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51. 发明授权

US07843201B2 Method of testing light metal parts, in particular aluminum components, which have been coated by anodising, in particular by TSA anodising 失效
标题翻译：通过阳极氧化涂覆的轻金属部件，特别是铝部件的测试方法，特别是通过TSA阳极氧化
公开(公告)号：US07843201B2
公开(公告)日：2010-11-30
申请号：US11983898
申请日：2007-11-13
申请人： Juergen Krueger
发明人： Juergen Krueger
IPC分类号： G01R27/08 , C25D5/00
CPC分类号： G01N33/20
摘要： A method of testing light metal parts, in particular aluminum components, which have been coated by anodizing, in particular by TSA anodizing, to determine whether they have been coated is described. According to the invention, the surface resistance of the surface of the component is measured and the surface coating of the component is classed as good when the surface resistance is higher than a prescribed high resistance value.
摘要翻译：描述了通过阳极氧化特别是通过TSA阳极氧化来涂覆的轻金属部件，特别是铝部件的方法，以确定它们是否被涂覆。根据本发明，测量部件表面的表面电阻，并且当表面电阻高于规定的高电阻值时，部件的表面涂层被分类为良好。

52. 发明申请

US20100294896A1 HOLDING DEVICE FOR MOUNTING PARTS INSTALLED INSIDE AN AIRCRAFT FUSELAGE 审中-公开
标题翻译：用于安装在飞机熔接内部的安装部件的保持装置
公开(公告)号：US20100294896A1
公开(公告)日：2010-11-25
申请号：US12763443
申请日：2010-04-20
申请人： Cihangir SAYILGAN
发明人： Cihangir SAYILGAN
IPC分类号： F16L3/08 , F16M13/02
CPC分类号： F16L3/233 , B64C1/406 , F16B21/073 , F16L3/137 , H02G3/30
摘要： A holding device for a mounting part installed inside an aircraft fuselage having a lining including an insulating mat, the holding device includes a fastening part attached to the aircraft fuselage and protruding through an opening in the insulating mat; a sealing disk; and a holding part configured to attach the mounting part and being disposed on an inner side of the aircraft fuselage and cooperating with the fastening part configured to attach the mounting part so as to simultaneously fix the insulating mat between the fastening part and the holding part, wherein the holding part extends through the opening in a sealed manner, and wherein a lower surface of the sealing disk contacts and seals an edge region of the opening when the holding part is installed on the fastening part.
摘要翻译：一种用于安装在具有包括绝缘垫的衬里的飞行器机身内的安装部分的保持装置，所述保持装置包括附接到飞机机身并通过绝缘垫中的开口突出的紧固部分; 密封盘; 以及保持部，其构造成安装所述安装部，并且设置在所述飞行器机身的内侧，并且与所述紧固部配合以构成为安装所述安装部，以将所述绝缘垫同时固定在所述紧固部与所述保持部之间，其中，所述保持部以密封方式延伸穿过所述开口，并且其中当所述保持部安装在所述紧固部上时，所述密封盘的下表面接触并密封所述开口的边缘区域。

53. 发明授权

US07837007B2 Sound-absorbing element for transport means, in particular for aircraft 有权
标题翻译：用于运输手段的吸音元件，特别是飞机
公开(公告)号：US07837007B2
公开(公告)日：2010-11-23
申请号：US11990861
申请日：2006-08-23
申请人： Stephan Hötzeldt , Malte Becker , Bernd Ohlendorf , Steffen Erfurth
发明人： Stephan Hötzeldt , Malte Becker , Bernd Ohlendorf , Steffen Erfurth
IPC分类号： G10K11/00 , F16F15/00 , E04B1/00 , E04B1/82 , E04B2/00 , E04C2/34
CPC分类号： B64C1/40 , B60R13/0815
摘要： A sound absorption element for means of transport, in particular for aircraft, comprising at least one sound absorption panel arranged on a base panel with the base panel comprising a multitude of recesses, in particular a hole grid or the like, for the transmission of sound.According to the invention, the sound absorption panels are each framed by a frame, wherein on the at least one frame at least in some sections a transition profile, in particular to prevent fatigue fractures due to stepwise changes of rigidity between the at least one frame and the base panel is arranged.Due to the base panel comprising a multitude of recesses, in particular comprising a hole grid, in connection with the sound absorption panels an air-permeable sound absorption element can be achieved.
摘要翻译：一种用于运输装置，特别是用于飞行器的吸声元件，包括布置在基座面板上的至少一个吸声板，其中底板包括多个凹槽，特别是孔网格等用于传播声音。根据本发明，吸声板各自由框架构成，其中在至少一个框架上至少在一些部分中具有过渡轮廓，特别是防止由于至少一个框架之间的刚性的逐步变化而引起的疲劳断裂并配置基板。由于基板包括多个凹部，特别是包括孔格栅，与吸声板相结合，可以实现透气的吸声元件。

