WO2008092428A2

WO2008092428A2 - Covering element, and method for attaching the same

Info

Publication number: WO2008092428A2
Application number: PCT/DE2008/000148
Authority: WO
Inventors: Bernhard Urbach
Original assignee: Bernhard Urbach
Priority date: 2007-01-30
Filing date: 2008-01-28
Publication date: 2008-08-07
Also published as: WO2008092428A3; DE202007005743U1; DE102007005424A1; EP2157890A2; DE102007005424B4

Abstract

The invention relates to a tarpaulin (1) that is to be attached to a support element (7) and comprises a plurality of rope-type fastening means (4a-4f), each of which has a first end mounted at a lateral edge (2) of the tarpaulin and a second end (6a, 6f) wrapped around the support element. The plurality of fastening means forms at least one group encompassing at least two fastening means (4a) that are arranged at an edge of the group. The second end (6a) of a fastening means (4a) located at a first edge of the group is retained by the adjacent fastening means (4b) while the second end (6f) of the fastening means (4f) located at a second edge of the group is removably fixed by means of a release system, said second edge of the group lying opposite the first edge.

Description

Cladding element, and method for its attachment

The invention relates to a cladding element for attachment to a support element, and a corresponding method for this.

Temporary stages for event venues - also known as so-called "flying buildings" - are usually provided with cladding elements in the form of side panels, for example, to protect the stage surface from drafts and / or rain The side panels are on a support element A common technique for assembling the side trim on the support member consists of eyelets and rubber loops, as shown in Fig. 11. The rubber loops are placed over the top of a roof rail or a vertical side support of the roof construction Looped supporting element, and then hung in itself.

DIN 4112 stipulates that in the case of flying structures, the dynamic pressure in the operating state may be set below the values of the control wind to q = 0.3 kN / m ² , if the design for the control wind can not be proved. This presupposes that the side cover is always removed during the unmonitored period. If the permitted dynamic pressure is reached in the operating condition of the stage, the operation must be stopped immediately and the side panel removed immediately to avoid excessive wind loads for the stage construction. This is to exclude a possible failure of the stage construction.

In Fig. 12, a conventional mounting technique of a side panel 11 is shown on a support member 7, wherein rubber loops each in eyelets 3, which are provided on a side edge of the panel 11, attached and wrapped around the support member 7 and hooked with a hook 10 in itself are. The removal of the side panel, according to the above The technique mentioned is mounted on the support element 7, proves to be impractical under time pressure, as an assembly worker has to solve all rubber loops individually. Furthermore, a climb to a roof traverse at considerable wind speeds, z. B. from wind force 8, and considerable roof heights too dangerous, which z. B. is not accepted by the examiners of the TÜV. The variant, instead of removing the side panel to lower the stage roof, also proves to be impractical, since the windings dissolve when lowering, and can be difficult to retighten with a suitable speed and thus the system is unstable, and / or the stage roof by the Wind pressure or the tense

Wind associations tilted and can not be lowered smoothly. In addition, on-stage installations can prevent a rapid lowering of the stage roof.

A variant of the assembly technique of FIG. 12 is to provide the side panel with a Kederwulst which is inserted into a Kederschienenprofil. In calm weather and good weather conditions, the side panel for disassembly can be pulled out longitudinally from the piping rail profile. Nevertheless, from a certain ¹ wind strength of the dynamic pressure on the side panel is very high and thus the friction in the piping rail too strong, so that the side panel can not be pulled out of the Kederschienenprofil. In addition, dangerous lateral forces act on the roof supports in windfalls. The required Kederschienenprofile are also relatively expensive to purchase. Another disadvantage is a complex installation of the side panel on the Kederschienenprofil, since the Kederwulst must be threaded over long lengths in the Kederschienenprofil.

