公开(公告)号：US07246771B2

公开(公告)日：2007-07-24

申请号：US11022114

申请日：2004-12-23

申请人： Bodo Wisch ,  Lars Rowold

发明人： Bodo Wisch ,  Lars Rowold

IPC分类号： B64D11/00

CPC分类号： B64D11/003 ,  B60R5/003

摘要： The application concerns a lifting device for a luggage compartment in an aircraft, wherein the luggage compartment can be moved between an open and closed position, and the lifting device includes a power generation element that exerts a lifting force on the luggage compartment. The application also concerns an aircraft with a lifting device for a luggage compartment. The power generation element is an electrical power generation element, and the lifting device has a rechargeable energy accumulator to store energy for operation of the electrical power generation element.

摘要翻译： 该应用涉及一种用于飞行器中的行李箱的提升装置，其中行李箱可以在打开和关闭位置之间移动，并且提升装置包括在行李箱上施加提升力的发电元件。 该应用还涉及具有用于行李箱的提升装置的飞机。 发电元件是发电元件，并且提升装置具有用于存储用于发电元件的操作的能量的可再充电能量蓄能器。

公开(公告)号：US20050141226A1

公开(公告)日：2005-06-30

申请号：US11027562

申请日：2004-12-30

申请人： Bodo Wisch ,  Lars Rowold

发明人： Bodo Wisch ,  Lars Rowold

IPC分类号： A62B3/00 ,  B64D11/00 ,  B64D25/00 ,  B64D47/02 ,  B64F1/20

CPC分类号： B64D25/00 ,  A62B3/00 ,  B64D11/00 ,  B64D47/02 ,  B64D2011/0038 ,  Y02T50/46

摘要： An emergency lighting arrangement preferably includes plural emergency light units connected to an on-board power supply network of an aircraft, and plural emergency current sources that each include at least one capacitor. Each emergency light unit includes an emergency light emitting element and a control unit that automatically connects the capacitor of the emergency current source to the emergency light emitting element upon the failure of the on-board power supply network. Preferably, the emergency current source including the capacitor is integrated into the emergency light unit. The emergency light unit may further include normal operation light emitting elements selectively connected by the control unit to the on-board power supply network. The control unit switches between normal operation of the normal light emitting elements and charging of the capacitor, and emergency operation in which the capacitor discharges through the emergency light emitting element.

摘要翻译： 紧急照明装置优选地包括连接到飞行器的车载电源网络的多个应急灯单元和各自包括至少一个电容器的多个应急电流源。 每个应急灯单元包括应急发光元件和一个控制单元，当车载电源网络发生故障时，自动将应急电流源的电容器连接到应急发光元件。 优选地，包括电容器的应急电流源集成到应急灯单元中。 应急灯单元还可以包括由控制单元选择性地连接到车载电源网络的正常操作发光元件。 控制单元在普通发光元件的正常工作和电容器的充电之间切换，电容器通过应急发光元件放电的紧急动作。

公开(公告)号：US07988091B2

公开(公告)日：2011-08-02

申请号：US11630308

申请日：2005-06-14

申请人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch ,  Bruno Alquier

发明人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch ,  Bruno Alquier

IPC分类号： B64D11/00

CPC分类号： G05G15/08 ,  B64D11/003

摘要： This device is provided for a luggage compartment designed to be placed overhead. The compartment comprises a mobile part (4) between an open position and a closed position and a mechanism for acting on said mobile part (4) to promote its closing. Said mobile part (4) presents an opening (14) designed for introducing and retrieving luggage as well as a lower exterior surface (12). The control device comprises detection means reacting when pressure is exerted on a predetermined zone of the lower exterior surface (12) of the mobile part (4) as well as for sending a control signal to the mechanism acting on the mobile part (4) to close the part when pressure is exerted on said detection means. The detection means are disposed at the lower exterior surface (12) of the mobile part (4).

