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51. 发明申请

US20100294564A1 CABLE GUIDING ARRANGEMENT FOR A CABLEFORM INSIDE AN AIRCRAFT CABIN 有权
标题翻译：用于航空仓库内的电缆的电缆导向装置
公开(公告)号：US20100294564A1
公开(公告)日：2010-11-25
申请号：US12762104
申请日：2010-04-16
申请人： Hans-Peter GUTHKE , Lueder KOSIANKOWSKI
发明人： Hans-Peter GUTHKE , Lueder KOSIANKOWSKI
IPC分类号： H02G3/04 , H01B7/00
CPC分类号： H02G3/32 , H02G3/0456
摘要： A cable guiding arrangement for at least one electrical cable harness installed in an aircraft cabin includes a guide rail having at least one receiving pocket and an attachment surface configured to receive the at least one cable harness; a plurality of retaining heads spaced apart from each other in a longitudinal direction along the guide rail and configured to affix the at least one electrical cable harness; and at least one insertion element disposed on an edge of the guide rail configured to attach at least one laterally branching-off cable of the at least one cable harness, the at least one insertion element including at least one retaining head section and an insertion section, wherein the insertion section is disposed in the at least one receiving pocket.
摘要翻译：用于安装在飞行器机舱中的至少一根电缆线束的电缆导引装置包括具有至少一个接收凹部和被配置为接纳所述至少一个电缆线束的附接表面的导轨; 多个保持头沿着导轨沿纵向方向彼此间隔开并且构造成固定至少一个电缆线束; 以及设置在所述导轨的边缘上的至少一个插入元件，其构造成附接所述至少一个电缆线束的至少一个横向分支电缆，所述至少一个插入元件包括至少一个保持头部分和插入部分，其中所述插入部分设置在所述至少一个接收口袋中。

52. 发明授权

US07837237B2 Quick connector with bayonet locking 有权
标题翻译：带卡口锁的快速接头
公开(公告)号：US07837237B2
公开(公告)日：2010-11-23
申请号：US12088609
申请日：2006-09-14
申请人： Werner Passlack
发明人： Werner Passlack
IPC分类号： F16L37/244 , F16L37/248 , F16L37/252
CPC分类号： F16L37/252 , Y10S285/901
摘要： A combination of two bodies having tube-shaped or sleeve-shaped connecting sections which can be plugged into one another as part of an air-conditioning line system in an aircraft, the combination including at least one radial locking projection on a first body, at least one locking clearance on a second body which is completely surrounded by a rim, at least one lead-in clearance which is angularly offset in the peripheral direction in relation to the appertaining locking clearance, and at least one releasing groove associated with each locking clearance and disposed angularly offset in the peripheral direction on the opposite side of the appertaining lead-in clearance.
摘要翻译：具有管状或套筒形连接部分的两个主体的组合，其可以彼此插入，作为飞行器中的空调线路系统的一部分，该组合包括在第一主体上的至少一个径向锁定突起至少一个由轮缘完全包围的第二主体上的锁定间隙，至少一个与周围方向成角度偏移的导入间隙相对于所述锁定间隙有角度偏移，以及与每个锁定间隙相关的至少一个释放槽并且在周向方向上在相应的引入间隙的相对侧上成角度地偏移。

53. 发明授权

US07832686B2 Combined displacement and swivel mechanism 有权
标题翻译：组合位移和旋转机构
公开(公告)号：US07832686B2
公开(公告)日：2010-11-16
申请号：US11466683
申请日：2006-08-23
申请人： Johann Konrad Erben , Jan Wijnia
发明人： Johann Konrad Erben , Jan Wijnia
IPC分类号： B64C1/14
CPC分类号： B64C1/1423 , B64C1/14 , B64C1/1415 , Y10T16/547 , Y10T16/5476
摘要： The present application relates to a specially designed hinge mechanism (4) which makes it possible to construct an aircraft door (2) that can be fitted in a fuselage (3) so as to be displaceable and swivellable on the fuselage (3). Furthermore, the invention relates to an aircraft door (2) comprising at least one such hinge mechanism (4) designed in this way, to a fuselage (3) with at least one aircraft door (2) that is linked to at least one hinge mechanism (4), designed in this way, on the fuselage (3), as well as to the use of at least one hinge mechanism (4) for installation of an aircraft door (2) on a fuselage (3). The hinge mechanism (4) essentially comprises a displacement mechanism (5, 6) as well as a telescopic scissor-type mechanism (7-12). The displacement mechanism (5, 6) can be linked to an aircraft door (2) and is kinematically designed such that as a result of its activation the aircraft door (2) can be displaced from its home position in the direction of the fuselage (3). The scissor-type mechanism (7-12) can be linked to a fuselage (3) and is kinematically designed such that as a result of its activation the aircraft door (2) is displaceable from the fuselage (3) to a final position, on a polar axis that is aligned perpendicularly in the direction of displacement.
摘要翻译：本申请涉及一种专门设计的铰链机构（4），其可以构造可装配在机身（3）中以便在机身（3）上可移动和可转动的飞机门（2）。此外，本发明涉及一种飞机门（2），其包括至少一个以这种方式设计的这种铰链机构（4）到具有至少一个飞机门（2）的机身（3），所述至少一个飞机门（2）连接到至少一个铰链机身（4），这样设计在机身（3）上，以及使用至少一个铰链机构（4）用于在机身（3）上安装飞机门（2）。铰链机构（4）基本上包括位移机构（5,6）以及伸缩式剪式机构（7-12）。位移机构（5,6）可以连接到飞行器门（2）并被运动学设计，使得由于其启动，飞行器门（2）可以在机身方向上从其起始位置移位（ 3）。剪刀式机构（7-12）可以与机身（3）连接，并被运动学设计，使得由于其激活，飞机门（2）可从机身（3）移动到最终位置，在垂直于位移方向对齐的极轴上。

