The present invention relates to the production of thin film seams, a method of manufacturing thin film seams, and a system for manufacturing such seams.
High altitude balloons include manned and unmanned balloons that may be released at ground level and climb into the troposphere, stratosphere, and even the mesosphere. High altitude balloons are filled with a lifting gas or with air that is maintained at an internal temperature that is higher than the surrounding atmospheric air temperature, thus generating lift. High altitude balloons are often made up of a number of “gores” attached to each other. The term “gore” refers to a tapering sector of a curved surface, such as the tapering panels of a hot-air balloon, a parachute, a beach ball, or a conventional plastic film high altitude balloon. Gored balloons are formed by carefully cutting and heat sealing gores to each other to form the balloon body, often referred to as the envelope. “Non-gored” high altitude balloons are made up of alternatively shaped film panels, such as flat round panels, although the seaming or joining techniques used in both types of high altitude balloons are similar.
High altitude balloon envelopes have been manufactured by heat sealing together tens, dozens, and even up to hundreds of plastic film gores together along the gore perimeters. Most of the plastic films in use include semi-crystalline plastics, with polyethylene (PE) being perhaps the most commonly used plastic high altitude balloon film to date. Conventional heat sealing machines used in the high altitude ballooning industry include continuous band heat sealers, impulse heat sealers, heated wheel sealers, and radio frequency (RF) heat sealers. Ultrasonic sealing, however, has not become a viable sealing technology for high altitude balloon film splicing even though it might, at first glance, seem to be an effective approach.
Various obstacles have kept ultrasonic sealing technology from being an effective tool in forming seams in high-altitude balloons. One obstacle is that conventional ultrasonic technologies generally produce a seam having weak seam strength. Further, the materials being sealed together experience a deterioration of their elongation to break properties. In other words, prior art attempts to ultrasonically weld balloon seams result in seams that either easily peel apart, unzip apart, or snap apart after relatively low force and elongation have been applied (as compared to balloon film seams created with alternative heat sealing technologies). Many major manufacturers of ultrasonic sealing equipment expressly acknowledge (e.g., in their company literature) that semi-crystalline plastics (such as polyethylene) are not suitable for ultrasonic welding. If not stating that semi-crystalline plastics are wholly unsuitable, such companies will instead give semi-crystalline films one of the lowest ratings on the scale of plastic weld suitability for ultrasonic welding processes.
Another major difficulty that has hampered the use of ultrasonic sealing and other semi-crystalline sealing industries has been the narrow margin of error for proper sealing parameters. There is very fine line between either under-welding or over-welding semi-crystalline films with ultrasonic techniques, and these parameters are often thrown into disarray if even the most minor of modifications is made to the structure and/or thickness of the base films being sealed together.
Embodiments of the present invention address these and other problems and enable semi-crystalline plastic films to be successfully welded at high performance standards using ultrasonic processes and techniques. Further, embodiments of the present invention open up the range of suitable ultrasonic parameters that can be used on varying film structures and thicknesses while still obtaining a strong peel resistant and elongatable seal.
The inventor of the embodiments of the present disclosure has recognized that there are various problems in joining thin film materials, such as semi-crystalline polymer materials. Some of those problems are discussed above and involve issues of seal strength, seal elongatability, and reliability while others involve issues relating to material characteristics and limitations of currently available manufacturing processes. Embodiments of the present invention provide innovative and productive solutions relating to the joining of thin film materials. These solutions are applicable to a variety of industries including, for example, the manufacture of high altitude balloons and the production of consumer and industrial packaging for both food and non-food products.
For example, embodiments of the present specification may make the speed advantages of ultrasonic sealing technology accessible to high altitude ballooning and other industries where thousands of feet of reliable, consistent, and fault-proof seams are required. Where current high altitude balloon sealing technologies, such as continuous band sealing and impulse sealing, may be able to produce, for example, ten or twenty feet of a given seam per minute, embodiments of the present invention may enable the production of seams at a rate of dozens, and even hundreds, of feet per minute. The applicant believes that balloon sealing speeds can be improved by a factor of up to 10 (or more) when utilizing one or more embodiments of the current specification. This significant increase in production, while maintaining (or even improving) seam reliability, can help to drive down unit-balloon envelope costs and reduce overhead and multi-line capital expenditures currently required in the manufacture of high altitude balloons.