Another alternative for securing the side panel is the use of curtain rails, as they are for. B. for truck side panels are known. Such curtain rails are attached to the roof frame. The side panel is attached to it with rollers, and pushed to the side in the oncoming wind. However, the possibility of mounting by means of curtain rails is subject to the disadvantage that in unfavorable wind and directional conditions, the tarpaulin can lift off after loosening the lower attachment and thus projects horizontally from the stage. The side panel can then no longer be pushed together and generates dangerous lateral forces, the side panel flutters loose in the wind. Even in deferred or collapsed condition, the side panel still provides a substantial wind attack surface which creates adverse transverse forces on the pillars of the stage roof construction. From certain stage sizes and heights such a curtain rail system can only be implemented with strong electric motors that ensure a shifting of the side panel. This makes the system comparatively expensive and expensive to install and operate.

The aforementioned systems for attaching a side panel in flying buildings are all subject to the disadvantage that a fast and for an assembly worker especially safe removal of the side panel is not possible.

Accordingly, the invention has for its object to provide a cladding element and a method for its attachment to a support element with which a quick release of the support member with in particular simple and inexpensive means is possible.

This object is achieved by a cladding element having the features of claim 1 and by a method having the features of claims 18 and 19, respectively. Advantageous developments are the subject of the dependent claims.

An inventive cladding element for attachment to a

Supporting element comprises a plurality of cable-like fastening means each having a first end attached to a side edge of the cladding element and a second end, with which the support element at least partially entwined. The plurality of fastening means forms at least one group with at least two fastening means which are respectively arranged on a first edge of the group and on a first edge opposite the second edge of the group. The second end of a fastener located at the first edge of the group is held by the fastener adjacent thereto, and the second end of the fastener located at the second edge of the group is releasably fixed by means of a release system.

A significant advantage of the cladding element according to the invention is that the second end of the fastening means located on the first edge is not fastened separately, but is held by the fastening means adjacent thereto in the direction of the second edge. If removal of the lining element from the support element is required if the dynamic pressure permitted by DIN 4112 is exceeded, the second end of the fastening element located on the second edge of the group is loosened, so that it can come loose from the support element. After this, the second end of the fastening means, which is adjacent in the direction of the first edge of the group, is automatically released, so that this fastening means can also escape from the support element. If the group of fasteners includes more than two fasteners mounted along the side edge of the trim member, releasing the second end of the fastener at the second edge will cause some sort of chain reaction towards the first edge, thereby causing all second ends of the fastener loosen respective fasteners and these can escape from the support element.

In an advantageous embodiment of the invention, the group of fastening means between its first and second edge may comprise at least one further fastening means, the second end of which is held by a fastening means adjacent to the second edge of the group and which the second end of a neighboring in the direction of the first edge Fastener stops. Thus, separate attachment points on the Support element for the second ends of the fastener omitted. As discussed above, upon release of the second end of the fastener located at the second edge of the group, a chain reaction begins in the direction of the first edge of the group, after which all second ends of the mutually adjacent fasteners are successively released so that the corresponding fasteners are released immediately can loosen the support element. After this Entschlaufen the cladding element falls off automatically from the support element.

In an advantageous embodiment of the invention causes a release of the second

End of the fastener located on the second edge, a release of the adjacent in the direction of the first edge of the group fastener and / or disposed on the first edge of the group fastener, so that the fastening means are entschlaufbar with their respective dissolved second end of the support member. This is already referred to above as chain reaction and explained. This chain reaction also occurs when the group of fasteners contains more than two elements, e.g. B. ten or even twenty mutually adjacent fasteners. In principle, the number of fasteners for a particular group is not limited.

In an advantageous development of the invention, the triggering system can be actuated mechanically, electrically (eg by motor or magnet) and / or pneumatically. The triggering system may comprise a suitable mechanism that the second end of the located on the second edge of the group

Holds fastener and releases when pressing the trigger system. Such a mechanism may, for example, comprise a pivotable hook or a displaceable bolt or the like, wherein the hook or the bolt are pivoted or displaced upon actuation of the triggering system. Alternatively, the trigger system may function in any other way, as long as it is actuated to ensure that the second end of the fastener is released at the second edge of the group. For example, this second end also be solved by means of an annealing with a filament, cutting with an electric scissors or the like. All of the above possibilities have the advantage that a kind of remote control by switching on a circuit is possible.