54. 发明授权

US07823834B2 Door configured to close an opening inside an aircraft 有权
标题翻译：关闭飞机内的开口的门
公开(公告)号：US07823834B2
公开(公告)日：2010-11-02
申请号：US11195749
申请日：2005-08-03
申请人： Clive French , Smail Maksen
发明人： Clive French , Smail Maksen
IPC分类号： B64C1/14
CPC分类号： B64C1/1469 , B64C2001/009 , B64D45/0015
摘要： This door includes a device that permits air to flow through the door in one direction but prevents this flow of air in the opposite direction.On the attached illustration, the door includes at least a window (74), that less air pass through as well as an elastic membrane (76) covering window (74).Elastic membrane (76) includes on the one hand an area that is airtight facing window (74) and capable of fully covering it and on the other hand, an area that is pervious to air near the impervious area.
摘要翻译：该门包括允许空气在一个方向上流过门的装置，但防止空气沿相反方向流动。在附图中，门包括至少一个窗口（74），较少的空气通过，以及覆盖窗口（74）的弹性膜（76）。弹性膜（76）一方面包括面向气密的窗（74）并能够完全覆盖的区域，另一方面包括在不渗透区域附近透过空气的区域。

55. 发明授权

US07808251B2 Method and apparatus for determining an interfering field strength in an aircraft 有权
标题翻译：用于确定飞行器中的干扰场强的方法和装置
公开(公告)号：US07808251B2
公开(公告)日：2010-10-05
申请号：US11970496
申请日：2008-01-07
申请人： Heinz-Wolfgang Krueger , Ralf Marcordes
发明人： Heinz-Wolfgang Krueger , Ralf Marcordes
IPC分类号： G01R27/28
CPC分类号： G01R29/0814 , H04B5/0018 , H04B17/345 , H05K9/0069
摘要： The disclosed embodiments relates to a method and an apparatus for determining the interfering field strength in an aircraft and the impairment of an electric system in the aircraft including cables between the outer shell and the interior panelling of the fuselage for transmitting signals within the aircraft. In order to enable direct and reliable determination of interfering field strength in an aircraft and assessment of the electromagnetic vulnerability of the communications system in the aircraft depending on the results of the determination, either a predetermined transmission signal is fed in at least one leaky line between outer shell and panelling of the fuselage and the reception signal that is irradiated by the leaky line is received with a receiver, or a predetermined transmission signal is transmitted with a transmitter and the reception signal is extracted from the leaky line. Subsequently the amplitudes of the transmission and the reception signals are compared with each other.
摘要翻译：所公开的实施例涉及用于确定飞行器中的干扰场强的方法和装置以及飞行器中的电气系统的损伤，包括用于在飞行器内传输信号的机身的外壳和内部镶板之间的电缆。为了能够直接和可靠地确定飞行器中的干扰场强，以及根据确定结果评估飞行器中的通信系统的电磁脆弱性，或者将预定的传输信号送入至少一条泄漏线之间，机身的外壳和镶板以及由泄漏线照射的接收信号被接收器接收，或者用发送器发送预定的发送信号，并且从泄漏线提取接收信号。随后将发送和接收信号的幅度相互比较。