Further, at least some embodiments of the present specification enable increased automation in the high altitude balloon manufacturing process. For example, in some applications, analog and digital inputs and outputs of ultrasonic high-frequency vibrations can be controlled on the fly faster and more accurately than currently used continuous band sealers, or hot wheel or impulse sealing machines. Waiting for a band sealer or hot wheel sealer's heating element to increase or decrease temperature at the weld surface will likely be deemed unacceptable in the industry where, in some instances, the near-immediate and precise increase or decrease in ultrasonic frequency vibration adjustments is available as a viable option. For example, where a constant band sealer or hot wheel sealer may require 10 minutes to warm up and 10 minutes to cool down, some ultrasonic welding embodiments can be ready for use in the matter of less than a second.
In addition to the advantages that may be provided in manufacturing efficiency and cost, the resulting seams may provide enhanced reliability and strength. As discussed in further detail below, a seam formed in accordance with some embodiments of the present specification may provide a tensile peel strength that is as strong, or in some cases even stronger, than the tensile strength of the same material in a virgin or non-joined state. In some embodiments, such is accomplished by having a seem having a central weld zone that is flanked by one or more reinforcing perimeter beads as will be further detailed below.
Embodiments of the present invention include seams formed in thin film material layers, systems for forming seams in thin film material layers, and methods of joining thin film material layers. Such material layers may include, for example, semi-crystalline polymers such as polyethylene, polypropylene, polyester, and nylon.
In accordance with one embodiment of the invention, a system is provided for forming ultrasonic welds. The system includes a sonotrode, an anvil positioned adjacent the sonotrode, and at least one heat-carrier layer contacting at least one of a surface of the sonotrode and a surface of the anvil.
In one embodiment, the heat-carrier layer comprises thermally conductive rubber silicone.
In one embodiment, the heat-carrier layer comprises a material selected from the group consisting of: metallic film, amorphous polymeric film, and semi-crystalline polymeric film.
In one embodiment, the heat-carrier layer comprises a material layer comprising polyurethane.
In one embodiment, the heat-carrier layer comprises a material layer comprising polytetrafluoroethylene.
In one embodiment, at least one of the sonotrode and the anvil comprises a rotary wheel.
In one embodiment, the heat-carrier layer includes a continuous strip of material fed between the sonotrode and the anvil.
In one embodiment, the heat-carrier layer includes a circuitous member extending about at least one of the sonotrode and the anvil.
In one embodiment, the system further includes a first pulley, wherein the circuitous member of the first heat-carrier layer extends about the first pulley.
In one embodiment, the system further includes a first compression member adjacent the sonotrode and a second compression member adjacent the anvil.
In one particular embodiment, the at least one heat-carrier layer includes a first heat-carrier layer contacting a surface of the sonotrode and a second heat-carrier layer contacting a surface of the anvil.
In accordance with another embodiment of the invention, a material assembly is provided. The material assembly comprises a first semi-crystalline film layer, a second semi-crystalline film layer and a seam joining the first semi-crystalline film layer and the second semi-crystalline film layer. The seam comprises a welded zone and at least one reinforcing seam bead adjacent the welded zone.
In one embodiment, the seam exhibits a peel tensile strength of between approximately 50% and approximately 120% of a tensile strength of at least one of the first and second semi-crystalline film layers.
In one embodiment, the seam exhibits an elongation-to-break strength of between approximately 50% and approximately 120% of an elongation-to-break strength of at least one of the first and second semi-crystalline film layers.
In one embodiment, the seam exhibits a yield strength of between approximately 50% and approximately 120% of a yield strength of at least one of the first and second semi-crystalline film layers.
In one embodiment, the welded zone includes a patterned weld.
In accordance with another embodiment of the present invention, a method is provided for joining two layers of material. The method comprises overlaying a portion of a first semi-crystalline film on a portion of a second semi-crystalline film, subjecting at least one heat carrier layer to ultrasonic energy to generate heat within the at least one heat-carrier layer, and contacting the overlaid portion of the first and second semi-crystalline films with the at least one heat-carrier.
In one embodiment, the method further comprises forming a seam in the overlaid portion of the of the first and second semi-crystalline films, the seam including a welded zone and at least one reinforcing perimeter bead adjacent the welded zone.
