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41. 发明授权

US07883056B2 Insulation arrangement for the internal insulation of a vehicle 有权
标题翻译：车辆内部绝缘的绝缘布置
公开(公告)号：US07883056B2
公开(公告)日：2011-02-08
申请号：US10596418
申请日：2005-01-05
申请人： Rainer Mueller , Peter Turanski , Wilko Oestereich , Thorsten Reinelt
发明人： Rainer Mueller , Peter Turanski , Wilko Oestereich , Thorsten Reinelt
IPC分类号： B64C1/40
CPC分类号： B64C1/40 , Y10T428/234
摘要： The present invention relates to an insulation structure for the internal insulation of a vehicle. The insulation structure is improved in such a way that using it a fire incursion of the flames of a source of fire acting from outside the vehicle environment into the vehicle interior is excluded as much as possible, an increase of the fire protection safety for separate interior regions lying proximal to a structure external skin being implemented by the type of the film insulation of the insulation package. The insulation structure comprises an insulation package (3), in which an insulation core (1) is embedded, and a film (11). The insulation package (3) is positioned inside an intermediate space which encloses internal paneling and an external skin. It is completely enclosed by the film (11). The film (11) is implemented using a burn-through safe film material, which is an obstruction to a flaming fire, to which a film surface region of this film is subjected during an occurring fire catastrophe.
摘要翻译：本发明涉及一种用于车辆内部绝缘的绝缘结构。绝缘结构的改进使得使用火焰从车辆环境外部到达车辆内部的火源起火被排除在尽可能之外，增加了对于单独内部的防火安全性通过绝缘包装的膜绝缘体的类型来实现靠近结构外皮的区域。绝缘结构包括其中嵌入绝缘芯（1）的绝缘封装（3）和薄膜（11）。绝缘包装（3）位于包围内部镶板和外部皮肤的中间空间的内部。它被电影（11）完全包围。胶片（11）使用穿透安全膜材料来实现，该烧穿安全膜材料是在发生的火灾灾难期间该膜的膜表面区域经受的火焰的阻塞。

42. 发明授权

US07880636B2 Information display system for aircraft 有权
标题翻译：飞机信息显示系统
公开(公告)号：US07880636B2
公开(公告)日：2011-02-01
申请号：US11571513
申请日：2005-06-27
申请人： Detlef Heym
发明人： Detlef Heym
IPC分类号： G08B5/22
CPC分类号： B64D11/00153 , B64D11/0015 , B64D2011/0038 , G09F19/18 , Y02T50/46
摘要： In current passenger aircraft, signs are used to represent specific information, which reproduce the information as writing or a pictogram. According to one exemplary embodiment of the present invention, an information display system for aircraft is specified, comprising a light source, a projection unit, and a housing. For this purpose, according to one exemplary embodiment of the present invention, the projection unit is implemented in the form of a liquid crystal display, so that, in combination with a high-performance light-emitting diode and a suitable lens, static and dynamic information may be presented on arbitrarily shaped projection surfaces. The flexibility of the onboard information display is thus advantageously increased.
摘要翻译：在目前的客机中，标志用于表示特定信息，以信件形式或象形图复制信息。根据本发明的一个示例性实施例，指定用于飞行器的信息显示系统，包括光源，投影单元和壳体。为此，根据本发明的一个示例性实施例，投影单元以液晶显示器的形式实现，使得与高性能发光二极管和合适的透镜结合，静态和动态信息可以呈现在任意形状的投影表面上。因此有利地增加了车载信息显示的灵活性。

43. 发明授权

US07874523B2 Method of controlling an aircraft in flight, especially to reduce wake vortices 有权
标题翻译：控制飞行中的飞机的方法，特别是减少尾涡
公开(公告)号：US07874523B2
公开(公告)日：2011-01-25
申请号：US11486911
申请日：2006-07-14
申请人： Florent Laporte , Heinz Hansen
发明人： Florent Laporte , Heinz Hansen
IPC分类号： B64C23/06
CPC分类号： B64C23/06 , Y02T50/162
摘要： The flight of an aircraft is controlled by controlling the aircraft propulsion thrust and adjusting aerodynamic control elements so that the aircraft flies along a specified flight path. In order to reduce wake vortices generated by and trailing behind the aircraft, a wake vortex parameter is determined as a function of a spoiler deflection, and a spoiler element is adjusted to a spoiler deflection value in an optimum range in which the spoiler influence on the wake vortex parameter is maximized and the spoiler influence on the aircraft performance is at its lowest level for achieving that maximum spoiler influence on the wake vortex parameter.
摘要翻译：飞机的飞行通过控制飞机推进推力和调整空气动力学控制元件来控制，使飞机沿着指定的飞行路线飞行。为了减少由飞行器产生和尾随飞行器的尾流涡流，尾涡流参数被确定为扰流器偏转的函数，并且扰流器元件被调节到扰流器对扰动器偏转的影响的最佳范围内的扰流板偏转值尾涡流参数最大化，扰流板对飞机性能的影响处于最低水平，以实现最大扰流器对尾涡流参数的影响。