56. 发明授权

US07807315B2 Rotable fuel cell system 有权
标题翻译：可旋转燃料电池系统
公开(公告)号：US07807315B2
公开(公告)日：2010-10-05
申请号：US11225589
申请日：2005-09-13
申请人： Claus Hoffjann , Hansgeorg Schuldzig , Hans-Juergen Heinrich
发明人： Claus Hoffjann , Hansgeorg Schuldzig , Hans-Juergen Heinrich
IPC分类号： H01M8/02 , H01M8/04
CPC分类号： H01M8/04291 , H01M8/00 , H01M8/004 , H01M8/0258 , H01M8/0267 , H01M8/04007 , H01M8/04059 , H01M8/04089 , H01M8/04111 , H01M8/04156 , H01M8/2475 , H01M2008/1095 , H01M2250/20 , Y02T90/32
摘要： For operation, PEMFCs require among other things a compressor for the cathode air, and a system for removing the water which is generated on the cathode side as a result of the electrochemical reaction. According to an embodiment of the present invention the removal of water is supported in that the fuel cell is made to rotate by way of an electric motor so that the water contained in the cathodes of the fuel cell can be extracted by centrifugal force. To this effect the air channels on the cathode side are arranged so as to extend radially or in a spiral shape from the inside towards the outside. In this way the efficiency of the fuel cell can be significantly improved.
摘要翻译：为了操作，PEMFC需要用于阴极空气的压缩机，以及用于去除由于电化学反应而在阴极侧产生的水的系统。根据本发明的一个实施方案，水的除去被支撑，因为燃料电池通过电动机旋转，使得包含在燃料电池的阴极中的水可以通过离心力提取。为此，阴极侧的空气通道被布置成从内向外径向或螺旋形地延伸。以这种方式，可以显着提高燃料电池的效率。

57. 发明授权

US07802732B2 Device and process for temperature regulation of sections of the interior of an aircraft 有权
标题翻译：飞机内部部分温度调节的装置和过程
公开(公告)号：US07802732B2
公开(公告)日：2010-09-28
申请号：US10582570
申请日：2004-12-30
申请人： Thomas Scherer , Torsten Schwan , Georg Mühlthaler , Jan Dittmar
发明人： Thomas Scherer , Torsten Schwan , Georg Mühlthaler , Jan Dittmar
IPC分类号： F24F11/00 , F24F7/00 , F24F3/00 , F24D19/10
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y02T50/44
摘要： A device for temperature regulation of sections of the interior of an aircraft includes a controlled mixer valve for the mixing of engine bleed air and air that is cooler than the engine bleed air in order to obtain pre-tempered mixed air flowing out of the mixer valve; a distribution line connected to the outlet of the mixer valve which is connected to the respective sections by at least two supply lines; individual heating units assigned to the respective sections; sensors assigned to the individual sections for the respective actual temperatures; transmitters for the respective nominal temperatures; and a regulator unit which controls the mixer valve dependent upon the respective nominal temperatures and the respective actual temperatures in the individual areas.
摘要翻译：用于飞行器内部的部分温度调节的装置包括用于混合发动机排出空气和比发动机放气更冷的空气的受控混合器阀，以获得从混合器阀流出的预调温混合空气 ; 连接到混合器阀的出口的分配线，其通过至少两条供应管线连接到各个部分; 分配给各个部分的各个加热单元; 分配给相应实际温度的各个部分的传感器; 发射机相应的标称温度; 以及调节器单元，其根据相应的标称温度和各个区域中的相应实际温度来控制混合器阀。

58. 发明授权

US07785694B2 Panel arrangement for an interior lining of a passenger cabin in an aircraft 有权
标题翻译：飞机上客舱内衬的面板布置
公开(公告)号：US07785694B2
公开(公告)日：2010-08-31
申请号：US10596981
申请日：2005-01-05
申请人： Rainer Müller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
发明人： Rainer Müller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
IPC分类号： B32B3/12 , B32B5/16
CPC分类号： B64C1/40 , A62C2/06 , A62C3/08 , A62C8/06 , A62C8/08 , B64C1/067 , Y10S428/92 , Y10S428/921 , Y10T428/236 , Y10T428/24149 , Y10T428/24917 , Y10T428/253
摘要： The invention relates to an arrangement for lining the interior of a passenger vehicle such as an airplane including a honeycomb formation of several honeycombs arranged side by side. At its end, the honeycomb body is supported by a cover layer supported above and below the honeycomb formation such that by means of two cover layers glued onto the honeycomb formation, a layer design of the honeycomb paneling is created, which layer design is arranged so as to extend parallel to the outer skin of the aircraft and follow the curvature of the outer skin. The honeycomb formation used is made of paper or aramide honeycombs or of a mixed combination of both honeycomb types; on whose cross section of the honeycomb body a CFK cover layer is positioned to both ends of the honeycomb bodies. As an alternative, further CFK insulation layers are glued onto the outer surface of the respective cover layer supported above and below the honeycomb formation, which cover layers comprise a CFK or GFK. Moreover, the layer design of the honeycomb paneling may comprise further honeycomb formations which are additionally stacked on and glued to the honeycomb formation used.
摘要翻译：本发明涉及一种用于衬垫乘客车辆的内部的装置，例如飞机，其包括并排布置的几个蜂窝的蜂窝结构。蜂窝体的端部由蜂窝结构体的上下支撑的覆盖层支承，通过粘合在蜂窝结构体上的两层覆盖层，形成蜂窝板的层设计，该层的设计被布置为平行于飞行器的外皮并且遵循外皮的曲率。使用的蜂窝结构体由纸或芳族聚酰胺蜂窝体或两种蜂窝类型的混合组合制成; 在蜂窝体的横截面上，CFK覆盖层位于蜂窝体的两端。作为替代方案，将另外的CFK绝缘层胶合到支撑在蜂窝结构上方和下方的相应覆盖层的外表面上，覆盖层包括CFK或GFK。此外，蜂窝板的层设计可以包括另外堆叠在所使用的蜂窝结构上并粘合到蜂窝结构上的蜂窝结构。