In a purely mechanical solution, the trigger system can be operated manually, z. B. by pulling on a pull rope, which operates a suitable mechanism or is connected to a pivotally mounted on the trigger system hook. The hook holds the second end of the fastener at the second edge of the group in the operative state, wherein pulling on the pull rope, the hook is pivoted about an axis and thereby releases the second end of the fastener. In particular, when such a release system is attached to a lower flange of the roof rail of the stage roof, the above-mentioned operation of a suitable mechanism by pulling on a rope does not require an assembly worker to climb up to release the panel element. Alternatively, and / or additionally, the triggering system may be electrically, magnetically, or pneumatically operable in any suitable form, including means for holding or releasing the second end of the fastener. Such means may also consist of a displaceable bolt or bolt, after its displacement, the second end of the fastener is released. The decisive factor is that the operation of the release system, the free end of the fastener is released, which has been previously releasably held.

In an electric, magnetic and / or pneumatic release system, a combination with wind force sensors or the like is possible. When measuring a specific wind force and / or wind forces on the side panel, the trigger system can be triggered automatically to ensure the reliability in the absence of people on a stage or in the vicinity due to incorrect operations or unresponsive operating personnel. Nevertheless, one is continuous monitoring of a stage construction according to the specifications of DIN 4112. In the presence of monitoring personnel, the triggering system can be actuated by it if necessary, to bring about a controlled release or falling of the cladding element.

In an advantageous embodiment of the invention, the second end of at least one fastening means having a closed loop, a ring device, an eyelet or the like, through which the adjacent thereto in the direction of the second edge of the group fastener is pulled and thus holds the second end of the aforementioned fastening means. Alternatively, the fastening means itself may be formed as a loop in its entire longitudinal extent. This represents an extremely inexpensive fixation of a fastener by the respectively adjacent fastener and makes additional attachment points on the support element superfluous. Furthermore, for this purpose, the said chain reaction is ensured, according to which, upon release of the fastening means located at the second edge of the group, the fastening means adjacent thereto in the direction of the first edge are also loosened, since the fastening means loops from one another and subsequently from the support element.

In an advantageous embodiment of the invention, the mutually adjacent fastening means of the group can wrap around the support element of opposite sides. As a result, the cladding element is reliably secured to the support element and substantially centrally to its longitudinal axis. Furthermore, in this case the number of wrap points of the mutually adjacent fastening means is minimized, so that the successive release of mutually adjacent fastening means in the direction of the first end of the group in the literal sense of friction or friction takes place.

If the cladding element has a large length, it is expedient to provide a plurality of groups of fastening means on the cladding element, which are arranged in the longitudinal direction of the support element and each have a triggering system. Regarding each individual group When releasing the fastening means located at a second edge of the group, it sets in a chain reaction, so that the release of all fasteners within one and the same group is ensured in a very short time. If the triggering systems of the respective groups can be actuated synchronously with one another and are triggered simultaneously, it is thus also possible to detach very long lining elements from a carrier element in a very short time.

For a low-friction sliding of the fastening means when releasing the cladding element from the support element, a wrapping with a fabric or with a textile is expedient. The fastening means may each be designed as a rubber band or as a rubber loop, whereby slight tolerances can be compensated for and the assembly of the cladding element is facilitated on the support element. The fabric with which the rubber bands or the rubber loops can be wrapped also causes less wear and tear when lashing the rubber loops on the support element.

An inventive method for attaching a cladding element to a support element comprises the steps:

a) providing a plurality of cable-like fastening means each having a first end attached to a side edge of the trim element and a second end, wherein the plurality of fastening means form at least one group with at least two fastening means respectively arranged at an edge of the group and at each second end thereof a loop or the like, b) wrapping the second end of the fastener at a first edge of the group about the support member so that the second end extends above the eyelet to the fastener adjacent the second edge of the group in the direction of the first edge . c) looping the second end of another fastener adjacent the second edge of the group about the support member; d) passing the second end of the fastener of step c) through the loop of the second end of the fastener adjacent to the first edge of the group; such that this second end is held by the fastener of step c), and e) releasably fixing the second end of the fastener located on the second edge of the group.

