The present invention relates to a textile structural element.
Mechanical and pneumatic structural elements are known which are used primarily in automated systems also using robotics, for example, for the manipulation of objects.
Linear movements have the aim, for example, to move an object from position A to position B or grasp an object or an object to secure a stable position spatially, etc. To achieve this, complicated drives, constructions or controls are employed, which directly, via rotational, translational or pivotal connections or indirectly, by means of hydraulic devices, chain drives or air cylinders result in the corresponding movements. For this purpose machine elements are traditionally used extensively in the engineering, which are often prone to wear and also costly and often require a large expenditure of sensors and precision control.
Also well known are structural elements for the configuration of spatial structures such as houses, industrial buildings, walls, partitions, etc., made of metal, foil, concrete, etc. which commonly feature the need for a supporting apparatus or skeletal support. Some of these spatial structures cannot be disassembled without some destruction and/or are no longer usable even after disassembly.
The invention has the object of proposing a textile structural element and a method for producing the same which avoids, or at least greatly diminishes, the known disadvantages of prior art.
The object is firstly achieved by a textile structural element as set forth in claim 1, namely a textile structural element, characterized by textile stretch elements and textile supporting elements, wherein said stretch elements and the supporting elements are locally connected to each other in allowing at least partially a spatial expansion of at least one inflatable stretch element and/or supporting element. The use of structural elements in accordance with the invention advantageously allows by pneumatic or hydraulic actuation and by structural elements accommodated in a spatial expansion the construction of spatial structures without an additional brace for the structural element or a plurality of structural elements in use, as well as incidentally achieving gripper functions and linear movements in conjunction with the pressurization of the airbag or air chamber structures.
In one advantageous embodiment of the invention, the textile structural element is characterized by integrated stretch elements which can be shortened, and integrated supporting elements which are extensible spatially or constant. The stretch elements in this arrangement become shortened in accordance with the invention, in thus resulting in traction, whilst the supporting elements extend, for example, in one direction in space, and result in a shortening in another direction. It is these effects that can be used to enhance the movements made by the stretch elements and the supporting elements as the design elements of which are connected together intermittently, as a result of pressure in the horizontal or vertical direction, or “into the third dimension.” In addition, the shaping possibilities of textile structural elements can be varied to boost the incentives for their use. The “arching textiles” proposed in accordance with the invention in this arrangement can also be appreciated as “textile muscles” representing actuators which by highly elegant and gentle means achieve low wear coupled with cost-effectiveness, requiring little sensing control.
In a further advantageous embodiment of the invention, the textile structural element is characterized in that the textile stretch elements and/or textile supporting elements are configured as a single and multi-layer woven textile sheeting comprising airbags or air chambers, woven in one piece (OPW=one-piece-woven technique).
The structural elements as combined in accordance with the invention consisting of supporting elements and stretch elements are joined together from both inflatable and non-inflatable elements, for example. The OPW fabricating stages can be advantageously extended by the stitching method, i.e. a specific combination of OPW structural elements with air chambers stitched with sections of fabric sheeting. The response to shaping the combined textile structural element is controlled by the pneumatic deployment of inflatable stretch or supporting elements. Shaping can also be determined by correspondingly adapting the joining of inflatable and non-inflatable components.
In an advantageous variant of the invention it is also conceivable to include the supporting elements in the form of non-textile elements (such as lightweight profiles, cylinders, tubes, etc.).
In a further advantageous embodiment of the invention, the textile structural element is characterized by a first fabric layer comprising stretch elements, a second fabric layer comprising supporting elements and a third fabric layer comprising stretch elements. This construction simultaneously results in a flat structural element, as it is in the idle state, for example, which, depending on the activation of the first or the third layer of fabric produces a curvature upwards (convex) or downwards (concave). An exemplary configuration in this respect by, for example, designing the first fabric layer with non-contractible, quasi “passive” stretch elements, which are longer than the stretch elements of the third layer of fabric now makes it possible that the passive stretch elements are tightened when the stretch elements of the third fabric layer are activated, i.e. inflated, with the effect that the first stretch elements determine the maximum degree of curvature of the textile structural element.
