The present technology relates generally to manufacturing techniques and, in particular, to systems and methods for manufacturing textile structures.
Next-generation structures in many industries will increasingly utilize high-performance engineered textiles, fabrics, laminates, and composite materials. These textiles may include functional fibers or embedded sensors or other elements such as, for example, photovoltaic filaments.
Manufacturing such structures, however, is challenging because of the unconventional handling requirements for these textiles. For example, the fabrication of airships with solar energy capturing textiles may require the welding together of large sections of textiles. Efficiently handling these large sections of textiles for welding, cutting, inspection, or other such manufacturing operations has been a technical problem for which a viable solution is now disclosed herein.
In general, the present invention provides a novel method and system for manufacturing textile structures. The invention uses pressurized air to cause the textile structure, or a subcomponent thereof, to hover. While the textile structure is hovering, the textile structure may be easily displaced, manoeuvred, rotated, or otherwise moved relative to one or more manufacturing machines that are used to perform manufacturing operations on the textile structure.
Thus, an aspect of the present invention is a method of manufacturing a textile structure. This novel manufacturing method comprises steps, acts, or operations of causing a textile structure to hover by applying air pressure to an underside of the textile structure, horizontally displacing the textile structure relative to a manufacturing machine while the textile structure is hovering, and performing a manufacturing operation on the textile structure using the manufacturing machine.
Another aspect of the present invention is a system for manufacturing a textile structure. This novel manufacturing system comprises an air pressure source for providing air pressure within a chamber having an upper surface that includes a plurality of air apertures for discharging air to cause a textile structure to hover above the upper surface, and a manufacturing machine that is substantially vertically aligned with the upper surface to enable a manufacturing operation to be performed on the textile structure.
Other aspects of the present invention are described below in relation to the accompanying drawings.
Further features and advantages of the present technology will become apparent from the following detailed description, taken in combination with the appended drawings, in which:
It will be noted that throughout the appended drawings, like features are identified by like reference numerals.
As depicted by way of example in
For the purposes of this specification, “manufacturing machines” are meant to encompass welding machines (e.g. high-frequency (HF) welding machines, ultrasonic textile welding machines, laser welding machines, hot air welding, chemical welding, etc.), cutting machines, drilling machines, plotters, inspection machines, sewing machines, or any other machine tools, equipment, apparatus, tool or device used to join, cut, drill, manipulate, fold, finish, clean, spray, or otherwise work the textile material.
For the purposes of this specification, a “textile” or “textile material” is intended to encompass any material or fabric with a woven substrate which may or may not be coated with a polymer to enhance its properties (e.g. to make it more easily welded, to provide a gas barrier, a weather barrier, etc.). The term “textile” or “textile material”, as used herein, is also intended to include more generally any flexible material whether woven, non-woven, and even an unreinforced film with no substrate. For example, “textiles” or “textile materials” may include any flexible plastic material such as polyamides, polyimides, polyethylene derivatives, polyvinylchloride (PVC), polyurethane films, polyester and polyurethane coated fabrics. A “textile structure”, as the expression is used herein, is therefore any structure made of (or incorporating) such a textile or textile material, and is meant to include any component, subcomponent, assembly, subassembly or part that is constructed or used to form a textile structure.
Alternatively, in another embodiment such as the one depicted in
As further shown in
As depicted in the embodiment of
The machines depicted for example in
The cantilevered cranes, which are depicted for example in the figures, may move freely on casters, wheels, rollers, etc. or along a guide rail mounted for example on the floor (8), either manually or via a motor drive (13). In one particular embodiment, the motor drive may be synchronized to the desired welding speed.
In one embodiment, a control system comprising sensors and a processor for executing a control algorithm that may be provided to control the displacement of the motor drives (12, 13).
