The present invention relates to a pneumatic support according to the preamble of Claim 1 and to a method for the production thereof according to Claim 10.
Pneumatic supports of the type mentioned are known and are based on a cylindrical basic shape according to WO 01/73245. This basic shape has been developed into, inter alia, a spindle-shaped support according to WO 2005/007991.
An advantage of such pneumatic supports is their low weight and the extremely small transport volume, since the inflatable body can be folded up and the tension members can be in the form of cables. A disadvantage of such pneumatic supports consists in that, although they can bear high distributed loads and are therefore suitable for many purposes, they are suitable to only a limited extent for asymmetric loads in comparison with the possible distributed load, which in particular prevents use as a bridge, since an axle rolling over a bridge, for instance of a heavy goods vehicle, represents a particularly unfavourable case in this respect.
The pneumatic body 4 preferably consists of a gas-tight, flexible, substantially non-elastic material which forms a sleeve which can be collapsed for transport and assumes a shape suitable for the pneumatic support in question when under operating pressure.
The support 1 is supported at its ends 6, 7 via rests 8, 9; the compression member 2 and the tension member 3 are also connected to each other there via a node 10, 11.
Schematically indicated planking 12 allows the support 1 to be used in this case as a bridge.
The following conceptual model can explain the operating principle of the support:
If a load 13 acts on the planking 11 and thus on the compression member 2, the latter is borne by the inflated body 4 under operating pressure, which body for its part, however, rests on the tension member 3 which thus actually bears the load 13. As a result, the tension member 3 tries to move downwards, which is not possible, however, since the compression member 2 holds apart the common end nodes 10 and 11 and thus also the end of the tension member 3. End nodes 10, 11 mean the regions in which the compression member 2 and the tension member 3 are connected to each other for operation. By means of the end nodes 10, 11, force is transmitted from the compression member 2 into the tension member 3, and conversely force is also transmitted from the tension member 3 into the compression member 2. The end nodes 10, 11 are therefore force introduction points for both the compression member 2 and the tension member 3.
As a result, the tension member 3 is loaded substantially only with axial tension, and the compression member 2 is loaded substantially only with axial compression, and therefore the tension member 3 can be in the form of a cable and the compression member 2 can be in the form of a thin rod. However, a thin rod under compression is susceptible to buckling, and therefore the buckling limit of the compression member 2 determines the load capacity of the support 1.
In the case of a distributed load which is distributed symmetrically over the length of the support, as is the case in roof structures, for instance, a reduced risk of buckling results, since buckling in a direction counter to the application of load is prevented by the load itself, and buckling in the loading direction is prevented by the compression member resting on the pneumatic body 4.
In the case of an asymmetrical load, however, the compression member sinks into the body 4 more at the location of the load 12 and protrudes at a different point, with a tendency to protrude beyond the rest surface on the body 4 and thus lift off from said body, which results in an increased risk of buckling and thus in a significantly reduced load capacity of the support 1.
Therefore, connecting elements are preferably arranged vertically (i.e. in the loading direction and perpendicular to the longitudinal axis of the support 1), said connecting elements being in the form of simple tension members 14 which connect the compression member 2 to the tension member 3. In the case of an asymmetrical load, the tension members 14 are suitable, to a certain extent, for preventing the compression member 2 from lifting off from the body 4 at an unloaded location and thus buckling. The horizontal spacing of the tension members 14 can be optimised to the specific case by a person skilled in the art.
The connecting points between the tension members 14 and the compression member 2 and the tension member 3 are again force introduction points for these elements.
In this case too, the connecting points of the nodes 18, 19 with the respective compression member 23, 25, tension member 26, 28 and the connecting points of the compression members 23 to 25 and of the tension members 26 to 28 with the connecting elements 32, 33 form force introduction points into the compression members 23 to 25 and into the tension members 26 to 28.
Common to the supports 1, 15, 40, 45 is the advantage that they can be transported easily when dismantled and can be assembled on site in that the end nodes, compression members, tension members and any connecting elements are assembled, then the pneumatic bodies are inflated and put under operating pressure. A disadvantage is that the supports 1, 15, 40, 45 become increasingly distorted during pressure buildup and finally, when under operating pressure but free of load, assume a position distorted in an arcuate manner, and only assume their extended desired position as shown in
The distortion (i.e. the undesired deformation which occurs when the pneumatic bodies 4 and 29-31 are inflated without load) takes place in the direction of the greater curvature of the compression member and of the tension member, and therefore the supports of
It can be seen from
It can be seen from Figure if that the pneumatic support 15 shown in
It can be seen from
It can be seen from Figure if that the pneumatic support 451 shown in
The above-discussed conditions for a support according to
Distortion and bending play or do not play a role depending on the intended use: for example, distortion is unfavourable in the case of a bridge, which should be as resistant to bending as possible. It is particularly disadvantageous if a bridge formed from supports according to
This also applies to other pneumatic supports, for example according to
Correspondingly, the object of the present invention is to create a pneumatic support which exhibits the phenomenon of distortion only to a reduced extent or avoids it altogether.
The object is achieved by the characterising features of Claims 1 and 10.
The fact that the pneumatic body has formations which extend between adjacent force introduction points and which project outwardly beyond a rectilinear connection between the adjacent force introduction points means that a pressure distribution is produced in the pneumatic body (or in the pneumatic bodies of the segments of a pneumatic support having multiple segments) which counteracts and thereby reduces or avoids distortion.
The invention is explained in more detail further below using the figures.