44. 发明申请

US20110006778A1 TESTER FOR TESTING OPERATIONAL RELIABILITY OF A COCKPIT OXYGEN DISTRIBUTION CIRCUIT 有权
标题翻译：测试氧化铁分布电路的运行可靠性测试仪
公开(公告)号：US20110006778A1
公开(公告)日：2011-01-13
申请号：US12745484
申请日：2007-11-29
申请人： Guenther Kruse
发明人： Guenther Kruse
IPC分类号： G01R31/02
CPC分类号： A62B27/00
摘要： The present invention relates to a tester (100) for testing operational reliability of a cockpit oxygen distribution circuit (1) having a plurality of components (20, 30, 40, 50) ensuring supply of oxygen from the cockpit oxygen distribution circuit (1) to a cockpit crew of an aircraft in an emergency situation. The tester (100) comprises means (20′, 30′, 40′, 500 for electrically connecting the tester (100), in place of at least one of the components (20, 30, 40, 50), to the cockpit oxygen distribution circuit (1), an indicator (120) for indicating that the electrical connection of the tester (100) to the cockpit oxygen distribution circuit (1) has been established in a predefined manner, and switching means (RL1, RL2, RL3, RL4) for initiating an output signal of the tester (100), wherein the output signal is indicative of an operating condition of the component (20, 30, 40, 50) when being connected to the cockpit oxygen distribution circuit (1). The invention further relates to the use of such a tester (100) and a method for testing operational reliability of a cockpit oxygen distribution circuit (1).
摘要翻译：本发明涉及一种用于测试驾驶舱氧气分配回路（1）的操作可靠性的测试器（100），该驾驶舱氧气分配回路（1）具有确保从驾驶舱氧气分配回路（1）供应氧气的多个部件（20,30,40,50）在紧急情况下飞机的驾驶舱。测试器（100）包括用于将测试器（100）电气连接到代替至少一个部件（20,30,40,50）的装置（20'，30'，40'，500）到驾驶舱氧气分配电路（1），用于指示测试器（100）与驾驶舱氧分配电路（1）的电连接已经以预定方式建立的指示器（120），以及切换装置（RL1，RL2，RL3， RL4），用于启动测试器（100）的输出信号，其中当连接到驾驶舱氧气分配回路（1）时，输出信号表示组件（20,30,40,50）的操作状态。本发明还涉及这种测试器（100）的使用和用于测试驾驶舱氧气分配回路（1）的操作可靠性的方法。

45. 发明授权

US07866928B2 Plug and method for fixing at least two devices 有权
标题翻译：用于固定至少两个设备的插头和方法
公开(公告)号：US07866928B2
公开(公告)日：2011-01-11
申请号：US11832882
申请日：2007-08-02
申请人： Guenter Schmitz
发明人： Guenter Schmitz
IPC分类号： F16B13/06
CPC分类号： F16B2/185 , Y10T24/44026 , Y10T403/591 , Y10T403/75
摘要： A plug and a method for fixing at least two devices, includes a tension element, a pin, a lever element and a compression element. In one example, the tension element includes a tension stamp on a first end and a coupling member on a second end and a lever element includes a first sliding and a coupling element, with the pin coupling the lever element with the tension element. A compression element having an area-shaped contact that is capable of sliding onto the tension element until the area-shaped contact contacts the tension stamp. When the lever element is coupled to the tension element by a pin and is engaged by using a lever movement, a compression element is compressed by shortening a distance between the tension stamp and the lever element.
摘要翻译：用于固定至少两个装置的插头和方法包括张紧元件，销，杠杆元件和压缩元件。在一个示例中，张紧元件包括在第一端上的张紧印模和在第二端上的联接构件，并且杠杆元件包括第一滑动件和联接元件，销钉将杠杆元件与张力元件连接。具有能够滑动到张力元件上的区域形状的接触件的压缩元件，直到该区域形状的接触件接触张紧印模。当杠杆元件通过销联接到张紧元件并且通过使用杠杆运动而接合时，压缩元件通过缩短张紧印模和杠杆元件之间的距离而被压缩。

