Abstract: A cable holder for aircraft comprising a cable receiver section and a main body. The main body is provided with a fastening section to be placed on a surface. The cable holder is essentially made of plastic. In this way, a cable holder is provided, which is easy to manufacture cost-effectively and may be attached to surfaces of greatly varying dimensions.

Abstract: 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.

Abstract: A mount for an aircraft secures insulation material to a structure of the aircraft in which a plate-shaped element and a connecting element that are implemented from a very heat-resistant material are provided. The remainder of the hanger may be implemented from plastic. Under the effect of strong heat, the plastic may melt. An insulation mat is nonetheless secured against falling down/detaching by the plate-shaped element, which is supported using the connecting element.

Abstract: A clamp support for holding and guiding a cable loom has a basic element and a wedge, which can be shifted relative to the basic unit to clamp the basic unit to a structural component. While clamping the basic unit with the structural component, the wedge is arranged in a position between the basic unit and structural component to reflect the width of the transverse carrier.

Abstract: A holder for mounting conduits and tubes at a carrier in airplanes, including a basic body and at least one slide-in part. In this context, the basic body has a recess for receiving the slide-in part. The slide-in part is held in an end position in the recess. By means of the slide-in part, the basic body may be disposed at the carrier. The holder is designed to receive conduits and tubes with a diameter in the order of magnitude of 30 to 50 mm thickness.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: A holder for mounting conduits and tubes at a carrier in airplanes, comprising a basic body and at least one slide-in part. In this context, the basic body has a recess for receiving the slide-in part. The slide-in part is held in an end position in the recess. By means of the slide-in part, the basic body may be disposed at the carrier. The holder is designed to receive conduits and tubes with a diameter in the order of magnitude of 30 to 50 mm thickness.

Abstract: A cable holder for aircraft comprising a cable receiver section and a main body. The main body is provided with a fastening section to be placed on a surface. The cable holder is essentially made of plastic. In this way, a cable holder is provided, which is easy to manufacture cost-effectively and may be attached to surfaces of greatly varying dimensions.

Abstract: A clamp support for holding and guiding a cable loom has a basic element and a wedge, which can be shifted relative to the basic unit to clamp the basic unit to a structural component. While clamping the basic unit with the structural component, the wedge is arranged in a position between the basic unit and structural component to reflect the width of the transverse carrier.

Abstract: The present invention relates to a holder for fastening lines and tubes to a support in aircraft, comprising a base body and at least one slide-in unit. In this connection, the base body has a recess for receiving the slide-in unit. The slide-in unit is held in an end position in the recess. The base body is mountable by means of the slide-in unit to the support. The holder is formed to receive lines and tubes having a diameter in the order of magnitude of 30 to 50 mm thickness.

Abstract: A mount for an aircraft secures insulation material to a structure of the aircraft in which a plate-shaped element and a connecting element that are implemented from a very heat-resistant material are provided. The remainder of the hanger may be implemented from plastic. Under the effect of strong heat, the plastic may melt. An insulation mat is nonetheless secured against falling down/detaching by the plate-shaped element, which is supported using the connecting element.

Abstract: A plurality of electrical conductors or cables are held in place by a cirar member, such as a ring or disk, or by two ring or disk elements forming a pair, to form a conductor or cable bunch. For this purpose a plurality of recesses are provided in the circumferential zone of the ring or disk, for holding a conductor or cable in place in each recess. The recesses in the ring or disk are closed by a rim section. The ring or disk elements have recess forming fingers or pieces which can be rotated into preliminary and final positions with an increased clamping force in the final position. In all embodiments the cable or conductors are held in place by a proper biasing force. The costs for forming cable or conductor bunches and for their final installation have been substantially reduced.