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1. 发明授权

US09650124B2 Switchable vortex generator and array formed therewith, and uses of the same 有权
公开(公告)号：US09650124B2
公开(公告)日：2017-05-16
申请号：US14089992
申请日：2013-11-26
申请人： Airbus Deutschland GmbH
发明人： Klaus-Peter Neitzke , Karin Bauer , Christian Bolzmacher , Winfried Kupke
IPC分类号： B64C21/00 , B64C3/38 , F15D1/12 , G01M9/04
CPC分类号： B64C3/38 , F15D1/12 , G01M9/04
摘要： A vortex generator is useable in a model in a fluid-dynamic channel. In order to save time during the development of vehicles, in particular, aircraft, to save wind tunnel time, it is suggested to configure the vortex generator to be switchable. A switchable vortex generator can be used, in particular, on models in fluid-dynamic channels and in fluid-dynamic channel tests.

2. 发明授权

US09242734B2 Device and method for distributing air in a cargo aircraft 有权
标题翻译：在货机中分配空气的装置和方法
公开(公告)号：US09242734B2
公开(公告)日：2016-01-26
申请号：US12294635
申请日：2007-03-29
申请人： Stefan Gumm , Manuela Horl , Dariusz Krakowski , Steffen Kalsow
发明人： Stefan Gumm , Manuela Horl , Dariusz Krakowski , Steffen Kalsow
IPC分类号： B64D13/00 , B64D13/06
CPC分类号： B64D13/06 , B64D2013/0618 , B64D2013/064 , Y02T50/56
摘要： A device for distributing air in a cargo aircraft includes using an air distribution system which is connected to a cargo deck. The air distribution system includes a source for bleed air, at least one air conditioning unit for treating the bleed air, a mixing unit which receives an air supply of recirculation air exiting the cargo deck and treated bleed air from the air conditioning unit, and at least one shut-off valve between the mixing unit and the cargo deck in order to interrupt or completely release the air supply to the cargo deck. A control unit establishes a desired air volume balance for the current operating state of the air distribution system and adjusts the flow volume through the at least one air conditioning unit such that the pressure prevailing in the mixing unit remains at a constant, predetermined value for all operating states.
摘要翻译：用于在货机中分配空气的装置包括使用连接到货物甲板的空气分配系统。空气分配系统包括用于排放空气的源，至少一个用于处理排放空气的空调单元，混合单元，其接收离开货物甲板的再循环空气的空气供应和来自空调单元的经处理的排出空气，以及在在混合单元和货物甲板之间的至少一个截止阀，以便中断或完全释放到货物甲板的空气供应。控制单元为空气分配系统的当前操作状态建立所需的空气量平衡，并调节通过至少一个空调单元的流量，使得混合单元中的压力保持恒定，预定值为所有运行状态。

3. 发明授权

US08752398B2 Refrigerating device, in particular for aircraft 有权
标题翻译：制冷装置，特别适用于飞机
公开(公告)号：US08752398B2
公开(公告)日：2014-06-17
申请号：US12790284
申请日：2010-05-28
申请人： Wilson Willy Casas Noriega , Stefan Wischhusen , Wolfgang Ebigt , Dirk Kastell
发明人： Wilson Willy Casas Noriega , Stefan Wischhusen , Wolfgang Ebigt , Dirk Kastell
IPC分类号： F25B41/00 , F25B49/00
CPC分类号： F25B41/00 , B64D13/08 , B64D2013/0674 , F25B2400/0401 , F25B2400/0411 , F25B2600/0251 , F25B2700/2106 , F25B2700/2116 , Y02T50/56
摘要： The invention relates to a refrigerating device (10), in particular for an aircraft, having a refrigerant circuit, in which a refrigerant container (12), an expansion valve (14), an evaporator (16), a compressor (20) and a condenser (22) are disposed. To save energy during operation and to increase the reliability and availability of the refrigerating device (10), in the refrigerant circuit there is a compressor bypass line (26), in which a bypass valve (18) is disposed, and a refrigerant pump (30) that is disposed downstream of the condenser (22) and upstream of the evaporator (16). It is possible to dispense with the refrigerant pump (30) if the condenser (22) is disposed at a higher level than the evaporator (16) in the refrigerant circuit.
摘要翻译：本发明涉及具有制冷剂回路的制冷装置（10），特别是用于航空器的制冷装置（10），其中制冷剂容器（12），膨胀阀（14），蒸发器（16），压缩机（20）和设置冷凝器（22）。为了节省运转时的能量，提高制冷装置（10）的可靠性和可利用性，在制冷剂回路中设置有配置有旁通阀（18）的压缩机旁通管路（26）和制冷剂泵 30），其设置在冷凝器（22）的下游和蒸发器（16）的上游。如果冷凝器（22）设置在比制冷剂回路中的蒸发器（16）更高的高度，则可以省略制冷剂泵（30）。