An inventive method according to an alternative embodiment by means of which the cladding element can be attached to a support element, comprises the steps:

A method of attaching a trim member to a support member, comprising the steps of: a) providing a plurality of cable-like fasteners each having a first end attached to a side edge of the trim member and a second end, the plurality of fastener means at least one group having at least two respective ones b) looping around the second end of the fastener at a first edge of the group around the support element so that the second end above the eyelet surrounds the fastener which is disposed on one edge of the group; C) passing the second end of a further fastener adjacent to the second edge of the group through the loop of the second end of the group in the direction of the first edge of the group Group adjacent fastener so that this second end is held by the fastener of step c), d) looping around the second end of the fastener of step c) at least partially around the support member, and e) releasably fixing the second end of the fastener located at the second edge of the group.

The method according to the invention ensures a simple assembly technique of a cladding element on a support element and, moreover, can be realized by extremely inexpensive means. At high wind forces by the method, a disengagement of the cladding element from the support element within a few seconds is possible by the free end of the located at the second edge of the group fastener is released and thereafter in the manner of a chain reaction, the second ends of all to in the direction of the first Rands of the group adjacent fasteners are entwined from each other. Thereafter, a subsequent loosening of the fastening means of the support element is possible. Thus, the method of the invention meets a requirement that was set up in the context of DIN 4112 by the commission building supervision.

The cladding element according to the invention and the inventive method can be z. B. in flying buildings to any stage size and height apply. Furthermore, a use of the inventive cladding element or a use of the method according to the invention is also useful wherever it depends on a disassembly of the cladding element within seconds. Thus, the invention relates to a safety device with which, for example, in fairing tarpaulins of flying buildings, a wind load reduction can be achieved. The cladding element may, for example, be a side cladding of a mobile stage construction.

Further advantages and embodiments of the invention will become apparent from the description and the accompanying drawings.

It is understood that the features mentioned above and those yet to be explained not only in the combination specified in each case, but also in other combinations or alone, without departing from the scope of the present invention. The invention is illustrated schematically with reference to a preferred embodiment in the drawing and will be described in detail below with reference to the drawing. Show it:

Fig. 1 is a front view of an upper part of an inventive

Cladding element with fastening means in the form of rubber loops, which are attached to the side edge of the cladding element,

2 shows a fastening means in the form of a loop,

Fig. 3 is a front view of the trim element of Fig. 1 when attached to a support member by means of the loops of Fig. 2;

4 is an enlarged view of the cladding element according to the

Section I of Figure 3, Fig. 5 to 9, a successive loosening and loosening of mutually adjacent fastening means for releasing the cladding element of the support element,

10 is a front view of a support element, on which a cladding element is fastened with fasteners combined into several separate groups,

11 is a front view of a cladding element according to another embodiment, and

Fig. 12 is a conventional mounting technique for a fairing tarpaulin.

Fig. 1 shows a front view of an upper part of a cladding element 1, at the upper side edge 2 a plurality of eyelets 3 is provided. In the eyelets 3 each fastening means 4 are attached in the form of rubber loops, which - are wrapped for optimal function as explained below - with a textile. In Fig. 2, a rubber band 4 is shown in a plan view. The rubber loop 4 has a first end 5 and a second end 6 on. Contrary to their name, the rubber loop 4 also made of a non-elastic material, eg. B. from a textile-like rope or the like, as known from the sail area, be prepared.

To attach in an eyelet 3, a respective rubber loop 4 is guided with its second end 6 through the eyelet 3 and then threaded through itself, so that thereby forming at the first end 5 loop on the side edge 2 of the covering tarpaulin 1 sets. The cladding element 1 may be formed from a covering tarpaulin and will hereinafter always be referred to as such, without being limiting. Such a fairing can z. B. in stage constructions serve as side and / or roof cladding. The fastening principle by means of which the covering tarpaulin 1 with the rubber loops 4 is mounted or fastened to a support element is explained below with reference to FIGS. 3 and 4 in detail.