In one embodiment, the act of contacting the overlaid portion of the first and second semi-crystalline films with at least one heat-carrier layer includes contacting the overlaid portion of the first and second semi-crystalline films with at least one layer of thermally conductive silicone rubber.
In one embodiment, the method further comprises applying pressure to the overlaid portion of the first and second semi-crystalline films via the at least one heat-carrier layer subsequent to the act of subjecting the at least one heat-carrier layer to ultrasonic energy.
In one embodiment, the method further comprises subjecting the overlaid portion of the first and second semi-crystalline films to ultrasonic energy.
In accordance with another embodiment of the present invention, another method is provide for joining two layers of material. The method comprises overlaying a portion of a first semi-crystalline film on a portion of a second semi-crystalline film, inducing internal heat in a central weld zone of the overlaid portion of the first semi-crystalline film and the second semi-crystalline film, and inducing external heat in a perimeter of the central weld zone.
In one embodiment, the act of inducing internal heat in a central weld zone includes subjecting the overlaid portion of the first semi-crystalline film and the second semi-crystalline film to ultrasonic energy.
In one embodiment, the act of inducing external heat in a perimeter of the central weld zone includes transferring heat to the perimeter of the weld zone from a heat-carrier layer.
In one embodiment, the method further comprises heat into the heat-carrier layer by subjecting the heat-carrier layer to ultrasonic energy.
In one embodiment, the act of transferring heat to the perimeter of the weld zone from a heat-carrier layer includes transferring heat from a layer of thermally conductive silicone rubber.
In one embodiment, the act of transferring heat to the perimeter of the weld zone from a heat-carrier layer includes transferring heat from a layer of polytetrafluoroethylene.
Additional embodiments, features, and aspects are described below. It is to be understood that the scope of the invention is to be measured by a given claim as issued and not by whether it addresses an issue in the Background section or provides a feature or aspect in this Brief Summary section. It is also noted that the embodiments described herein are not to be considered mutually exclusive of one another and that any feature, aspect, or component of one embodiment described herein may be combined with other features, aspects, or components of other embodiments.
The applicant's preferred and some other embodiments are disclosed in association with the accompanying Figures in which:
Illustrative embodiments presented herein include embodiments directed toward high altitude balloons, including hermetically sealed superpressure balloons and zero-pressure balloons. However, other balloons and other non-balloon inflatables, consumer packaging goods, and commercial sheeting products may also be manufactured in accordance with principles and embodiments described in the present disclosure.
At least some embodiments of the present specification enable ultrasonically welded semi-crystalline polymer film seams to achieve greatly improved peel seam tensile strength and increased elongation-to-break in material assemblies that may be used in a variety of constructions including high-altitude balloons, consumer packaging, and other products that require heat sealing of two or more semi-crystalline polymer film layers.
In their most basic form, ultrasonic plastic welding machines are conventionally built from an ultrasonic stack and an anvil. The ultrasonic stack includes a converter, a booster, and a sonotrode. The sonotrode is often referred to as an ultrasonic horn. The converter converts an electrical signal into a mechanical vibration. The booster modifies the amplitude of the vibration. The sonotrode applies the mechanical vibration to the parts that are to be welded. The anvil is on the opposing side of the parts (e.g., material film layers) being welded from where the sonotrode is located and enables the high frequency vibration to be directed to the part interfaces. In one embodiment, an electronic ultrasonic generator delivers a high power AC (alternating current) signal with a frequency matching the resonance frequency of the stack. A controller controls the movement of the components, the application of pressure, and the delivery of the ultrasonic energy to the pieces being welded. The pieces being sealed together are often held under pressure during the ultrasonic vibration step, though in other processes a gap may also be run between the sonotrode and the anvil for far-field welding as opposed to near-field welding (where there is direct mechanical pressure between the sonotrode, the film, and the anvil). A multitude of ultrasonic sonotrode and anvil types and shapes are known. Much of the present disclosure will use the example of a rotary (wheel) sonotrode and anvil. However, the present specification is not limited to such rotary wheel configurations as ultrasonic welding can use flat, cylindrical, or irregularly shaped pieces, smooth or patterned sonotrode and anvil surfaces, index sealing and continuous sealing movements, among a variety of other ultrasonic sealing configurations. Many present day ultrasonic sonotrodes and anvils are made from metal and alloy bases, such as titanium, steel, aluminum, etc.