46. 发明申请

US20110003218A1 Device, Method and System for Producing Thermal and/or Kinetic and Electrical Energy 审中-公开
标题翻译：用于生产热和/或动能和电能的装置，方法和系统
公开(公告)号：US20110003218A1
公开(公告)日：2011-01-06
申请号：US12293468
申请日：2007-03-20
申请人： Ralf-Henning Stolte , Martin Saballus
发明人： Ralf-Henning Stolte , Martin Saballus
IPC分类号： H01M8/06
CPC分类号： H01M8/0606 , F02M25/12 , H01M8/0662 , Y02T10/121
摘要： The present concerns an apparatus (5, 105) for energy production from a hydrocarbon mixture (15) having at least one dehydrogenatable compound, in particular from a hydrocarbon-based fuel, preferably from kerosene, comprising a tank (10, 110) for providing the hydrocarbon mixture (15), and a combustion machine (20, 120) connected to the tank (10, 110) for combustion of hydrocarbons for producing thermal and/or kinetic energy (25, 125, 30, 130). To provide such an apparatus (5, 105), a corresponding method and a corresponding system in which thermal, kinetic and electrical energy (25, 125, 30, 130, 55, 155) is efficiently produced it is proposed that the apparatus (5, 105) further comprises a separating device (35, 135) for at least partially separating the at least one dehydrogenatable compound from the hydrocarbon mixture (15), dehydrogenating means (40, 140) for producing hydrogen from the separated dehydrogenatable compound by dehydrogenation, first feed means (45, 145) for directly or indirectly feeding the dehydrogenated compound to the combustion machine (20, 120), and a fuel cell (50, 150) for producing electrical energy (55, 155), with reaction of the hydrogen obtained.
摘要翻译：本发明涉及一种用于从具有至少一种可脱氢化合物，特别是烃类燃料，优选煤油的烃混合物（15）产生能量的装置（5,105），该装置包括一个罐（10,110），用于提供烃混合物（15）和连接到罐（10,110）上用于燃烧碳氢化合物以产生热能和/或动能（25,125,30，130）的燃烧机（20,120）。为了提供这样的装置（5,105），有效地产生热，动能和电能（25,125,30，130,55,155）的相应方法和相应的系统，建议装置（5 ，105）还包括用于至少部分地从所述烃混合物（15）分离所述至少一种可脱氢化合物的分离装置（35,135），用于通过脱氢从所分离的可脱氢化合物产生氢的脱氢装置（40,140）用于直接或间接地将脱氢化合物供给到燃烧机（20,120）的第一进料装置（45,145）和用于产生电能（55,155）的燃料电池（50,150），通过氢获得。

47. 发明授权

US07856884B2 Method for performing a ground vibration test in airplanes 有权
标题翻译：在飞机上进行地面振动试验的方法
公开(公告)号：US07856884B2
公开(公告)日：2010-12-28
申请号：US12107516
申请日：2008-04-22
申请人： Detlef Schierenbeck
发明人： Detlef Schierenbeck
IPC分类号： B06B3/00
CPC分类号： G01N29/045 , G01M7/00 , G01N29/4463 , G01N2291/2694
摘要： The invention relates to an improved method for a ground vibration test (so-called “ground vibration test”) on an airplane. In the method according to the invention, the airplane is jacked up essentially undamped (“rigidly”) in conventional holding points with lifting devices. For purposes of the ground vibration test, the airplane is then excited to vibrate in a known manner using a plurality of vibration exciters, and the vibrations are acquired with a plurality of measuring transducers, in particular accelerometers. A dynamic vibration model of the airplane theoretically calculated beforehand can here be adjusted. The boundary conditions are removed during or after the ground vibration test, meaning the influence of the lifting device is “mathematically canceled out”, so that the determined measured values reflect the so-called “free-free” state of the airplane, as if the airplane had actually been in free flight during the ground vibration tests.
摘要翻译：本发明涉及一种用于飞机上的地面振动试验（所谓的“地面振动试验”）的改进方法。在根据本发明的方法中，在具有提升装置的常规保持点中，飞机基本上无阻尼地（“刚性地”）地被顶起。为了地面振动试验的目的，飞机然后被激励以已知的方式使用多个振动激励器振动，并且用多个测量换能器，特别是加速度计获取振动。理论上预先计算的飞机的动态振动模型可以在这里进行调整。边界条件在地面振动试验期间或之后被去除，这意味着提升装置的影响“数学上被抵消”，使得确定的测量值反映了飞机所谓的“自由”状态，好像飞机在地面振动试验中实际上已经进入自由飞行。

