Airbus Deutschland Gmbh

Airbus Operations Gmbh

Doris Zyrull

Hans-Georg Plate

Lutz Schapke

Lueder Kosiankowski

Hans Peter Guthke

Barbara Lunitz

Marcus Juenemann

The present invention provides a mounting arrangement for mounting at least one electrical line on a structure, in particular of an aircraft or spacecraft, said mounting arrangement comprising: at least one module which comprises at least one terminal for connecting the electrical line; and a substantially U-shaped holder which comprises a central portion for mounting the electrical line for strain relief thereof and two side portions which are connected to the respective ends of the central portion and carry the central portion with spacing from the at least one module; the central portion of the holder having a changeable length.

Mounting arrangement for mounting systems and aircraft or spacecraft

A suspension clamping holder is designed for use with a supporting structure. The supporting structure may have a first region and a another region extending from the first region at an angle. The first region has a holding portion, which is used to support the weight of the holder any load carried by the holder. The holder is capable of being suspended from the supporting structure. A holding element on one end of the holder is suspended from the supporting structure and a clamping slider is connected releasably with the bar region of the supporting structure. The clamping slider is capable of being fixedly clamped onto the bar region and the holder is capable of being locked on the supporting structure without any necessary screws.

Suspension clamping holder for a support structure

A clamp holder to be suspended in an opening of vertical. The clamp holder includes a cantilever beam, a pillar, and a clamp slider. The cantilever beam is vertically at the beam end on an upper end of the pillar, on the back of the pillar. A beam extension is angled upward from the beam on the front of the pillar. A clamp slider, in a U-shape is on a free leg end vertically at a lower end of the pillar. A beam-like holding element is molded onto a free end of the beam extension. A cuboid support element is molded onto the free end of the holding element, with a cuboid transverse surface of the holding element placed in front of the pillar, and is angled upward from the support element molding. The support element has a mutual relationship with a cuboid pressure element. The latter is positioned removably attached to the support element. The pressure element has a receiver region with a chamber open to the base and the cover faces of the pressure element. The open chamber cross-section is tailored to the element cross-section and the spatial position of the support element, and because of that, an internal chamber wall region of the chamber, if the support element is guided through the chamber, is fixed in place on the support element by correlation of multiple mechanical means.

Clamp holder for a support structure

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Neu Wulmstorf, Germany

Doris Zyrull