In yet another advantageous embodiment of the invention, the textile structural element is characterized by a fourth fabric layer comprising supporting elements which advantageously increases the stability of the structural element.
In still another advantageous embodiment of the invention, the textile structural element is characterized by a first fabric layer comprising non-inflatable stretch elements, a second fabric layer comprising inflatable supporting elements and a third fabric layer comprising non-inflatable stretch elements. To advantage this variant provides for a predefined end position of the textile structural element, achieving a constant curvature when the supporting elements are inflated to a maximum.
In yet a further advantageous embodiment of the invention, the textile structural element is characterized by a fabric layer comprising fourth, inflatable supporting elements and a fabric layer comprising fifth, inflatable stretch elements. This variant represents a variation advantageously increasing the stability of the structural element described above.
In still another advantageous embodiment of the invention, the textile structural element is characterized by stretch elements and supporting elements inflatable at least in part, wherein the stretch elements and/or the supporting elements are individually inflatable, and wherein the outer shape of the textile structural element can be varied by inflating. The advantages of the method in accordance with the invention will become apparent from the detailed discussion above.
In yet another advantageous embodiment of the invention, the structural element can be rendered curved, there being no limit to the number of possible shapes in this respect. The curved shape has the particular advantage that e.g. a hall or an archway or, for instance, other self-standing structures requiring no further supporting means can now be formed.
In yet a further advantageous embodiment of the invention, the structural element is adapted to grip and/or hold and/or clamp objects. The curvature of the structural element can be extremely extended, for example, resulting in a holding, clamping or gripping device.
The object of the invention is further achieved by a method for fabricating a textile structural element as set forth in any of the claims 4 to 10, wherein in one-piece-woven (OPW) airbags, or single or multilayer woven textile sheets provided with air chambers and sections of sheet fabrics are stitched together. The advantages of the method in accordance with the invention read from the detailed discussion above, especially from the fact that the OPW stages in fabrication can be extended to advantage to the stitching process, i.e. that a specific combination of OPW structural elements with air chambers stitched with sheet fabric sections results in economically interesting solutions.
For a better understanding of the invention it is briefly described below with reference to embodiments with reference to a drawing, all FIGs. of which are diagrammatic sectional views.
All like components in the example embodiments are identified by like reference numerals.
Referring now to
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It is also possible to pressurize both fabric layers I and III by gas inflation, resulting in a solid mat. Shaping is mainly due to the geometric design of the stretch elements and supporting elements and the line of attachment to one another.
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In this construction, two supporting layers (fabric layers II and IV) are arranged between the stretching layers (fabric layers I, III and V). The greater spacing apart of the stretch elements makes for a higher loading capacity, for example. Furthermore, shaping can now be set more precisely in addition to designing the length and contraction distance of the stretching layers.
The stretch elements 61 and 62 in this case are not acted upon with pressure, they supporting shaping simply by the distance between the attachment points.
To enhance the stability in rendering the arching more precise a stretch layer V can be added.
Referring now to
In this construction one supporting layer (fabric layer II) is disposed between two stretch layers (fabric layers I and III). The stretch elements 61 and 62 in this case are not to be activated upon by this pressure. Shaping is only influenced here by the distance of the stretch elements located between the fixing points 4 and the dimensions of the supporting layer.
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It is understood that all structural elements cited in the claims and the example embodiments (
It is understood that any indication in the present description as to chambers or airbags being “inflated”, this always includes the meaning of being charged with fluids, such as gases, liquids, or foams, as well as including fluids which cure hard at least, i.e. in becoming solids.
The invention is, for example, applicable also for the following applications such as pneumatic structural elements, temporary rescue shelters, supporting structures, bionic structures (flat-hollow hand palm), load securing of sensitive goods, textile clamps, baseball mitts, inner linings of silos, buffered connections, butt connector, tensairity structures such as bridge building components, aircraft wings etc. used.
Number | Date | Country | Kind |
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10 2011 016 032.9 | Apr 2011 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2012/001463 | 4/2/2012 | WO | 00 | 8/2/2013 |