54. 发明申请

US20100282937A1 MODULAR HOLDING DEVICE FOR MOUNTING PARTS LOCATED INSIDE AN AIRCAFT FUSELAGE 有权
标题翻译：用于安装位于机舱内的部件的模块化保持装置
公开(公告)号：US20100282937A1
公开(公告)日：2010-11-11
申请号：US12771081
申请日：2010-04-30
申请人： Martin Schnoor , Lueder Kosiankowski
发明人： Martin Schnoor , Lueder Kosiankowski
IPC分类号： F16M13/02
CPC分类号： H02G3/32
摘要： A holding device for a mounting part installed inside an aircraft fuselage includes an anchor plate configured to attach the holding device to a support rail of the aircraft fuselage and including at least one engagement section. The holding device further includes a holder module separably connected to the anchor plate and configured to fix the mounting part to the aircraft fuselage and having a hook section configured to postively engage the at least one engagement section so as to fasten the holder module to the anchor plate, and at least two clamping blocks disposed on the holder module.
摘要翻译：用于安装在飞行器机身内部的安装部件的保持装置包括：锚板，其构造成将保持装置附接到飞行器机身的支撑轨道并且包括至少一个接合部分。所述保持装置还包括保持器模块，所述保持器模块可分离地连接到所述锚板并且被构造成将所述安装部分固定到所述飞行器机身并且具有被配置为与所述至少一个接合部分接合的钩部分，以将所述保持器模块固定到所述锚板，以及设置在保持器模块上的至少两个夹紧块。

55. 发明申请

US20100279013A1 Painting device, painting arrangement, method for painting a curved surface of an object, and use of an inkjet device for painting an aircraft 有权
标题翻译：绘画装置，绘画装置，用于绘制物体的曲面的方法，以及使用用于喷涂飞行器的喷墨装置
公开(公告)号：US20100279013A1
公开(公告)日：2010-11-04
申请号：US12800271
申请日：2010-05-12
申请人： Eckart Frankenberger , Thorsten Bergemann , Heinz-Detlef Naeve
发明人： Eckart Frankenberger , Thorsten Bergemann , Heinz-Detlef Naeve
IPC分类号： B05D5/00 , B05D1/36
CPC分类号： B05B13/0405
摘要： A painting device for painting a curved surface (102) of an object (101), with a paint material ejection device (103), with a guide device (104, 105) and with a control device. The paint material ejection device (103) is designed for ejecting paint material. By means of the guide device (104, 105) the paint material ejection device (103) can be mechanically guided along a curved surface of an object. By means of the control device the paint material ejection device (103) and the guide device (104, 105) can be controlled in such a way that by means of guiding the paint material ejection device (103) along a predefinable path and by means of predefinable ejection of paint from the paint material ejection device (103) along the predefinable path a curved surface (102) of an object (101) to be painted can be painted.
摘要翻译：一种用涂料（101）的弯曲表面（102）和涂料输出装置（103），用导向装置（104,105）和控制装置进行涂装的涂装装置。涂料排出装置（103）被设计用于喷射涂料。通过引导装置（104,105），可以沿着物体的弯曲表面机械地引导涂料材料排出装置（103）。通过控制装置，可以以这样的方式控制涂料材料排出装置（103）和引导装置（104,105），即通过沿着可预定路径引导涂料输出装置（103）可以从涂料输出装置（103）沿着可预定路径预先喷射涂料，可以涂漆待涂漆的物体（101）的弯曲表面（102）。

56. 发明申请

US20100267323A1 Method For Controlling The Temperature Of Feed Air Injected Into The Cabin Zone Of A Passenger Aircraft 有权
标题翻译：用于控制进入客机客舱区域的进料空气温度的方法
公开(公告)号：US20100267323A1
公开(公告)日：2010-10-21
申请号：US12824898
申请日：2010-06-28
申请人： Thomas Scherer , Michael Markwart , Torsten Schwan
发明人： Thomas Scherer , Michael Markwart , Torsten Schwan
IPC分类号： B64D13/08 , B64D13/00
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y10S62/05
摘要： With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.
摘要翻译：使用一种用于控制喷射到客机的客舱区域中的进料空气的温度的方法，其将舱室分成几个舱区，分别提供特别温度控制的进料空气，喷射进料的温度根据喷射温度最佳值，根据传感器测量的注入到所述舱室区域的进料空气的喷射温度实际值的偏差，对每个舱室进行空气控制。如果对于客舱区域没有或至少没有可用的该舱室区域的环境温度读数，则可以根据变化确定该舱区域的喷射温度的最佳值，由此根据喷射温度最佳值和/或其他舱区的喷射温度实际值的基础，由此由客舱温度的传感器进行的测量可靠地工作。根据另一个变化，可以建立客舱区域的喷射温度最佳值，而不需要通过传感器测量环境温度，或者不会从对飞行器的外部环境测量的温度可靠地测量环境温度。

