| Patent application number | Description | Published |
|---|
| 20080296443 | DEVICE FOR SUPPORTING SYSTEMS - 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. | 12-04-2008 |
| 20090026327 | 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. | 01-29-2009 |
| 20090136321 | Device and method for mounting objects on a vehicle wall - The invention relates to a retaining device for retaining objects on a vehicle wall, comprising: a supporting element ( | 05-28-2009 |
| 20090218452 | Clamping Part and Retention Device Having a Clamping Part of this Type - 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. | 09-03-2009 |
| 20100001135 | Retaining Device - A retaining device includes a fireproof core enclosed by a non-fireproof case, wherein a pre-tensioned fireproof device is integrated in the case and attached to the core. The fireproof device relaxes in such a way, when the case melts, that a construction element is reliably held between the carrier and the device. | 01-07-2010 |
| 20100294564 | CABLE GUIDING ARRANGEMENT FOR A CABLEFORM INSIDE AN AIRCRAFT CABIN - 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. | 11-25-2010 |
| 20100301177 | DEVICE FOR LAYING A CABLE HARNESS 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. | 12-02-2010 |
| 20110290951 | CABLE MANAGEMENT DEVICE FOR BUNDLES OF CABLES IN AN AIRCRAFT - 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. | 12-01-2011 |