In the figures:
It should be noted at this point that in principle any type of pneumatic support exhibiting the phenomenon of distortion can be modified according to the invention.
Shown are the compression rods 74 to 76 and the tension elements in the form of tension cables 77, 79 and the tension rod 78 of the segments 71 to 73. Also shown are the connecting elements 33, 34 which are unchanged in comparison with the embodiment of
Thanks to these formations 86 to 89, a force equilibrium is produced according to the invention in the pneumatic bodies 80, 82 by the operating pressure, with which force equilibrium deformation of the pneumatic body by the operating pressure is substantially omitted, in contrast to the prior art. Formations 86 to 89 are advantageously, and preferably as shown in
Further preferably, the formations 86 to 89 have a height above the connection line between the force introduction points 83 to 85 delimiting them of 10 to 15% of the spacing of these force introduction points 83 to 85. The applicant has found that such a height already effectively prevents the undesirable distortion.
Finally, the tension member 77, 79 is further preferably operatively connected to the pneumatic body 80, 82 only at the location of the force introduction points 83 to 85, so that the tension member between the force introduction points 83 to 85 can extend rectilinearly and do not have to follow the contour of the pneumatic body 80, 82 or of the contour of the formations 86 to 89, which results in a shortening of the spacing of the force introduction points 83, 85 under operating pressure, and then results in a more complicated design of the whole segment 71, 73 in relation to the compression rod 74, 76, the pressure body 80, 82, the tension cable 77, 79 and the contour of the formations 86 to 89, which is very complex to calculate and therefore would have to be determined by experiments as well.
According to the preferred embodiment shown in the figure, a pneumatic support (having one or more asymmetrical pneumatic bodies in the longitudinal direction) is produced, in which, when under operating pressure but load-free, the side thereof with the compression member is at least partially curved in an arcuate manner, and the side thereof with the tension member is designed such that the force introduction points thereof lie substantially on a straight line.
It should be mentioned at this point that the configuration of the pneumatic support according to
In summary, a pneumatic support is produced according to the invention having a (or multiple) pneumatic body which can be placed pneumatically under pressure and which, under operating pressure, operationally keeps at a distance apart a compression member which extends substantially over its length and a tension member which likewise extends substantially over its length, wherein forces are introduced at force introduction points in end regions of the compression member and the tension member into said members and wherein connecting elements are provided between the compression member and the tension member and introduce forces into the compression member and the tension member likewise at force introduction points, wherein the pneumatic body has formations which extend between adjacent force introduction points and which project outwardly beyond a rectilinear connection between the adjacent force introduction points.
As already mentioned above, the pneumatic support preferably has a flexible sleeve (specifically the pneumatic body or, in the case of multiple segments, multiple pneumatic bodies having multiple flexible sleeves), the pattern of which defines the shape of the support under operating pressure such that the formations are formed in a predefined contour.
There is preferably at least one connecting element in the pneumatic support, said connecting element extending in a zigzag manner continuously through the entire length of the pneumatic body and particularly preferably running, as mentioned above, at an angle of 45° to the intended loading direction (therefore, 45° to the horizontal in the case of a bridge). Therefore, the adjacent force introduction points have different spacings from one another when the spacing of the compression member and the tension member changes, as is the case in the embodiment according to
In a particularly simple manner, the height of the formations is defined iteratively, since the calculation for this is complex: In a first step, the height is defined at 10 to 15% of the spacing of the associated (i.e. adjacent) force introduction points. Then, the pneumatic support can still have an undesirable residual distortion, and therefore the height of the formations is increased further by 30-50% in a second step (with an initial 10% increase, the resulting height would then be between 13 and 15% of the spacing of the adjacent force introduction points). With most configurations of a pneumatic support to be defined for the specific case by a person skilled in the art, this iterative method converges very rapidly but can easily be continued until the distortion substantially disappears or no further improvement occurs for the intended use of the support.
Specifically, a method is provided according to the invention with which arcuate, preferably circular arc-shaped, formations are preferably provided in a pneumatic support, the height of which formations being 10 to 15% of the spacing of the associated force introduction points.
Therefore, the structure of a pneumatic support according to the invention is preferably designed such that a (or multiple) formation has a height above the connecting line between the force introduction points delimiting them of 10 to 15% of the spacing of these force introduction points.
The pneumatic support designed according to the invention is then constructed for the case of the application of the iterative method, and the pneumatic body of the support is brought to operating pressure and checked for the presence of a persistent distortion of the support relative to the intended shape, and in the positive case the height of selected formations is increased by 30-50%. Usually, a person skilled in the art will increase all the formations equally but can change only selected formations, for example by experimentation, if the affected pneumatic body has a particular shape.
Finally, if desired for the intended use of the pneumatic support, the iterative method can be continued, i.e. the height of the formations can be increased iteratively until a further increase does not produce a further improvement in the curvature of the unloaded support.
As a result, a method is provided according to the invention for producing a pneumatic support, in which the shape of the pneumatic support during operation and the location of the force introduction points are defined in advance and then the distortion to be expected under operating pressure but without operating load is defined, and then formations on the inside of the curve of the pneumatic support are provided, said formations extending outwardly from force introduction point to force introduction point via a connecting line between associated force introduction points.
Number | Date | Country | Kind |
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00728/16 | Jun 2016 | CH | national |
Filing Document | Filing Date | Country | Kind |
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PCT/CH2017/000053 | 6/1/2017 | WO | 00 |