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    • 1. 发明授权
    • Device for mounting systems and aircraft or spacecraft
    • 用于安装系统和飞机或航天器的装置
    • US08651435B2
    • 2014-02-18
    • US13193253
    • 2011-07-28
    • Hans Peter GuthkeBarbara Lunitz
    • Hans Peter GuthkeBarbara Lunitz
    • F16L3/08E04G5/06
    • H02G3/263B64C1/406F16L3/24
    • The present invention provides a device for mounting systems, for example an electrical or fluid-conveying line, on a structure, in particular of an aircraft or spacecraft, the device comprising: a basic holder which can be fastened to the structure; and at least a first system holder for mounting the systems; the basic holder being made up of at least a first part comprising a first interface for fastening the first system holder and a second part comprising a second interface for fastening the first or a second system holder, the interfaces being formed in an identical manner and pointing in different spatial directions.
    • 本发明提供了一种用于将系统(例如电气或流体输送线)安装在特别是飞机或航天器的结构上的装置,该装置包括:可固定到结构的基座; 和用于安装系统的至少第一系统保持器; 所述基本保持器由至少第一部分构成,所述第一部分包括用于紧固所述第一系统保持器的第一接口和包括用于紧固所述第一或第二系统保持器的第二接口的第二部分,所述接口以相同的方式形成并且指向 在不同的空间方向。
    • 2. 发明授权
    • Device for supporting systems
    • 支持系统的设备
    • US08534624B2
    • 2013-09-17
    • US12130382
    • 2008-05-30
    • Barbara LunitzHans Peter GuthkeMarcus Juenemann
    • Barbara LunitzHans Peter GuthkeMarcus Juenemann
    • A47B96/00
    • H02G3/32F16B3/00F16L3/24
    • The present invention relates to a device for supporting systems, for example an electric cable or a fluid-carrying pipe, on a structure of an aircraft or space craft, and to an aircraft or space craft with such a device. The device has a basic bracket arrangement which can be fastened to at least one predetermined fastening section of the structure, and also has at least one system bracket for supporting the systems. The at least one system bracket can be fastened to the basic bracket arrangement locationally variable with respect to the fastening section. The advantage of the invention consists in the fact that a route of a system can be flexibly varied even during the equipment assembly, i.e. the structure is no longer modifiable or is only modifiable at considerable expense.
    • 本发明涉及一种用于在飞机或航天飞机的结构上支撑系统的装置,例如电缆或流体输送管,以及具有这种装置的飞机或航天飞机。 该装置具有基本的支架装置,其可以紧固到结构的至少一个预定的紧固部分,并且还具有用于支撑系统的至少一个系统支架。 所述至少一个系统支架可被固定到相对于所述紧固部分位置可变的所述基本支架装置。 本发明的优点在于,即使在设备组装期间,系统的路线也可以灵活地变化,即结构不再是可修改的,或者仅在可观的费用下是可修改的。
    • 5. 发明申请
    • Device and method for mounting objects on a vehicle wall
    • 将物体安装在车辆墙壁上的装置和方法
    • US20090136321A1
    • 2009-05-28
    • US11990865
    • 2006-08-21
    • Lueder KosiankowskiLutz ZeunerHans-Peter Guthke
    • Lueder KosiankowskiLutz ZeunerHans-Peter Guthke
    • F16B37/08E01B9/12
    • F16B37/005F16B37/0828F16B37/0842
    • The invention relates to a retaining device for retaining objects on a vehicle wall, comprising: a supporting element (4) for placing on a front side (2) of the wall (1) with devices (5) for retaining one or a plurality of objects (6) and a fastening element (8, 9) for locking the supporting element (4) on a rear side (3) of the wall (1), as well as a method for mounting objects with this retaining device. In order to reduce the installation cost, and in order not to be dependent on the supporting wall thickness, the fastening element (8) is pin-shaped and has a head (9) at one end so that it can be inserted through an opening (7) in the wall (1) and can be prevented against sliding out in one direction, and the supporting element (4) comprises a connecting device (13) with which the supporting element (4) can be solidly connected to the fastening element (8) projecting from the front side (2) of the wall.