57. 发明申请

US20100243814A1 Emergency Evacuation System, in Particular for a Tailless Aeroplane 失效
标题翻译：紧急疏散系统，特别是无尾飞机
公开(公告)号：US20100243814A1
公开(公告)日：2010-09-30
申请号：US11992274
申请日：2006-09-14
申请人： André Anger , Wolfram Schöne
发明人： André Anger , Wolfram Schöne
IPC分类号： B64C1/22 , A62B1/20
CPC分类号： B64C39/10 , B64C2039/105 , B64D25/08 , B64D25/14
摘要： A device for selective emergency evacuation of persons from a first level to a second level situated above the first level, or to a third level situated below the first level. For evacuation to the second level a stair arrangement is provided. One end of the device is connected to the first level while the other end is displaceable between the second level and the third level or vice versa. For evacuation to the third level, the device is changeable to a slide. The device may provide for emergency evacuation of persons from a first level deck, or passenger deck of a blended wing-body aircraft, selectively to the top, second level of the aircraft, or to the bottom third level of the aircraft.
摘要翻译：一种用于选择性地将人员从第一级升级到位于第一级以上的第二级或第一级以下的第三级别的装置。为了撤离到第二级，提供了一个楼梯安排。设备的一端连接到第一级，而另一端可在第二级和第三级之间移位，反之亦然。为了撤离到第三级，设备可以更改为幻灯片。该装置可以选择性地向飞机的顶部，第二级或飞机的底部第三级的第一级甲板或混合翼体飞机的乘客甲板紧急撤离人员。

58. 发明授权

US07803453B2 Laminated structure and method for producing a laminated structure 有权
标题翻译：叠层结构及其制造方法
公开(公告)号：US07803453B2
公开(公告)日：2010-09-28
申请号：US11749935
申请日：2007-05-17
申请人： Uwe Steinke
发明人： Uwe Steinke
IPC分类号： B32B27/00
CPC分类号： B32B1/00 , B32B15/08 , B32B15/14 , B32B15/18 , B32B15/20 , B32B2262/0269 , B32B2262/062 , B32B2262/101 , B32B2262/106 , B32B2307/554 , B32B2307/734 , B32B2605/18 , B64C1/12 , B64C2001/0072 , Y02T50/43 , Y10T428/24942 , Y10T428/26 , Y10T428/31504
摘要： A method for producing a laminated structure, where the method comprises the forming of a primary laminated structure from a plurality of layers; and the forming of an additional layer, the additional layer comprising an erosion-resistant material, on the primary laminated structure. In addition, such a laminated structure is disclosed.
摘要翻译：一种叠层结构体的制造方法，其特征在于，所述方法包括：从多层形成初级层压结构体; 并且在初级层压结构上形成附加层，该附加层包括抗侵蚀材料。此外，公开了这种层叠结构。

59. 发明授权

US07789085B2 Presentation arrangement for an oxygen mask or a pull flag 有权
标题翻译：用于氧气面罩或拉旗的展示布置
公开(公告)号：US07789085B2
公开(公告)日：2010-09-07
申请号：US11355675
申请日：2006-02-16
申请人： Thomas Vogt
发明人： Thomas Vogt
IPC分类号： A62B18/08
CPC分类号： B64D11/00 , B64D2231/025
摘要： A presentation arrangement for presenting an oxygen mask or pull flag including an inflatable lever wherein for presenting the oxygen mask or pull flag at a preset first location, the inflatable lever is inflated such that the oxygen mask or pull flag is located at the first location.
摘要翻译：一种呈现装置，用于呈现包括可充气杆的氧气面罩或拉旗，其中为了在预设的第一位置呈现氧气面罩或拉旗，充气杆被充气，使得氧气面罩或拉片标志位于第一位置。

60. 发明授权

US07788966B2 Device and method to diagnose vacuum systems 有权
标题翻译：诊断真空系统的装置和方法
公开(公告)号：US07788966B2
公开(公告)日：2010-09-07
申请号：US11627178
申请日：2007-01-25
申请人： Hannes Mueller , Wilhelm Lutzer , Marc Scheel
发明人： Hannes Mueller , Wilhelm Lutzer , Marc Scheel
IPC分类号： G01M3/02
CPC分类号： E03F1/006 , B64F5/60
摘要： A device to diagnose a vacuum system comprises a pipe with a first opening that can be closed by a hingable cover, and a second opening that is designed to establish a pressure-proof connection to the vacuum system. The diagnostic device may be operated in a volume-flow mode in which the cover is open in order to determine a volume flow in the base body, and in a negative-pressure mode in which the cover is closed so as to allow to draw conclusions about the available pressure difference.
摘要翻译：用于诊断真空系统的装置包括具有可由可铰接盖封闭的第一开口的管道和被设计成建立与真空系统的耐压连接的第二开口。诊断装置可以在其中盖打开的体积流动模式下操作，以便确定基体中的体积流量，并且在封闭盖的负压模式中，以便得出结论关于可用的压力差。

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