In ultrasonic plastic film welding, high-frequency mechanical vibrations pass though the plastic films and create frictional heat where the film layers come into contact as they pass between the sonotrode and the anvil. There are two primary types of polymers that can be ultrasonically welded: amorphous and semi-crystalline polymers. Amorphous polymers, arranged in random molecular chains, have a wide melt temperature range that enables the material to slowly soften and flow without solidifying too early after minor fluctuations in seal temperature. Because of these properties, amorphous polymers are able to consistently create successful welds under many ultrasonic welding parameters. Examples of amorphous polymers are ABS, Acrylic, Polycarbonate, and PVC. Many of these materials are not commonly used as sealant layers in, for example, the high altitude balloon and packaging goods industries.
The term “semi-crystalline” refers to a polymer with both amorphous and crystalline properties. Semi-crystalline polymers materials have a sharper melting temperature, meaning that they have a much narrower melt temperature range than amorphous polymers and in which they can soften and flow. This makes it harder to achieve a good quality weld without either under-welding or over-welding the films. The molecules of the semi-crystalline polymer films are more orderly and make transmission of the ultrasonic mechanical vibrations difficult to control. Polyethylene, polypropylene, polyester (including polyethylene terephthalate (PET) also known as Mylar®) and nylon are examples of semi-crystalline polymers. As mentioned above, polyethylene is the most commonly used high altitude balloon film material, and thus the at least some embodiments of the present specification may enable great manufacturing advances to be introduced into the industry. Polyethylene (PE) and polypropylene (PP) are two of the most common packaging industry sealant layers, as well, further offering alternative industry advantages of at least some embodiments of the present specification.
Ultrasonic sealing differs from other types of heat sealing in that the heat required to seal two layers together is generated from inside the sealing layers (inside the films being sealed together), rather than heat being introduced by conduction or convection from the outside. Outside heat energy is the primary heat supply for other methods of joining such as constant heat jaws, band sealers, hot wheel sealers, and impulse sealers.
Some embodiments of the present disclosure provide for both internal and external heat to be employed during the ultrasonic welding process. As will be further detailed below, the use of a sonotrode and anvil in sealing technologies is unique in that these components typically remain cold during the ultrasonic sealing process. Some embodiments of the present specification provide for heat generated from within the layers being sealed (by introduction of sonic energy into these material layers) as well as heat introduced from one or more outside sources to combine for a greater strength seal.
In one embodiment, one or more heat-carrier layers, such as thermally conducting silicone rubber strips, are disposed between the sonotrode and the anvil with the materials layers to be sealed then being placed in contact with the one or more heat-carrier layers. The ultrasonic sealing process creates vibrational heat both in the heat-carrier layers and the inner film layers that are to be sealed. Excess heat (generated in the heat-carrier layers) is conducted across the heat carrier layer surface area to be conducted into the internal film layers being sealed. This causes the resulting seam to extend beyond (or be wider than) the “weld width” of the sonotrode and anvil (the “weld width” being the width across which ultrasonic energy is applied by the sonotrode and the anvil). The combination of the internal film heat and the excess heat distributed by the heat-carrier layer provides a seam having a central weld zone (created by the ultrasonic energy or the internal heat) and at least one reinforcing seam perimeter bead at the edge of the central weld zone, the bead being formed from the external, distributed heat applied by heat-carrier layer. The result is, in some embodiments, a much stronger seam than a traditional ultrasonic seam formed without the use of a heat-carrier layer.
Testing procedures relevant to the present disclosure for comparative purposes include but are not limited to ASTM F88 PACKAGE SEAL STRENGTH TESTING and ASTM D882 TENSILE TESTING OF THIN PLASTIC SHEETING. In ASTM F88, a so-called “peel test” is conducted wherein, for example, the right edge (referring to the orientation of the materials in
In ASTM D882, a tensile test of a single sheet (or film) of material is conducted wherein a first edge is placed in a first grip of a tensile test machine and a second, opposing edge of the material sheet is placed in an opposing grip of the tensile test machine. The material sheet is then subjected to a specified tensile force applied at a specified rate until the sample fails. The data gathered in the test may be used to calculate various properties of the sample including tensile modulus (Young's Modulus) and the tensile strength of the material at failure.