The covering tarpaulin 1 is first brought with its upper side edge 2 to a support element 7, so that the side edge 2 extends substantially parallel to the support element 7. The trim sheet 1 is shown by way of example with six rubber loops 4, which are designated below with 4a to 4f (Fig. 1). Similarly, the second ends of the respective rubber loops 4a to 4f are designated 6a to 6f. These six rubber loops 4a to 4f together form a group of rubber loops, with a first edge (at the far left in FIG. 3) and a second edge opposite the first edge (at the far right in FIG. 3). Accordingly are the

Rubber loop 4a at the first edge of the group and the rubber band 4f at the second edge of the group.

It should be understood that a set of fastener or rubber loops is not limited to the number of six, but may include two, more than two, or any number of fasteners. To fasten the trim sheet 1, the second end 6a of the rubber band 4a is first looped around the support member 7 and then guided in the direction of the rubber loop 4b, which is adjacent thereto in the direction of the second edge of the group. The second end 6b of the rubber loop 4b is also looped around the support member 7, then threaded through the loop of the second end 6a and thereafter guided in the direction of the rubber loop 4c. Analogously to the rubber loop 4b, the rubber loop 4c is now looped with its second end 5c around the support element 7, then threaded through the loop of the second end 6b and guided in the direction of the second edge of the group to the next rubber loop 4d. The above procedure is also illustrated in Fig. 4, which shows an enlargement of the area I of Fig. 3. The looping of the support member 7 and the entrainment of the second end of a respective left adjacent rubber band is now continued for the rubber loops 4d, 4e to the rubber loop 4f, the latter rubber loop on the second edge of the group (in Fig. 3 rightmost) is arranged , In this way, the side edge 2 of the covering tarpaulin 1 is "crocheted" on the support element 7, without separate attachment points or the like being provided on the support element 7 adjacent to the course of the side edge 2.

In the illustration of Fig. 4, the rubber loops 4a, 4b, 4c and 4d are alternately wrapped around the support member 7 from opposite sides. This effectively prevents unintentional slipping of the covering tarpaulin 1 from the support element 7 and thus ensures a secure attachment of the covering tarp 1 substantially centrally relative to a longitudinal axis of the support element 7. Alternatively to the "crocheting" shown in Fig. 4 of the rubber loops 4 of opposite sides Her is also a looping of the support member 7 of each of the same side possible, in which case the second ends of the respective rubber loops after wrapping above a corresponding eyelet 3 between the panel 1 and the first end of the rubber loop are to be passed. As a result, an unintentional falling off of the covering tarpaulin 1 is likewise prevented by the support element 7.

Instead of the above-mentioned alternative for wrapping the fastening means around the support element 7, any other manner of entanglement is possible which ensures reliable holding of the covering tarpaulin 1 on the support element 7.

The second end 6f of the rubber loop 4f is releasably secured to the support member 7 by means of a triggering system 8, as shown in FIG. The triggering system 8 includes suitable means such. B. a pivotable about an axis hook, a sliding bolt or the like, whereby both a secure holding of the second end 6 f and a targeted release is possible. By fixing the second end 6f of the rubber loop 4f, all other rubber loops 4a to 4e are automatically fixed and secured against unwanted loosening of the support element 7.

To release the second end 6f of the rubber loop 4f, the triggering system 8 can be actuated electrically (by electric motor or magnetically) and / or pneumatically. Alternatively, a purely mechanical actuation of the

Tripping system 8 possible, z. B. via a (not shown) pull rope, which is connected to a suitable mechanism. By pulling the pull cable, the mechanism is actuated or released and thereby releases the second end 6f.

Below, with reference to Figures 5 to 9, a release of the covering tarpaulin 1 is explained by the support member 7.

For releasing the covering tarpaulin 1, the triggering system 8 is actuated, as a result of which the second end 6f drops off the supporting element 7. This is shown in FIGS. 5 and 6. Following this, the rubber loop 4f escapes from the support element 7 (FIG. 7) due to the dead weight of the covering tarpaulin 1 or because of an attacking wind load. In this case, the second end 6e releases from the rubber loop 4f, so that now also the rubber loop 4e can escape from the support element 7, which is shown in Fig. 7. The successive loosening of adjacent rubber loops starting from the second edge of the group towards the first edge of the group (from right to left in FIGS. 5 to 9) takes place in the manner of a chain reaction, through which, as shown in FIG Rubber loops 4a to 4f detach from each other and can accordingly disentangled from the support member 7. As a result, the trim sheet 1 falls from the support member 7 as shown in FIG. The above-mentioned chain reaction or the automatic release of all rubber loops 4a to 4f of the group takes place within a few seconds. A manual release of the individual rubber loops by an assembly worker is not required. Solely the release of the second end 6f, which is caused by an actuation of the triggering system 8, leads to a successive release of all remaining rubber loops to the first edge of the group.