4. 发明授权

US08499887B2 Acoustically optimized cabin wall element 有权
标题翻译：声学优化舱壁元件
公开(公告)号：US08499887B2
公开(公告)日：2013-08-06
申请号：US12417695
申请日：2009-04-03
申请人： Wolfgang Gleine , Christian Thomas
发明人： Wolfgang Gleine , Christian Thomas
IPC分类号： E04B1/82
CPC分类号： G10K11/168 , B32B3/12 , B32B3/266 , B32B5/024 , B32B5/18 , B32B5/245 , B32B5/26 , B32B27/065 , B32B27/12 , B32B27/18 , B32B2260/021 , B32B2260/046 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2307/102 , B32B2307/51 , B32B2307/542 , B32B2307/718 , B32B2307/734 , B32B2605/18 , B60R13/0815 , B64C1/40
摘要： A wall element for the sound-insulating interior lining of a transport device, comprising at least one sandwich element, at least one insulation package and at least one absorber plane element. The sandwich element comprises at least one core layer, a first cover layer and a second cover layer, wherein the first cover layer and the second cover layer are each arranged on one side of the core layer. At least the first or the second cover layer is a microperforated layer; the sandwich element possesses a shear rigidity that is adjusted in such a way that the sandwich element comprises one or several coincidence boundary frequencies that are determined by the shear rigidity, which coincidence boundary frequencies are outside the frequency range that dominates the noise in the interior of the cabin; and the shear rigidity of the sandwich element at the same time is sufficient for said sandwich element to be used as an interior lining. Sound-insulating interior lining according to the aspects according to the invention provides adequate sound insulation also in the lower frequency range of below 500 Hz, without increasing the weight of the interior lining when compared to the weight of conventional interior linings.
摘要翻译：一种用于输送装置的隔音内衬的壁元件，包括至少一个夹层元件，至少一个绝缘封装和至少一个吸收体平面元件。夹层元件包括至少一个芯层，第一覆盖层和第二覆盖层，其中第一覆盖层和第二覆盖层分别布置在芯层的一侧上。至少第一或第二覆盖层是微穿孔层; 夹层元件具有剪切刚度，该剪切刚度以这样的方式调节，使得夹层元件包括由剪切刚度确定的一个或多个重合边界频率，该重合边界频率在主导内部噪声的频率范围之外机舱; 并且同时夹层元件的剪切刚度对于所述夹层元件用作内衬是足够的。根据本发明的方面，隔音内衬在低于500Hz的较低频率范围内也提供了足够的隔音，而与常规内衬的重量相比，不增加内衬的重量。

5. 发明授权

US08439061B2 Emergency ram air inlet valve of an aircraft 有权
标题翻译：飞机紧急冲压进气阀
公开(公告)号：US08439061B2
公开(公告)日：2013-05-14
申请号：US12093008
申请日：2006-10-25
申请人： Joerg Baumann
发明人： Joerg Baumann
IPC分类号： F02K99/00 , B64D33/02 , B64D13/00 , B64D13/02
CPC分类号： B64D13/02 , Y10T137/0536 , Y10T137/0645
摘要： The present invention relates to an emergency ram air inlet valve, also designated as an ERAI valve, of an aircraft. The valve includes an actuating element for opening and/or closing the valve and a controller operatively coupled to the valve, by which the valve can be set at different open angles. The open angle is set as a function of a temperature prevailing or preset in the aircraft cabin.
摘要翻译：本发明涉及飞机的也称为ERAI阀的紧急冲压进气阀。阀包括用于打开和/或关闭阀的致动元件以及可操作地连接到阀的控制器，通过该控制阀可以将阀设置在不同的敞开角度。打开角度被设定为飞机机舱中普遍或预设的温度的函数。