摘要翻译： 该设备提供用于设置在顶部的行李舱。 隔间包括在打开位置和关闭位置之间的可移动部件（4）和用于作用在所述移动部件（4）上以促进其关闭的机构。 所述移动部件（4）具有用于引入和取回行李以及下部外表面（12）的开口（14）。 控制装置包括当压力施加在可移动部件（4）的下部外表面（12）的预定区域上并且用于向作用在移动部件（4）上的机构发送控制信号时响应的检测装置 当对所述检测装置施加压力时，关闭该部件。 检测装置设置在移动部件（4）的下外表面（12）处。

公开(公告)号：US07934678B2

公开(公告)日：2011-05-03

申请号：US12321211

申请日：2009-01-16

申请人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch

发明人： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch

IPC分类号： B64D11/00

CPC分类号： G05G15/08 ,  B64D11/003

摘要： A detection unit for integration in a luggage compartment of an airplane, having a capacitive sensor with an active layer, wherein the capacitive sensor is adapted to detect a first event triggered by a user, wherein the detection unit is adapted to transmit a first control signal to a control mechanism, wherein the first control signal corresponds to the first event and wherein the active layer comprises carbon fiber electrically isolated from a surrounding compartment structure.

摘要翻译： 一种用于集成在具有有源层的电容传感器的飞机行李舱中的检测单元，其中所述电容传感器适于检测由用户触发的第一事件，其中所述检测单元适于发送第一控制信号 涉及控制机构，其中所述第一控制信号对应于所述第一事件，并且其中所述有源层包括与周围隔室结构电隔离的碳纤维。

公开(公告)号：US20080143186A1

公开(公告)日：2008-06-19

申请号：US11813465

申请日：2006-01-18

申请人： Bodo Wisch ,  Lars Rowold

发明人： Bodo Wisch ,  Lars Rowold

IPC分类号： H02J15/00

CPC分类号： H02J4/00 ,  H02J7/345 ,  Y10T307/527

摘要： An energy buffer device supplies energy to a consumer in an aircraft, and an electrical system for an aircraft. In one example, the device includes an energy feed device, an energy storage device and an energy supply device. The energy supply device may have line with a larger cross-sectional area than a corresponding line of the energy feed device. With the use of an energy buffer device, power may be switched on only for a short period of time. In addition, in case of a voltage breakdown in an on-board network, energy may be stored in an energy storage device. Supply of energy may thus occur over a short time at correspondingly high power, without placing a load on an on-board network or a generator.

摘要翻译： 能量缓冲装置为飞机上的消费者和飞机的电气系统提供能量。 在一个示例中，该装置包括能量馈送装置，能量存储装置和能量供应装置。 能量供应装置可以具有比能量馈送装置的相应线更大的横截面积的线。 通过使用能量缓冲装置，可以在短时间内接通电源。 此外，在车载网络中的电压故障的情况下，能量可以存储在能量存储装置中。 因此，能够在相当大的功率下在短时间内进行能量供给，而不会在车载网络或发电机上施加负载。

公开(公告)号：US20050072879A1

公开(公告)日：2005-04-07

申请号：US10207273

申请日：2002-07-30

申请人： Andre Hessling ,  Bodo Wisch

发明人： Andre Hessling ,  Bodo Wisch

IPC分类号： B60R13/02 ,  B64C1/00

CPC分类号： B60R13/0206 ,  F16B2200/50 ,  Y10T403/66 ,  Y10T403/7073

摘要： The invention relates to a device for fastening an in-fill panel element to a plane panel element of a covering for an aircraft, the in-fill panel element and the panel element being releasably Interconnected at longitudinal sides facing each other, a transverse pin being arranged at least in the end portion of a longitudinal side so that a hook element arranged In the corresponding end portion of the other longitudinal side is able to clampingly engage with a hook opening, in such a manner that a covering surface of the in-fill panel element is arranged so as to be even with a covering surface of the panel element.