The textile fabric with which the individual rubber loops 4a to 4f are respectively wound, supports the loosening of the rubber loops of the support member 7 and the corresponding Entfädeln of mutually adjacent rubber loops. As a result, a quick, since low-friction sliding of the rubber loops ensured both by the support member 7 and from each other.

Especially with high stage structures, when the support element 7 is located at a height of several meters above a stage surface, the actuation of the triggering system 8 for releasing or releasing the second end 6f is of particular advantage, as hereby a climbing up a stage worker to the support element 7 is superfluous , The triggering system 8 can be done mechanically or electrically-mechanically in the same way, for. B. in the form of a pivotable hook which holds the second end 6f in the assembled state of the covering tarpaulin 1 and by pivoting about an axis, the second end 6f releases. Such a pivoting of the hook can by a Pull rope, which is to be operated by a stagehand without further ado, or carried out by electric motor.

A length of the side edge of the covering tarpaulin 1, which is fastened to the support element 7 according to the above-mentioned principle of crooking the rubber loops together, has no limits in principle. With considerable lengths of the side edge of the covering tarpaulin 1, the rubber loops 4 can advantageously be combined into individual groups, as shown in FIG. This means that a respective second end 6f of a specific rubber band, without having reached an edge of the support element 7, as described above by a release system 8 is releasably fixed. After this marginal rubber band adjoins a first edge of a new group of rubber loops adjacent to the second edge of a second end of a rubber band is again set by a triggering system 8. Extra long trim tarpaulins can thus be fastened to a support element 7 with a plurality of rubber loops, which are combined into individual groups. For a desired immediate release of the covering tarpaulin 1 of the support member 7 then the individual trigger systems 8 of the respective groups are simultaneously or at least pressed shortly after one another, so that an immediate drop of the covering tarpaulin 1 is ensured by the support member 7 even at long lengths.

In the support member 7, it may be z. B. to act a lower flange of a roof beam of a flying construction or the like. In the same way, the support member 7 may consist of a vertically arranged mounting tube of a stage construction. The falling of the covering tarpaulin 1 from a vertically arranged support element 7 takes place in the same way by their gravity or by attacking wind forces.

FIG. 11 shows a further embodiment of the cladding element 1 according to the invention. The embodiment of the cladding element 1 according to FIG. 11 is identical to that of FIGS. 1 and 3 with respect to the eyelets 3 and the plurality of rubber loops 4 and differs therefrom solely in a different fastening of the lining element 1 to the support element 7.

In the same way as in Fig. 3, in the illustration of Fig. 11, the covering element 1 is shown in a position when it is completely fastened or "crocheted" to the supporting element 7 by means of the respective rubber loops 4. However, in contrast to Figs 3, in the embodiment according to FIG. 11, the individual rubber loops are not completely wound around the support element 7. The rubber loops 4a to 4c illustrate this before the rubber loop 4b at least partially surrounds the support element 7 Then, as seen in Fig. 11, the rubber loop 4b is looped around substantially half a circumference of the support member 7 therearound, and thereafter, the second end 6b is passed through the loop of the second end 6a of the rubber loop 4a the loop of the second end 6b thread through the next adjacent rubber loop 4c, which then again in We sentlichen around half a circumference around the support member 7 is wrapped around. Thus, the mode of attachment of the rubber loops 4 in the embodiment according to FIG. 11 differs from that of FIG. 3 by the time at which a rubber loop is threaded through the loop of a rubber band adjacent thereto in the direction of the first edge of the lining element 1. In the embodiment of FIG. 11, this threading of a respective rubber loop through the loop of a rubber band adjacent to the first edge of the trim element 1 takes place before the rubber loop in question is wrapped around the support element 7. In the embodiment according to FIG respective rubber loop initially wrapped substantially completely around the support element around, and then only through the loop of an adjacent in the direction of the first edge of the cladding element 1 rubber loop passed through. The type of attachment according to Illustration of FIG. 11 has the advantage that hereby the cladding element 1 can be fastened even more quickly to the support element 7.