6. 发明授权

US08413878B2 System and method for manufacturing welded structures, and a welding additive material for this purpose 有权
标题翻译：用于制造焊接结构的系统和方法以及用于此目的的焊接添加剂材料
公开(公告)号：US08413878B2
公开(公告)日：2013-04-09
申请号：US12503809
申请日：2009-07-15
申请人： Jens Hackius , Rainer Kocik
发明人： Jens Hackius , Rainer Kocik
IPC分类号： B23K35/12
CPC分类号： B23K33/00 , B23K9/235 , B23K26/211 , B23K26/24 , B23K26/242 , B23K26/702 , B23K2101/006 , B23K2101/045 , B23K2101/24
摘要： A system and method for manufacturing welded structures comprises components to be welded, a welding additive material which, before the welding, has a shaped profile and the shaped profile is disposed between components to be welded and conforms with at least one of the components to be welded. At least one heat source is used in the method to weld the components, producing a weld seam on at least one side of one of the components.
摘要翻译：用于制造焊接结构的系统和方法包括待焊接的部件，焊接添加剂材料，其在焊接之前具有成形轮廓，并且成形轮廓设置在待焊接的部件之间，并且与要被焊接的部件中的至少一个部件一致焊接在用于焊接部件的方法中使用至少一个热源，在其中一个部件的至少一侧上产生焊缝。

7. 发明授权

US08220744B2 Fitting for introducing high forces into a fuselage cell of an aircraft 有权
标题翻译：适用于将高力量引入飞机的机身单元
公开(公告)号：US08220744B2
公开(公告)日：2012-07-17
申请号：US12009149
申请日：2008-01-16
申请人： Herrmann Benthien
发明人： Herrmann Benthien
IPC分类号： B64C1/06
CPC分类号： B60P7/0807 , B64D9/00 , B64D9/003 , Y02T50/46
摘要： Disclosed is a fitting for introducing great loads into a fuselage cell of an aircraft, in particular those which emanate from undercarriage components or are introduced into them. The fitting has a shoulder plate for bearing against the inside of the skin of the fuselage cell for example over its full surface area. Arranged underneath the shoulder plate is a vertical lug shackle with a lug for introducing the loads, wherein the lug shackle is led to the outside through a clearance in the skin of the fuselage cell. At least one approximately upright fastening shackle is provided on the upper side of the shoulder plate for connecting the fitting to a frame web. According to the invention, the loads occurring are introduced into the frame, substantially “moment-free” in the region of a neutral fiber, so that the said frame is not exposed to any appreciable flexural stresses and can be of a more lightweight design. The frame becomes the load introducing instrument and distributes the loads uniformly into the skin of the fuselage cell. Radially acting loads are transferred from the shoulder plate directly into the skin of the fuselage cell by way of shearing.
摘要翻译：公开了一种用于将大负载引入飞机的机身单元中的装置，特别是从起落架部件发出或被引入其中的那些。配件具有用于例如在其整个表面区域上抵靠机身单元的皮肤内部的肩板。安置在肩板下面的是具有用于引入负载的凸耳的垂直凸耳钩环，其中通过机身单元的皮肤中的间隙将凸耳钩环导向外部。至少一个大致直立的紧固钩环设置在肩板的上侧，用于将配件连接到框架网。根据本发明，发生的载荷被引入框架中，在中性纤维的区域中基本上“无力”，使得所述框架不暴露于任何明显的弯曲应力并且可以是更轻量化的设计。框架成为载荷引导仪器，并将载荷均匀分布到机身单元的皮肤中。径向作用载荷通过剪切从肩板直接传递到机身细胞的皮肤。

