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    • 113. 发明授权
    • Cargo hold floor for a cargo hold of an aircraft and method for the installation thereof
    • 飞机货舱货舱及其安装方法
    • US08474754B2
    • 2013-07-02
    • US12721475
    • 2010-03-10
    • Thomas HuberRichard Holzner
    • Thomas HuberRichard Holzner
    • B64C1/22
    • B64D9/00B64C1/18B64C1/22Y10T29/53
    • Cargo hold floors are provided, and comprise panels or similar two-dimensional floor elements for the attachment of roller elements, ball elements, locking bar elements or similar functional elements. Support elements, in particular floor beams, are provided which support the two-dimensional floor elements whereby the floor elements are permanently joined to the support elements to make pre-fabricated floor modules and the floor modules are installable in the aircraft. To make installation work easier, separate load-bearing elements, for supporting the floor modules on and joining the floor modules to a body or a skin of the aircraft, are provided which, before the floor modules are installed in the aircraft, are joinable to the body or skin of the aircraft, and, when the floor modules are installed in the aircraft, are joinable to the support elements. As a result, it is possible in particular cases to make installation significantly easier.
    • 提供货舱底板,并且包括用于附接滚子元件,滚珠元件,锁定杆元件或类似功能元件的面板或类似的二维地板元件。 提供支撑元件,特别是地板梁,其支撑二维地板元件,由此地板元件永久地连接到支撑元件,以制造预制地板模块,并且地板模块可安装在飞行器中。 为了更容易地进行安装工作,提供了单独的承载元件,用于将地板模块支撑在地板模块上并将其连接到飞机的主体或皮肤上,其在地板模块安装在飞行器之前可连接到 飞机的身体或皮肤,并且当地板模块安装在飞行器中时,可连接到支撑元件。 结果,在特定情况下可能使安装更容易。
    • 118. 发明授权
    • Fixing rail for attaching loading devices to the loading deck of an aircraft
    • 用于将装载装置连接到飞行器的装载甲板上的固定轨道
    • US08286913B2
    • 2012-10-16
    • US11961819
    • 2007-12-20
    • Christoph BaraukeAndreas PatzlspergerThomas Huber
    • Christoph BaraukeAndreas PatzlspergerThomas Huber
    • B64C1/22
    • B64D9/003B64C1/20B64D2009/006Y02T50/46
    • The invention relates to a fixing rail for attaching loading devices, particularly rollers, locking bars or power drive units to the loading deck of an aircraft. This fixing rail comprises a first and a second rail, each rail having a cheek with first attachment devices, to which the loading devices can be fixed, and first floor sections, to which the cheek is attached by a lower edge, each first floor section having second attachment devices, by means of which the floor section can be attached to the loading deck. In this arrangement, the cheeks separated from each other are mountable on the loading devices, so that they are connected to each other by means of the loading devices and the loading deck, following mounting and attaching to the loading deck. In this way, a considerable weight saving is achieved along with increased variability of use of the fixing rail.
    • 本发明涉及一种用于将装载装置,特别是滚子,锁定杆或动力驱动装置附接到飞行器的装载甲板上的固定轨道。 该固定轨道包括第一和第二轨道,每个轨道具有带有第一附接装置的面颊,装载装置可固定到该颊部,以及通过下边缘将面颊附接到其上的第一底板部分, 具有第二附接装置,通过该第二附接装置,地板部分可以附接到装载甲板。 在这种布置中,彼此分离的面颊可以安装在装载装置上,使得它们通过装载装置和装载甲板在安装和附接到装载甲板之后彼此连接。 以这种方式,随着使用固定轨道的可变性的增加,实现了相当大的重量节省。
    • 120. 发明申请
    • FUNCTION ELEMENT, METHOD FOR PRODUCING A FUNCTION ELEMENT
    • 功能元件,产生功能元件的方法
    • US20120119052A1
    • 2012-05-17
    • US13379963
    • 2009-06-22
    • Thomas HuberRichard Holzner
    • Thomas HuberRichard Holzner
    • B64D47/00B23P11/00B60N2/075
    • B64D9/003B64D11/0696Y10T29/49826
    • Some embodiments of the invention relate to function elements for fixing in seat rails of aircraft. The function element according to the invention may include: a fixing rail with a web running in the x direction and a multiplicity of extensions which protrude beyond the web in a y direction to form a T profile, wherein the fixing rail is formed corresponding to the seat rail such that the fixing rail can be inserted in the seat rail and moved along the x direction into a holding position in which the extensions sit between the holes below the slots, at least one fixing peg which is arranged mobile on the fixing rail and can be brought into a blocking position in which the fixing peg engages in a hole of the seat rail so that the function element is fixed in the x direction.
    • 本发明的一些实施例涉及用于固定在飞行器的座椅轨道中的功能元件。 根据本发明的功能元件可以包括:具有在x方向上延伸的幅材的固定轨道和多个延伸部,其沿ay方向突出超过幅材以形成T轮廓,其中,固定轨道对应于座椅 导轨,使得固定导轨能够插入座椅导轨中并沿着x方向移动到保持位置,在该保持位置,延伸部位于狭槽下方的孔之间,至少一个固定栓,其可移动地固定在固定轨道上, 进入阻挡位置,其中固定栓接合在座椅导轨的孔中,使得功能元件在x方向上固定。