摘要翻译： 本发明涉及一种用于将填充面板元件紧固到用于飞行器的覆盖物的平面屏元件的装置，所述插入面板元件和所述屏元件可释放地相互连接在彼此面对的纵向侧，横向销为 至少布置在纵向侧的端部中，使得布置在另一纵向侧的相应端部中的钩元件能够以与钩开口夹紧接合的方式使得填充物的覆盖表面 面板元件布置成与面板元件的覆盖表面均匀。

公开(公告)号：US07059568B2

公开(公告)日：2006-06-13

申请号：US10207273

申请日：2002-07-30

申请人： André Hessling ,  Bodo Wisch

发明人： André Hessling ,  Bodo Wisch

IPC分类号： B64C1/00

CPC分类号： B60R13/0206 ,  F16B2200/50 ,  Y10T403/66 ,  Y10T403/7073

摘要： The invention relates to a device for fastening an in-fill panel element to a plane panel element of a covering for an aircraft, the in-fill panel element and the panel element being releasably interconnected at longitudinal sides facing each other, a transverse pin being arranged at least in the end portion of a longitudinal side so that a hook element arranged in the corresponding end portion of the other longitudinal side is able to clampingly engage with a hook opening, in such a manner that a covering surface of the in-fill panel element is arranged so as to be even with a covering surface of the panel element.

摘要翻译： 本发明涉及一种用于将填充面板元件紧固到用于飞行器的覆盖物的平面面板元件的装置，所述插入面板元件和所述面板元件在彼此面对的纵向侧面可释放地互连，横向销为 至少布置在纵向侧的端部中，使得布置在另一纵向侧的相应端部中的钩元件能够以钩形开口夹紧地接合，使得填充物的覆盖表面 面板元件布置成与面板元件的覆盖表面均匀。

公开(公告)号：US06732976B2

公开(公告)日：2004-05-11

申请号：US10208812

申请日：2002-08-01

申请人： André Hessling ,  Bodo Wisch

发明人： André Hessling ,  Bodo Wisch

IPC分类号： B64C114

CPC分类号： B64C1/066 ,  Y10T292/1029

摘要： A device for fastening a first part to a second part, particularly for fastening a lining element in the interior of a vehicle, for example an aircraft, is provided with at least one fastening element connectable with the first part and releasably attachable to the second part. The fastening element is provided with a locking element that is supported on the fastening element so as to be movable between a disengaged position in which the fastening element is able to be set to the second part and to be detached therefrom, and a pre-locking position in which the fastening element is held at the second part. Further, the fastening element comprises an actuating element for moving the locking element between the disengaged position and the pre-locking position. The fastening element is further provided with a first biasing element for biasing the locking element into the pre-locking position thereof, and a trigger element comprising at least one retaining projection for the locking element, the trigger element being supported on the fastening element between a retaining position in which the at least one retaining projection retains the locking element in the disengaged position thereof, and a releasing position in which the at least one retaining projection releases the locking element for moving into the pre-locking position. The trigger element is provided for abutting on the second part upon setting the fastening element to the second part.

摘要翻译： 用于将第一部分紧固到第二部分，特别是用于将衬垫元件紧固在车辆内部例如飞行器中的装置设置有至少一个紧固元件，该紧固元件可与第一部件连接并可释放地附接到第二部件 。 紧固元件设置有锁定元件，该锁定元件被支撑在紧固元件上，以便能够在紧固元件能够被固定到第二部分并且从其脱离的脱离位置之间移动，并且预锁定 紧固元件保持在第二部分的位置。 此外，紧固元件包括用于在分离位置和预锁定位置之间移动锁定元件的致动元件。 紧固元件还设置有用于将锁定元件偏置到其预锁定位置的第一偏置元件，以及包括用于锁定元件的至少一个保持突起的触发器元件，触发器元件被支撑在紧固元件之间 保持位置，其中所述至少一个保持突起将所述锁定元件保持在其脱离位置;以及释放位置，其中所述至少一个保持突起释放所述锁定元件以移动到所述预锁定位置。 触发元件设置成在将紧固元件设置到第二部分时抵靠在第二部分上。