Some embodiments of the current specification are directed toward increasing the peel strength, yield strength, and elongation to break properties of semi-crystalline polymer film seams. In one such embodiment, using peel tests and tensile sheet tests such as described above, the peel tensile strength of an ultrasonically welded seam may be approximately 50% of the tensile strength of the sheet material (i.e., the tensile strength of the virgin material prior to any seams being formed). In another embodiment, the peel tensile strength of an ultrasonically welded seam may be approximately 60% of the tensile strength of the sheet material. In another embodiment, the peel tensile strength of an ultrasonically welded seam may be approximately 100% of the tensile strength of the sheet material. In yet another embodiment, the peel tensile strength of an ultrasonically welded seam may be as much as approximately 120% of the tensile strength of the sheet material. Yield strength characteristics of exhibited ultrasonically welded seams constructed in accordance with embodiments of the present invention may likewise be approximately 50% to approximately 120% of the yield strength characteristics of the virgin sheet material. Elongation-to-break characteristics of exhibited ultrasonically welded seams constructed in accordance with embodiments of the present invention may likewise be approximately 50% to approximately 120% of the elongation-to-break characteristics of the virgin sheet material. Such characteristics may even be exhibited by some embodiments at temperatures as low as approximately −60 to −90° F.
The heat-carrier layers 201 and 202 may be made from a variety of different materials and exhibit a variety of different thicknesses. In one embodiment, thermally conductive rubber silicone may be used as a heat-carrier layer strip. Thermally conductive rubber silicone has a high temperature resistance, enabling it to transfer heat, generated from ultrasonic vibrations, across a portion of its surface area and toward internal polymer layers with a lower melt temperature. Many grades of thermally conductive rubber silicone have good memory and return back to their previous physical shape after having been subjected to substantial temperature and sealing pressure, thus enabling the material to be reused in additional ultrasonic sealing operations. An additional advantage of thermally conductive rubber silicone for a heat-carrier layer is that the silicone rubber surface can effectively grab and draw materials inward to mitigate against unwanted sonotrode/anvil-to-film layer slippage during sealing operations.
Other suitable materials for use as a heat-carrier layer include thin thermally conductive metallic films, such as copper and aluminum films. Thicker polymeric layers such as amorphous and semi-crystalline films, may also be used as stand-alone heat-carrier layers, or part of multi-layer heat-carrier laminates. Teflon® (polytetrafluoroethylene or PTFE) may be also used as stand-alone heat-carrier layers, or part of multi-layer heat-carrier layers. PTFE coated fiberglass or other PTFE coated and laminated materials may also be suitable heat-carrier layers due to their high temperature resistance and thermal conductivity properties. PTFE and other non-stick coatings may be added to the heat-carrier layers to allow for better release from the inner film layers being sealed together. Polymers such as polyurethane do not adhere well to other plastic films such as polyethylene, so adding a polyurethane layer to a heat-carrier layer, for example, may also ensure good seal release in certain embodiments.
Just as heat-carrier layers may be made from a wide variety of base materials and laminate layers, so too can they exhibit different geometries, cross-sectional profiles and sizes. For example, thermally conductive silicone rubber may be formed in flat strips, rolls of flat sheet material, tubes, wire, cords (solid tubes), belts, among other profile shapes. Likewise, other metallic and polymeric heat-carrier layers may be found in a multitude of different geometries, cross-sectional shapes, materials, and thicknesses to adapt to a required ultrasonic seam performance specification.
The heat-carrier layers 201 and 202 accommodate the transfer of applied heat from the ultrasonic mechanical vibrations (heat generated within the heat-carrier layers from application of ultrasonic energy) across a width of their surface area and transfer a portion of that heat down into the two or more semi-crystalline film layers that are disposed between the heat-carrier layers 201 and 202.
