Abstract: 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.

Abstract: The present invention provides a device for mounting systems, for example an electrical or fluid-conveying line, on a structure, in particular of an aircraft or spacecraft, the device comprising a basic holder which is fastenable to the structure and a system holder for mounting the systems, the system holder being fastenable to a first interface of the basic holder, which system holder is fastenable to a first interface of the basic holder; the basic holder comprising a first part, which comprises the first interface, and a second part, one end of which is attachable to the first part so as to be pivotal about a pivot axis and the other end of which is fastenable to the structure.

Abstract: The present invention provides a device for mounting systems, for example an electrical or fluid-conveying line, on a structure, in particular of an aircraft or spacecraft, the device comprising: a basic holder which can be fastened to the structure; and at least a first system holder for mounting the systems; the basic holder being made up of at least a first part comprising a first interface for fastening the first system holder and a second part comprising a second interface for fastening the first or a second system holder, the interfaces being formed in an identical manner and pointing in different spatial directions.

Abstract: The present invention relates to a device for holding systems, for example an electric or fluid-guiding line, on a structure, in particular an aircraft or spacecraft, comprising: a first holding part, which has a first encompassing portion to encompass the system in portions and a first foot portion; a second holding part, which has a second encompassing portion for encompassing the system in portions and a second foot portion; a fastening mechanism, by means of which the first and second foot portion of the first and second holding part can be detachably fastened to one another, so the first and second encompassing portion of the first and second holding part encompass a region, in which the system is located with its entire periphery.

Abstract: 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.

Abstract: The present invention provides a device for mounting systems, for example an electrical or fluid-conveying line, on a structure, in particular of an aircraft or spacecraft, the device comprising: a basic holder which is fastenable to the structure; and a system holder for mounting the systems, which system holder is fastenable to a first interface of the basic holder; the basic holder comprising a first part, which comprises the first interface, and a second part, one end of which is attachable to the first part so as to be pivotal about a pivot axis and the other end of which is fastenable to the structure.

Abstract: The present invention provides a device for mounting systems, for example an electrical or fluid-conveying line, on a structure, in particular of an aircraft or spacecraft, the device comprising: a basic holder which can be fastened to the structure; and at least a first system holder for mounting the systems; the basic holder being made up of at least a first part comprising a first interface for fastening the first system holder and a second part comprising a second interface for fastening the first or a second system holder, the interfaces being formed in an identical manner and pointing in different spatial directions.

Abstract: The present invention relates to a device for holding systems, for example an electric or fluid-guiding line, on a structure, in particular an aircraft or spacecraft, comprising: a first holding part, which has a first encompassing portion to encompass the system in portions and a first foot portion; a second holding part, which has a second encompassing portion for encompassing the system in portions and a second foot portion; a fastening mechanism, by means of which the first and second foot portion of the first and second holding part can be detachably fastened to one another, so the first and second encompassing portion of the first and second holding part encompass a region, in which the system is located with its entire periphery.

Abstract: 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.

Abstract: 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.