The principle of attachment of the second end 6f of the rubber loop 4f to the triggering system 8 corresponds to that of the embodiment of FIG. 3.

The same applies to the release of the second end 6f of the triggering system 8 and a subsequent automatic dropping of the cladding element 1 of the support member 7. In this regard, reference is made to avoid repetition of the above explanation.

It is understood that the above-mentioned trim sheet 1 can be used not only in flying structures, but also everywhere, where a speedy removal of a fairing tarp or the like from a support member, a holder o.a. is required.

Claims

A cladding element (1) for attachment to a support element (7), comprising a plurality of rope-like attachment means (4) each having a first end (5) attached to a side edge (2) of the cladding element (1) and a second end (6) ), with which the support element (7) is looped, characterized in that the plurality of fastening means form at least one group (4a - 4f) with at least two respectively arranged on one edge of the group fastening means, wherein the second end (6a) of an a fastener (4a) located at a first edge of the group is at least partially looped around the support element (7) so as to extend to the fastener (6f) adjacent to the second edge of the group and from the fastener adjacent thereto (4b) is held, wherein the second end (6f) of the fastening element located on a second edge of the group opposite the first edge of the group Telt (4f) by means of a release system (8) is releasably fixed.

2. cladding element (1) according to claim 1, wherein the group of fastening means (4a - 4f) between the respective attachment center at its first and second edge (4a, 4f) at least one further

Fastening means (4b - 4e), the second end (6b - 6e) of which is held in the direction of the second edge of the group adjacent fastening means (6f) and which the second end (6a) of an adjacent in the direction of the first edge fastening means (4a ) holds.

3. cladding element (1) according to claim 1 or 2, wherein a release of the second end (6f) of the located on the second edge Fixing means (4f) effecting loosening of the fastening means (4b-4e) adjacent to the first edge of the group and / or fastening means (4a) arranged on the first edge of the group, so that the fastening means (4a-4f) engage with their respective ones dissolved second ends (6a - 6f) are entschlaufbar of the support element.

4. cladding element (1) according to one of claims 1 to 3, wherein the triggering system (8) is mechanically, electrically and / or pneumatically actuated.

5. cladding element (1) according to one of claims 1 to 4, wherein the triggering system (8) comprises a suitable mechanism which holds the second end (6f) of the located at the second edge of the group fastening means (4f) and upon actuation of

Release system (8) releases.

6. cladding element according to claim 5, wherein the mechanism comprises a hook which is pivotally hinged to the triggering system about an axis, or a displaceable bolt or the like, wherein the hook or the bolt are pivoted upon actuation of the triggering system ,

7. cladding element according to claim 6, wherein the hook or the bolt are manually displaceable by a pull cable, electric or electric motor.

8. cladding element (1) according to one of claims 1 to 7, wherein the second end of at least one fastening means (4a - 4f) has a closed loop, a ring device, an eyelet or the like or the fastening means (4a-4f) each of a Loop having a first end (5a-5f) and a second end (6a-6f), wherein by the loop or by its second end (6a-6f) that is drawn towards the second edge of the group adjacent fastener and thus holds the second end of the aforementioned fastener.

9. cladding element (1) according to one of claims 1 to 8, in which mutually adjacent fastening means of the group (4a - 4f) wrap around the support member (7) from opposite sides.

10. cladding element (1) according to one of claims 1 to 9, which has a plurality of groups of fastening means which in

Longitudinal direction of the support element (7) are arranged and each having a trigger system (8).

11. cladding element (1) according to claim 10, wherein the triggering systems (8) of the respective groups of fastening means are synchronized aktuierbar each other.

12. cladding element (1) according to one of claims 1 to 11, wherein the fastening means (4a - 4f) at its first end (5a-5f) has a loop or the like and at an eyelet (3) of the

Cladding element is fixed by the second end (6a - 6f) of the fastener is first passed through the eyelet (3) and then through the loop of its first end (5a-5f).