59. 发明授权

US07784743B2 Line holder in an aircraft 有权
标题翻译：飞机上的线架
公开(公告)号：US07784743B2
公开(公告)日：2010-08-31
申请号：US12067971
申请日：2006-09-28
申请人： Lutz Zeuner , Lueder Kosiankowski , Hans-Peter Guthke
发明人： Lutz Zeuner , Lueder Kosiankowski , Hans-Peter Guthke
IPC分类号： F16L17/02
CPC分类号： F16L3/123 , F16B19/1081 , H02G3/30
摘要： The present invention relates to a retainer or holder for positioning a line on a structural component, a line guiding system for reducing sag in line guiding, and an aircraft having at least one line, which is equipped with a line guiding system according to the present invention. In addition, the present invention relates to the use of the line guiding system according to the present invention in an aircraft. The holder essentially comprises a main body, a bracing element and an engagement element. The bracing element projects from the bottom side of the main body and divides the main body globally into a cantilever section and a support section. The engagement element is adapted to be received frictionally locked by a reception opening in a structural component. A support for a line is located on the top side of the main body in the area of the cantilever section, through whose weight load the holder experiences a torque, which is transferred via the bracing element and the engagement element as a force couple into the structural component.
摘要翻译：本发明涉及一种用于将线定位在结构部件上的保持器或保持器，用于减少线引导中的下垂的线引导系统，以及具有至少一条线的飞机，其配备有根据本发明的线引导系统发明。此外，本发明涉及根据本发明的线路引导系统在飞行器中的用途。保持器基本上包括主体，支撑元件和接合元件。支撑元件从主体的底部突出，并将主体全局分成悬臂部分和支撑部分。接合元件适于被结构部件中的接收开口摩擦地锁定。线的支撑件位于悬臂部分区域的主体的顶侧，通过其重量负载，保持器经受扭矩，其通过支撑元件和接合元件作为力耦合传递到结构部件。

60. 发明授权

US07766592B2 Screw nut for torque limiting, and the use of such a screw nut in a retainer module for limiting the clamping force 有权
标题翻译：用于扭矩限制的螺母，以及用于限制夹紧力的保持器模块中使用这种螺母
公开(公告)号：US07766592B2
公开(公告)日：2010-08-03
申请号：US11584210
申请日：2006-10-20
申请人： Lutz Zeuner , Lueder Kosiankowski , Hans-Peter Guthke
发明人： Lutz Zeuner , Lueder Kosiankowski , Hans-Peter Guthke
IPC分类号： F16B31/00
CPC分类号： F16B2/065 , F16B31/02 , F16B37/00
摘要： The present application describes to a screw nut for limiting the torque or the clamping force that is produced by screwing a screw onto a component to be screwed into place, as well as to the use of such a screw nut in a retainer module. The screw nut comprises a clamping body which during screwing comes to rest against the component to be screwed into place. Furthermore, the screw nut comprises a screw body, by means of which the screw nut can be screwed onto the screw. The clamping body and the screw body are movably arranged between an unlocked position and a locked position so that when a defined clamping force is exceeded the unlocked position is taken up, with a restoring force continuously acting against this state transition.
摘要翻译：本申请描述了一种用于限制通过将螺钉拧入待拧入到的部件上产生的扭矩或夹紧力的螺母，以及在保持器模块中使用这种螺母。螺母包括夹紧体，该夹紧体在拧紧过程中抵靠部件固定以便被拧入到位。此外，螺母包括螺丝体，通过螺纹本体可将螺母拧入螺钉上。夹紧体和螺纹体可移动地布置在解锁位置和锁定位置之间，使得当超过限定的夹紧力时，解锁位置被吸收，恢复力持续地抵抗该状态转变。

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