48. 发明授权

US07850209B2 Tube assembly and tube assembly system having such tube assemblies 有权
标题翻译：具有这种管组件的管组件和管组件系统
公开(公告)号：US07850209B2
公开(公告)日：2010-12-14
申请号：US11769426
申请日：2007-06-27
申请人： Wilhelm Lutzer , Marc Scheel , Christian Wildhagen , Thorsten Otto
发明人： Wilhelm Lutzer , Marc Scheel , Christian Wildhagen , Thorsten Otto
IPC分类号： F16L27/00
CPC分类号： F16L27/0849 , F16L27/12
摘要： The invention relates to a tube assembly for connecting a first tube to a second tube, wherein a connection end of the first tube and a connection end of the second tube form a swivel joint, a rotational axis of the swivel joint and a tube axis of the first and the second tube form an angle α, and the first tube is rotatable relative to the second tube in the region of between 0° and 2α.
摘要翻译：本发明涉及一种用于将第一管连接到第二管的管组件，其中第一管的连接端和第二管的连接端形成旋转接头，旋转接头的旋转轴线和管轴线第一管和第二管形成角度α，并且第一管可以在0°和2α之间的相对于第二管旋转。

49. 发明授权

US07850118B2 Structural element, method for manufacturing a structural element and use of a structural element for an aircraft hull 有权
标题翻译：结构元件，制造结构元件的方法和飞机机身的结构元件的使用
公开(公告)号：US07850118B2
公开(公告)日：2010-12-14
申请号：US11290042
申请日：2005-11-29
申请人： Alexei Vichniakov
发明人： Alexei Vichniakov
IPC分类号： B64C1/00
CPC分类号： B64C1/06 , B64C1/12 , B64C2001/0081 , Y02T50/42 , Y10T428/24174
摘要： A structural element includes the following elements: a carrier element, a reinforcing element, and a sheathing element. At least a portion of the reinforcing element is enveloped by the sheathing element and the reinforcing element is embedded in the carrier element. Materials of the elements are selected to inhibit crack initiation or propagation in the elements and/or from one element to another. An intermediate layer of a different material may be added between elements to further inhibit crack initiation and propagation and to inhibit corrosion, such as galvanic corrosion.
摘要翻译：结构元件包括以下元件：载体元件，加强元件和护套元件。增强元件的至少一部分被护套元件包围，并且加强元件嵌入载体元件中。选择元件的材料以抑制元件和/或从一个元件到另一个元件的裂纹开始或传播。可以在元件之间添加不同材料的中间层，以进一步抑制裂纹的产生和扩展，并抑制诸如电偶腐蚀的腐蚀。

50. 发明授权

US07850117B2 Fuselage structure 有权
标题翻译：机身结构
公开(公告)号：US07850117B2
公开(公告)日：2010-12-14
申请号：US11811364
申请日：2007-06-07
申请人： Daniela Lohwasser , Sven Werner , Andreas Behr , Christian Frank , Marco Pacchione , Axel Bonde , Christian Kulik
发明人： Daniela Lohwasser , Sven Werner , Andreas Behr , Christian Frank , Marco Pacchione , Axel Bonde , Christian Kulik
IPC分类号： B64C1/00
CPC分类号： B64C1/068 , B64C1/12 , B64C2001/0081 , F16B5/08
摘要： A fuselage structure comprises a plurality of elements that in longitudinal direction are interconnected by weld joints; a plurality of circumferential ribs that are connected to the plurality of elements and that extend so as to be substantially perpendicular in relation to the longitudinal direction of the elements; and a plurality of clips that are arranged between the elements and the ribs such that said clips do not cover the respective weld joints.
摘要翻译：机身结构包括沿纵向方向通过焊接接头相互连接的多个元件; 多个周向肋，其连接到所述多个元件并且相对于所述元件的纵向方向基本垂直地延伸; 以及布置在元件和肋之间的多个夹子，使得所述夹子不覆盖相应的焊接接头。

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