8. 发明授权

US08205834B2 Support structure for a wing 有权
标题翻译：翼的支撑结构
公开(公告)号：US08205834B2
公开(公告)日：2012-06-26
申请号：US12063699
申请日：2006-08-16
申请人： Christian Maenz
发明人： Christian Maenz
IPC分类号： B64C3/22
CPC分类号： B64C1/26 , B64C3/00 , B64C3/26 , B64C5/06 , E04B2001/193 , Y10T403/4381
摘要： A support structure for an aircraft, includes one or several bar elements and one or several junction elements. At least one bar element includes a transition region which can be made to engage at least one junction element. When the transition region of the bar element engages at least one junction element, centric force transmission takes place between the bar element and the junction element.
摘要翻译：用于飞行器的支撑结构包括一个或几个杆元件和一个或多个接合元件。至少一个杆元件包括能够使至少一个接合元件接合的过渡区域。当杆元件的过渡区域接合至少一个接合元件时，在杆元件和接合元件之间发生中心的力传递。

9. 发明授权

US08205824B2 Aircraft fuselage structure 有权
标题翻译：飞机机身结构
公开(公告)号：US08205824B2
公开(公告)日：2012-06-26
申请号：US12077121
申请日：2008-03-17
申请人： Joern Goos
发明人： Joern Goos
IPC分类号： B64C1/00 , B64C3/00
CPC分类号： B64C1/061 , B64C1/064 , B64C2039/105
摘要： An aircraft fuselage structure is described for a flying-wing aircraft, having a central area of slight curvature and side areas of greater curvature, which forms a pressure body and has an outer skin and structure reinforcements which support the outer skin. According to the invention, the structure reinforcements contain three-dimensional truss bending supports which extend over the area of light curvature and comprise first straps, which run close to the outer skin 9, and second straps, which run at a distance from the outer skin, and are connected to one another by coupling elements.
摘要翻译：飞机机身结构描述为飞翼飞机，具有轻微曲率的中心区域和较大曲率的侧面区域，其形成压力体并具有支撑外皮的外表皮和结构增强件。根据本发明，结构增强件包括在光弯曲区域上延伸的三维桁架弯曲支撑件，并且包括靠近外部皮肤9延伸的第一条带和与外部皮肤相距一定距离的第二条带并且通过耦合元件彼此连接。

10. 发明授权

US08156628B2 Holding device 有权
标题翻译：保持装置
公开(公告)号：US08156628B2
公开(公告)日：2012-04-17
申请号：US11959979
申请日：2007-12-19
申请人： Ingo Roth
发明人： Ingo Roth
IPC分类号： B23P19/00 , F16B7/10
CPC分类号： F16B21/16 , E05B47/0038 , E05B47/0045 , E05B65/006 , F16B5/01 , F16B5/0657 , F16B2001/0035 , Y10T24/45775 , Y10T29/49815 , Y10T29/49822 , Y10T29/49824 , Y10T292/0817 , Y10T292/438 , Y10T403/32475 , Y10T403/32483
摘要： A holding device for holding a structural component for aircraft to a further structural component; may be coupled to one of the components and is moved from a holding mode, where the first component is held to the second component by the holding device, to a release mode using a magnetic force. Furthermore, a method for deinstalling two components is disclosed, where carrying out deinstallation merely requires pressing a first component against a second component, and placing a magnetic key on or over one of the components in the region of the holding device, where at least some method-related steps may take place at substantially the same time.
摘要翻译：一种用于将飞机结构部件保持在另一结构部件上的保持装置; 可以耦合到其中一个部件，并且通过保持装置将第一部件保持到第二部件的保持模式移动到使用磁力的释放模式。此外，公开了一种用于卸载两个部件的方法，其中进行卸载仅需要将第一部件压靠在第二部件上，并且将磁性钥匙放置在保持装置的区域中的一个部件上或上方，其中至少一些方法相关的步骤可能在基本相同的时间进行。

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