjustable by a retention- and actuation mechanism coupled between the flap and wing box, between a first, retracted, position and a second, extended, position, wherein the first transition region of the flap is slidable to rest in each position essentially free of any gap, against the first skin of the wing box or against the wing end cover, in relation to the wing end cover.
摘要翻译：一种用于飞行器的携带翼的提升增加的前缘翼片，其中所述翼片包括基本上刚性的主体，其从翼的第一侧向第二侧过渡，所述翼可通过保持和致动机构联接在所述翼片和翼盒之间，在第一缩回位置和第二延伸位置之间，其中所述翼片的第一过渡区域可滑动以在基本上没有任何间隙的每个位置中抵靠所述翼片的第一皮肤相对于机翼端盖，机翼盒或机翼端盖。

98. 发明申请

US20090272844A1 Method and Device for Supporting the Take-Off Rotation of an Aircraft 有权
标题翻译：支持飞机起飞旋转的方法和装置
公开(公告)号：US20090272844A1
公开(公告)日：2009-11-05
申请号：US11922059
申请日：2006-06-13
申请人： André Anger , Wolfram Schöne
发明人： André Anger , Wolfram Schöne
IPC分类号： B64C25/04 , B64C25/34
CPC分类号： B64C25/00
摘要： A method and a device for supporting the take-off rotation of an aircraft, which aircraft comprises on each side of the aircraft at least two main landing gear units, arranged one behind the other, which main landing gear units comprising wheels. For supporting the take-off rotation, in at least one rear pair of the main landing gear units the distance between the wheels of these rear main landing gear units, which wheels roll on the ground, and the fuselage, may actively be reduced.
摘要翻译：一种用于支撑飞行器的起飞旋转的方法和装置，该飞行器在飞行器的每一侧上包括一个彼此相邻布置的至少两个主起落架单元，其中主起落架单元包括轮。为了支撑起飞旋转，在主起落架单元的至少一对后部中，这些后主起落架单元的车轮与地面之间的距离与机身之间的距离可以被有效地减小。

99. 发明申请

US20090266937A1 REDUCTION OF FRICTIONAL LOSSES IN THE REGION OF BOUNDARY LAYERS ON SURFACES, AROUND WHICH A FLUID FLOWS 有权
标题翻译：在边界层的边界层中减少流体流动的表面上的摩擦损失
公开(公告)号：US20090266937A1
公开(公告)日：2009-10-29
申请号：US11911138
申请日：2006-04-05
申请人： Eckart Frankenberger , Matthias Meussen
发明人： Eckart Frankenberger , Matthias Meussen
IPC分类号： B64C21/06 , F15D1/12
CPC分类号： F15D1/12 , B64C21/06 , B64C2230/04 , B64C2230/22 , Y02T50/166
摘要： An aerodynamic body with a plurality of nozzles for throttling a fluid flow to be removed by suction through the nozzles in a self-regulated fashion is disclosed. The aerodynamic body according to one example, includes a plurality of throttling nozzles with a throttle section that is defined by an inlet and an outlet. In one example, the interior wall of the throttle section may be designed such that an effective flow cross section is reduced in a self-regulated fashion due to the creation of turbulences on the interior wall of the throttle section as the pressure differential between the inlet and the outlet of the throttle section increases.
摘要翻译：公开了一种具有多个喷嘴的空气动力体，用于以自调节的方式通过喷嘴抽吸来节流待流动的流体流。根据一个示例的空气动力体包括具有由入口和出口限定的节流部分的多个节流喷嘴。在一个示例中，节流部分的内壁可以被设计成使得由于在节流部分的内壁上产生湍流而以自调节方式减小有效流动横截面，因为入口并且节流部的出口增加。

100. 发明授权

US07607612B2 Passenger seat unit, in particular for commercial aircraft 失效
标题翻译：乘客座椅单元，特别是商用飞机
公开(公告)号：US07607612B2
公开(公告)日：2009-10-27
申请号：US11311858
申请日：2005-12-19
申请人： Andreas Baatz , Michael Supan , Frank Klepka
发明人： Andreas Baatz , Michael Supan , Frank Klepka
IPC分类号： B64D11/06
CPC分类号： B64D11/0604 , B64D11/06 , B64D11/0606
摘要： A passenger seat unit comprises modular designed elements, such as at least one seat, and shield elements in the head and foot region. The shield elements are formed by seat dividers that are arranged opposite each other, which seat dividers comprise laterally arranged limbs of the partition wall. One side of the limbs of the partition wall encloses a wall element and forms a closed longitudinal side. The other side of the limbs of the partition wall forms a second longitudinal side which frames an access opening. The longitudinal sides comprise means for length adjustment.It is particularly advantageous if the passenger seat unit according to the invention makes possible more flexible and more economical use of the existing cabin area in passenger aircraft. Flexible adaptation to various cabin lengths is possible without effort.
摘要翻译：乘客座椅单元包括模块化设计的元件，例如至少一个座椅，以及头部和脚部区域中的屏蔽元件。屏蔽元件由彼此相对布置的座隔板形成，该座隔板包括侧壁布置的分隔壁的四肢。分隔壁的四肢的一侧包围壁元件并形成封闭的纵向侧面。分隔壁的四肢的另一侧形成一个第二纵向侧面，其形成一个进入开口。纵向侧面包括用于长度调节的装置。如果根据本发明的乘客座椅单元使得客机中现有的客舱区域更加灵活和更经济地使用是特别有利的。可以毫不费力地灵活地适应各种舱室长度。

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