13. cladding element (1) according to one of claims 1 to 12, wherein at least one fastening means of a rubber band or a rubber loop (4) is formed.

14. cladding element (1) according to one of claims 1 to 13, wherein all fastening means of at least one group of a rubber band or a rubber loop (4) are formed.

15. cladding element (1) according to claim 13 or 14, wherein the

Rubber band or the rubber loop (4) is covered with a tissue.

16. cladding element (1) according to one of claims 1 to 15, wherein the length of the fastening means a sum of a wrap around the support element (7), the respective distance between two attachment points on the side edge of the cladding element (1) and possibly the Distance of the cladding element (1) to the support element (7) in the attached

State corresponds.

17. cladding element (1) according to one of claims 1 to 15, wherein the length of the fastening means a sum of a length of a Teilumschlingung to the support member (7), the respective distance between two attachment points on the side edge of the cladding element (1) and if necessary corresponds to the distance of the cladding element (1) to the support element (7) in its attached state.

18. A method for attaching a cladding element to a support element, comprising the steps of: a) providing a plurality of rope-like fastening means (4) each having a first end attached to a side edge (2) of the cladding element (1) and a second end (6a); 6f), wherein the plurality of fastening means form at least one fastening element (4a, 4f) arranged at each edge of the group and have a loop or the like at their second end (6a, 6f), b) looping around the second End (6a) of the fastener (4a) located at a first edge of the group about the support element (7), so that the second end (6a) above the eyelet adjoins the in C) looping the second end (6f) of a further fastening means (4f) adjacent to the second edge of the group about the support element (7), d) of the second end (6f) of the fastening means (4f) of step c) through the loop of the second end (6a) of the fastening means (4a) adjacent to the first edge of the group, such that this second end (6a) is fixed by the fastening means (6a). 4f) of step c), and e) releasably fixing the second end (6f) of the fastener means located at the second edge of the group.

19. A method for attaching a cladding element to a support element, comprising the steps of: a) providing a plurality of rope-like attachment means (4) each having a first end attached to a side edge (2) of the cladding element (1) and a second end (6a); 6f), wherein the plurality of fastening means arranged at least one group with at least two each at one edge of the group

B) looping around the second end (6a) of the fastening means (4a) located at a first edge of the group around the support element (7) ), so that the second end (6a) above the eyelet to the in

C) passing the second end (6f) of a further fastening means (4f) adjacent to the second edge of the group through the loop of the second end (6a) of the second fastening element (6f) in the direction of the first

Edge of the group of adjacent attachment means (4a) so that this second end (6a) is held by the attachment means (4f) of step c), d) looping around the second end (6f) of the fastener (4f) of step c) at least partially around the support element (7), and e) releasably fixing the second end (6f) of the fastener (4T) located on the second edge of the group ,

20. A method according to claim 18 or 19, wherein releasing the second end (6f) in step f) releases the second ends (6a-6e) of all fasteners adjacent to the first edge of the group so that all fasteners (4a-4a) 4f) of the support element (7) are entschlaufbar.

A method according to any one of claims 18 to 20, wherein the group comprises two attachment means (4a, 4f) mounted adjacent to each other on the side edge of the cladding element, the attachment means in steps c) and d) being connected to the attachment means (4f ) at the second edge of the group.

22. The method according to any one of claims 18 to 20, wherein the group comprises more than two fastening means (4a -4f), wherein in step d) the fastening means (4b - 4e) from step c) guided in the direction of the second edge of the group and steps c) and d) are repeated as many times as the group contains fasteners exceeding the number of two.

23. The method according to any one of claims 18 to 22, wherein the mutually adjacent fastening means (4) are wound with their second ends (5) respectively from opposite sides to the support member (7).

24. Use of a cladding element (1) according to one of claims 1 to 17 in a method according to one of claims 18 to 23.

25. Flying construction, with a cladding element (1) according to one of claims 1 to 17.

26. A flying construction comprising a cladding element (1) attached to a support element by a method according to any one of claims 18 to 23.