The reinforcing seam perimeter beads 204 and 205 extend beyond the sonotrode 101 and anvil 102 common surface area width 106. By incorporating one or more heat-carrier layers 201 or 202 during ultrasonic sealing of semi-crystalline films 103 and 104, the middle portion of the seam (the weld zone 203) achieves a more evenly distributed heat seal than it would by direct ultrasonic sealing without a heat-carrier layer. The seam perimeter beads 204 and 205 become reinforcing elements of the seam by utilizing excess heat transferred from the heat-carriers 201 and 202 to extend the film seam's width or area of melting beyond the width that a directly welded ultrasonic seam 105 (
Referring to
Referring to
The mechanically vibrating sonotrode 101 creates internal heat within the two film layers 103 and 104 and likewise creates heat within the heat-carrier layers 201 and 202. Due to the thermally conductive nature of some or all of the heat-carrier layer's material, excess heat 302 is spread across at least a portion of the heat carrier layers' surface area and down into the film layers 103 and 104 being sealed together. In certain embodiments of the current specification, the heat-carrier layers 201 and 202 act as an insulated oven of sorts, and increase the melt flow of the film layers 103 and 104 as well as the width of the seam 203, providing reinforcing seam perimeter beads 204 and 205 at locations that are laterally beyond the width that the sonotrode 101 and the anvil 102. Thus, at least some such embodiments of the current specification provide major ultrasonic seam performance improvements by protecting the film layers 103 and 104 from excessive heat, distributing heat more evenly across the seam, expanding the heating zone and providing one or more reinforcing beads when welding together two or more semi-crystalline film layers.
It is noted that while various embodiments described herein include two heat-carrier layers (e.g., heat carrier layers 201 and 202), that in certain embodiments, only a single heat-carrier layer may be used. For example, a heat carrier layer may be in contact with a sonotrode with one of the film layers being in contact with an anvil—the single heat carrier layer and the film layers passing between the anvil and sonotrode together. In another embodiment, a heat-carrier layer may be in contact with the anvil while one of the film layers is in contact with the sonotrode—again, the single heat carrier layer and the film layers passing between the anvil and sonotrode together. In yet another embodiment, one or more heat-carrier layers may be in contact with the sonotrode and anvil, receiving heat from the application of ultrasonic energy, while the film layers never directly interact with the anvil and/or sonotrode. Instead, the film layers may interact with the heat carrier layer or layers at a point in time following the one or more heat carrier layers being “heated” by the sonotrode. In such an embodiment, the film layers may be pressed between two previously energized heat-carrier layers, or they may be pressed between a single heat-carrier layer (previously energized) and another anvil or similar structure.
Ultrasonic heat sealing is typically characterized by a rapid cooling of the seam after the material leaves contact with the sonotrode 101 and the anvil 102.
Such control over sustained heat transfer to the internal layers enables the seam melt to over more area of the width of the seam (e.g., not just across the width where ultrasonic energy is applied between a sonotrode and an anvil) and provides for a wide variety of seam pressure and dwell time configurations to be utilized before the seam has fully resolidified. This can, in some applications, open up a host of opportunities to improvements in the seam strength and elongation to break properties of thin polymer films, most notably semi-crystalline films with the use of ultrasonic sealing technology.
By comparison, at least some embodiments of the present specification improve the performance metrics of ultrasonically welded film seams on semi-crystalline films. For example,
Performance variation between different heat seal types of semi-crystalline films is further illustrated in
Some embodiments of the present specification including the ultrasonic seam 602 depicted in
Referring now to
While the heat carrier layers 702 and 703 are shown as extending substantially across the entire width of the sonotrode 101 and the entire width of the anvil 102, in other embodiments, the heat-carrier layers 702 and 703 do not necessarily have to extend across the entire surface area of the sonotrode 101 or anvil 102. Rather, the heat-carrier layers may come into contact with only a portion of the width of the circumferential surface of the sonotrode 101 and/or anvil 102. The heat-carrier layers may also comprise several independent layers that collectively cover all of, or only a portion of, the sonotrode and/or anvil depending on a given seal design. For example, in some embodiments, it may be desirable to leave portions of the sonotrode and/or anvil circumferential surfaces area exposed (i.e., not entirely covered by a heat-carrier layer) in order to have direct ultrasonic access to the relevant film portions. Thus, as with any other embodiment described herein, heat-carrier layers may, if desired, fully cover one or more of a sonotrode and/or anvil surface areas in relation to the film layers being sealed, or they may only partially cover the sonotrode and/or anvil surface areas in relation to the film layers being sealed.