In embodiments of the present invention, the work surface (1) of the manufacturing system has a ventilated upper surface (14) with a chamber or chambers underneath (15). The chambers may be pressurized (with a pressure P) with a gas such as air from a fan system (16) or equivalent to create a stream of air (17) underneath the textile structure (3) under construction. This creates a cushion of air under the textile structure allowing it to ‘hover’ and thus to be easily moved (while the textile structure is hovering) into a desired position with minimal effort. For the purposes of this specification, to “hover” means to float or remain aloft in the air at a substantially constant vertical position or elevation relative to the ground or a work surface. When the textile structure hovers, there is a small gap or space between the bottom of the textile structure and the ground or work surface such that the textile structure does not contact the ground or work surface while hovering. While hovering, the lift force produced by the pressurized air is equal and opposite to the weight of the structure, thereby placing the structure is vertical equilibrium. The hovering of the textile structure minimizes the possibility of damage to the fabric. Alternatively, the chambers may be evacuated of air to create a vacuum (V) beneath the textile structure to stabilize its position, i.e. to immobilize the textile structure. For the purposes of the specification, it is understood that a vacuum includes a partial vacuum. One such exemplary arrangement is depicted for example in
In some embodiments of the present invention, as depicted in
In yet other embodiments of the present invention, as depicted by way of example in
In the embodiment depicted by way of example in
As shown by way of example in
In one embodiment, the system may comprise a means (air flow subsystem) to vary the air pressure. Variable air pressure may be used to support (hover) structures of different weight or to increase or decrease the hover elevation. Such a system may include a computerized control system to control air pressure based on the vertical position of the textile. For example, the control system may include a height or elevation sensor and a feedback control loop implemented in software executed by a processor the control system. This control system is thus able to control an elevation or vertical position of the textile structure. For example, an optical sensor may be used to measure an elevation of the structure over the work surface. The processor of the control system may then generate a control signal to the air flow subsystem to vary the pressure of the air, either by controlling an air compressor and/or by regulating an air supply valve. Controlling the air pressure enables the elevation over the work surface to be adjusted to ensure that the textile structure remains substantially vertically aligned with the welding machine or other manufacturing machine. Alternatively, the air collector boxes may include zones and valves so that air flows only when and where it is needed (e.g. for larger or smaller items). In another embodiment, the system may provide positive flow in some areas and negative flow in others so that part of the structure under construction may be hovered while, at the same time, vacuuming other parts of the structure to hold the structure in a fixed (stable) position.
The novel method and system disclosed herein may be applied to a broad variety of manufacturing processes. Some examples of how this novel method and system may be used in different applications are described below to illustrate the versatility of this novel method and system.
As a first example, this novel manufacturing method and system may be used for the fabrication of textile structures for the airship industry in which the textile structures (e.g. textiles made of polyesters and polyurethanes, etc) are impermeable to small gas molecules such as helium (He) or hydrogen (H2). Similarly, the process may be used for the sailboat industry.
As a second example, this novel method and system may be used for the fabrication of textiles for the solar-based transportation industry where solar cells or modules (or other electricity generating means) are integrated into the textile.
As a third example, this novel method and system may be used for the fabrication of textiles for the solar-based infrastructure industry where solar cells or modules (or other electricity generating means) are integrated into a textile. These textiles require structural integrity to withstand winds and the elements (e.g. military or disaster-relief tents). For inflatable tents, the textiles may also need to withstand the stress and strain of pressurization and depressurization cycles.
As a fourth example, this novel method and system may be used for the fabrication of textiles into which power generators and/or power storage elements are integrated.
As a fifth example, this novel method and system may be used for the fabrication of textiles with sensing capabilities (e.g. leak sensing, pressure sensing, etc).
As a sixth example, this novel method and system may be used for the fabrication of textiles with media capabilities such as flexible displays, banners, etc.
As a seventh example, this novel method and system may be used for the fabrication of textiles with deicing capabilities for the transportation and the infrastructure industries.
As an eighth example, this novel method and system may be used for the fabrication of textiles with self-cleaning capabilities for the transportation and the infrastructure industries.
As a ninth example, this novel method and system may be used for the fabrication of textiles with self-healing capabilities for the transportation and the infrastructure industries.
Other uses or applications of this novel technology will become apparent to those of skill in the art. Therefore, the examples presented above are not intended to restrict the uses of this technology.
It should be appreciated that wherever human operators are shown as being involved in the manufacturing process these human operators can be replaced by robotics for a fully automated manufacturing process.
It should also be appreciated that although the hovering is achieved using air, other gases e.g. nitrogen, may be used. In some embodiments, the air or other gas may be heated to increase lift. In other embodiments, self-contained portions or components of the textile structure may be fully or partially inflated with a lifting gas like hydrogen or helium.
This new technology has been described in terms of specific implementations and configurations which are intended to be exemplary only. Persons of ordinary skill in the art will appreciate that many obvious variations, refinements and modifications may be made without departing from the inventive concepts presented in this application. The scope of the exclusive right sought by the Applicant(s) is therefore intended to be limited solely by the appended claims.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/CA2012/001024 | 11/7/2012 | WO | 00 | 5/8/2014 |
Number | Date | Country | |
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61557018 | Nov 2011 | US |