    • 本发明涉及一种用于将物体保持在车辆墙壁上的保持装置,包括:用于将墙壁(1)的前侧(2)放置在其上的支撑元件(4),其具有用于保持一个或多个 物体(6)和用于将支撑元件(4)锁定在壁(1)的后侧(3)上的紧固元件(8,9)以及用于使用该保持装置安装物体的方法。 为了降低安装成本,为了不依赖于支撑壁厚度,紧固元件(8)是销状的,并且在一端具有头部(9),使得其可以插入通过开口 (1)中的(7)并且可以防止在一个方向上滑出,并且支撑元件(4)包括连接装置(13),支撑元件(4)可以通过该连接装置牢固地连接到紧固元件 (8)从所述壁的前侧(2)突出。
    • 6. 发明申请
    • DEVICE FOR SUPPORTING SYSTEMS
    • 支持系统的设备
    • US20080296443A1
    • 2008-12-04
    • US12130382
    • 2008-05-30
    • Barbara LunitzHans Peter GuthkeMarcus Juenemann
    • Barbara LunitzHans Peter GuthkeMarcus Juenemann
    • F16L3/23
    • H02G3/32F16B3/00F16L3/24
    • The present invention relates to a device for supporting systems, for example an electric cable or a fluid-carrying pipe, on a structure of an aircraft or space craft, and to an aircraft or space craft with such a device. The device has a basic bracket arrangement which can be fastened to at least one predetermined fastening section of the structure, and also has at least one system bracket for supporting the systems. The at least one system bracket can be fastened to the basic bracket arrangement locationally variable with respect to the fastening section. The advantage of the invention consists in the fact that a route of a system can be flexibly varied even during the equipment assembly, i.e. the structure is no longer modifiable or is only modifiable at considerable expense.
    • 本发明涉及一种用于在飞机或航天飞机的结构上支撑系统的装置,例如电缆或流体输送管,以及具有这种装置的飞机或航天飞机。 该装置具有基本的支架装置,其可以紧固到结构的至少一个预定的紧固部分,并且还具有用于支撑系统的至少一个系统支架。 所述至少一个系统支架可被固定到相对于所述紧固部分位置可变的所述基本支架装置。 本发明的优点在于,即使在设备组装期间,系统的路线也可以灵活地变化,即结构不再是可修改的,或者仅在可观的费用下是可修改的。
    • 8. 发明授权
    • Cable guiding arrangement for a cableform inside an aircraft cabin
    • 飞机机舱内电缆线的电缆引导装置
    • US08242367B2
    • 2012-08-14
    • US12762104
    • 2010-04-16
    • Hans-Peter GuthkeLueder Kosiankowski
    • Hans-Peter GuthkeLueder Kosiankowski
    • H02G3/04
    • H02G3/32H02G3/0456
    • 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.
    • 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。
    • 10. 发明申请
    • DEVICE FOR LAYING A CABLE HARNESS IN AN AIRCRAFT
    • 用于在飞机上铺设电缆线束的装置
    • US20100301177A1
    • 2010-12-02
    • US12788703
    • 2010-05-27
    • Hans-Peter GUTHKELueder KOSIANKOWSKIMartin SCHNOORAndreas JACOBI
    • Hans-Peter GUTHKELueder KOSIANKOWSKIMartin SCHNOORAndreas JACOBI
    • F16L3/22F16L3/08
    • H02G3/30B60R16/0222
    • A device for bridging a cable harness between two aircraft structure elements of an aircraft includes an elongated connecting rod having a plurality of radial snap-in holes and configured to bridge a space between the two aircraft structure elements and affix to at least one of the two aircraft structure elements. The device also includes a cable guiding element having at least one receiving section for receiving the cable harness and at least one attachment section circumferentially surrounding the connecting rod, the attachment section having a resiliently held radially directed locking pin, wherein the locking pin corresponds to one of the plurality of the radial snap-in holes so as to form a clip connection and a positive locking engagement between the at least one attachment section and the connecting rod.
    • 用于桥接在飞行器的两个飞行器结构元件之间的电缆线束的装置包括细长的连接杆,其具有多个径向卡入孔,并且被配置为桥接两个飞行器结构元件之间的空间并且固定到两个飞行器结构元件中的至少一个 飞机结构元素。 所述装置还包括电缆引导元件,所述电缆引导元件具有至少一个用于容纳所述电缆线束的接收部分和至少一个围绕所述连接杆的连接部分,所述连接部分具有弹性保持的径向定位的锁定销,其中所述锁定销对应于一个 所述多个所述径向卡入孔中的一个以形成所述至少一个附接部分和所述连接杆之间的夹子连接和正向锁定接合。