Referring to
In the embodiment shown
In other embodiments, the compression rollers 801 and 802 may be configured to rotate independent of the sonotrode 101 and the anvil 102, rotating on different axes and exhibiting different diameters. In one such an embodiment, pressure applied by the compression rollers 801 and 802 may be separated from, and independently controlled relative to the pressure applied by the sonotrode 101 and the anvil 102. In yet other embodiments, the placement of heat carrier layers may be varied such that all the compression rollers 801 and 802 have heat carrier layers extending across all, part or none of their widths and, similarly, heat carrier layers extending across all, part or none of the widths of the sonotrode 101 and the anvil 102, depending on the design of a particular seam being formed.
Another embodiment is illustrated by
In the embodiment shown in
Many embodiments have been described in terms of rotary ultrasonic heat seal systems. However the present disclosure is directed to other ultrasonic sealing embodiments as well, such as the non-rotary ultrasonic seal press as depicted in
Some embodiments include consumer packaging goods (CPGs) having semi-crystalline sealant layers, such as often is found in laminate film pet food bags 900 illustrated in
As previously noted, some high altitude balloon embodiments may also achieve improved seam tensile peel strength and elongation-to-break with ultrasonic heat seals formed in semi-crystalline sealant layers, such as often is found in a polyethylene film high altitude balloon 1000 as shown in
High altitude balloon embodiments may include the addition of common balloon components such as top (apex) balloon termination caps and/or tendon termination fittings 1007 and 1008, ballast chambers 1013, ballast control systems, payload lines 1009, payloads 1010, radar reflectors, inflation and deflation valves 1011, cut down systems, tracking systems, parachutes, and solar panels, among many other components and accessories used in the high altitude ballooning industry.
Other examples of products that can benefit from the increased seam strength and increased elongation to break of ultrasonically welded semi-crystalline films, include, but are not limited to, food packaging, agricultural and geomembrane covers, and tarps, among other products that require the mass heat sealing of polyethylene (PE), polypropylene (PP) and other semi-crystalline films. The present disclosure is not limited to semi-crystalline polymer films, as fully crystalline polymers, amorphous polymers and non-plastic materials may also find a substantial increase in bonding strength and/or seam elongation-to-break properties by use of aspects of the present specification. Polyurethane laminated fabric, used in blimps and aerostats for example, has also been found to achieve an increase in seam strength and elongation-to-break performance, using embodiments of the present disclosure during ultrasonic seam welding.
Referring to
The heat within the heat-carrier layer 1109 may then be transferred to an overlaid portion 1115 of two film layers 1117 and 1119 (e.g., two layers of semi-crystalline polymer material). The two film layers 1117 and 1119 may be placed on a backing structure 1121 so that pressure is applied to the overlaid portion 1115 between the heat-carrier layer 1109 and the backing structure. In such an embodiment, the heat generated by the sonotrode is applied to the overlaid portion 1115 of the film layers 1117 and 1119 only by way of the heat-carrier layer 1109. In other words, the overlaid portion 1115 is not subjected to ultrasonic energy during the joining or welding process.
In other embodiments, various alterations may be made to the system illustrated in
While specific embodiments have been shown by way of example in the drawings and have been described in detail herein. However, it should be understood that the invention is not intended to be limited to the particular forms disclosed. Indeed, features or elements of any disclosed embodiment may be combined with features or elements of any other disclosed embodiment without limitation. This specification includes all modifications, equivalents, and alternatives falling within the spirit and scope of the following appended claims and others supported by this specification.
This application claims the benefit of U.S. Provisional Patent Application No. 62/292,808, filed Feb. 8, 2016, entitled ULTRASONICALLY SEALED HIGH ALTITUDE BALLOON SEAM, the disclosure of which is incorporated by reference herein in its entirety. This application is also a continuation-in-part of U.S. Patent Application No. 14/746,835, filed Jun. 22, 2015, entitled HIGH ALTITUDE BALLOON AND METHOD AND APPARATUS FOR ITS MANUFACTURE, the disclosure of which is also incorporated by reference herein in its entirety.
Number | Date | Country | |
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62292808 | Feb 2016 | US |
Number | Date | Country | |
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Parent | 14746835 | