Airbus Deutschland Gmbh

Airbus Operations Gmbh

Lueder Kosiankowski

Hans-Peter Guthke

Lutz Zeuner

Hans-Georg Plate

Martin Schnoor

Hans Peter Guthke

Barbara Lunitz

Doris Zyrull

Marcus Juenemann

Andreas Jacobi

Nico Papke

Philipp Rathgeber

Didier Chassaigne

Carsten Papke

A cover sheath includes a main body being adapted to define a channel for accommodating at least one conducting cable extending there through, and a hook and loop arrangement disposed on at least a portion of an outer surface of the main body. The main body is made of an electrically conducting material.

Cover sheath, fastening arrangement and method of fastening a conducting cable to a carrier component

A holding device for a mounting part installed inside an aircraft fuselage includes an anchor plate configured to attach the holding device to a support rail of the aircraft fuselage and including at least one engagement section. The holding device further includes a holder module separably connected to the anchor plate and configured to fix the mounting part to the aircraft fuselage and having a hook section configured to positively engage the at least one engagement section so as to fasten the holder module to the anchor plate, and at least two clamping blocks disposed on the holder module.

Modular holding device for mounting parts located inside an aircraft fuselage

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 cable management device accommodates bundles of cables in an aircraft. The cable management device includes a star shaped cable management element and a retaining clamp. The star-shaped cable management element includes a plurality of outer-radial recesses disposed in an outer radius of the star-shaped cable management element that are spaced apart from each other. Each outer-radial recess is configured to accommodate a cable inserted therein. The retaining clamp is disposed around an outer circumference of the star-shaped cable management element so as to encompass the star-shaped cable management element and close the outer radial recesses. The retaining clamp includes an attachment portion configured to affix the cable management element to a stationary supporting structure.

Cable management device for bundles of cables in an aircraft

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.

Device for laying a cable harness in an aircraft

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.

Cable guiding arrangement for a cableform inside an aircraft cabin

A retaining device for attachment to a screw contains a hollow base element for receiving a clamping part. The hollow base element has a floor having a hole, and an inner surface of the base element on the floor area of the retaining device is implemented as conical to contact the outer surface of the conical body of the clamping part. The clamping part can be moved downward in the direction of the floor by rotating the retaining device around its own axis and biting into a screw which is inserted through the hole and runs through the opening of the clamping part.

Clamping part and retention device having a clamping part of this type

The invention relates to a holder module for affixing lines of various thicknesses in an aircraft, as well as to a holder system comprising two of the above-mentioned holder modules. Furthermore, the invention relates to a method that makes it possible to lead lines reliably and in an ordered manner through an aperture in a structural component of an aircraft. Finally, the invention relates to an aircraft that is equipped with a plurality of the above-mentioned holder modules, as well as to the use of a plurality of the holder modules according to the invention in an aircraft. The holder module comprises a basic body as well as at least one cross arm. The basic body comprises at least one bearing face to accommodate or support a line. Corresponding to the basic body, the cross arm, too, comprises at least one counter-bearing face that interacts with the bearing face of the basic body. To make it possible for the holder module to reliably accommodate at least one line, the at least one cross arm is movably positioned in relation to the basic body such that the line, due to movement of the at least one cross arm is affixed between the at least one bearing face of the basic body and the at least one counter-bearing face of the at least one cross arm.

Line holder in an aircraft

The present invention relates to a retainer or holder for positioning a line on a structural component, a line guiding system for reducing sag in line guiding, and an aircraft having at least one line, which is equipped with a line guiding system according to the present invention. In addition, the present invention relates to the use of the line guiding system according to the present invention in an aircraft. The holder essentially comprises a main body, a bracing element and an engagement element. The bracing element projects from the bottom side of the main body and divides the main body globally into a cantilever section and a support section. The engagement element is adapted to be received frictionally locked by a reception opening in a structural component. A support for a line is located on the top side of the main body in the area of the cantilever section, through whose weight load the holder experiences a torque, which is transferred via the bracing element and the engagement element as a force couple into the structural component.

The present application describes to a screw nut for limiting the torque or the clamping force that is produced by screwing a screw onto a component to be screwed into place, as well as to the use of such a screw nut in a retainer module. The screw nut comprises a clamping body which during screwing comes to rest against the component to be screwed into place. Furthermore, the screw nut comprises a screw body, by means of which the screw nut can be screwed onto the screw. The clamping body and the screw body are movably arranged between an unlocked position and a locked position so that when a defined clamping force is exceeded the unlocked position is taken up, with a restoring force continuously acting against this state transition.

Screw nut for torque limiting, and the use of such a screw nut in a retainer module for limiting the clamping force

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.

Cable holder for aircraft

The present invention relates to a holding device for moveably accommodating a line. Furthermore, the invention relates to an aircraft that comprises a multitude of such holding devices. Finally, the invention relates to a multitude of holding devices according to the invention for section-by-section line routing in an aircraft. The holding device according to the invention, for movably accommodating at least one line, comprises a guide body that can be attached to an attachment surface in an aircraft, as well as a slide body that is designed to envelope at least one line in the region of the guide body. To prevent any tensile stress or abrasion in or on the line from arising when the attachment surface moves, the slide body is movably held in the guide body in such a way that the slide body compensates for any movement.

Holder for attaching electrical line bundles and pipes etc. to carriers and boards

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.

Multi-purpose mount for securing insulation and holding cables

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.

Clamp support

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.

Growing community of inventors

Jork, Germany

Lueder Kosiankowski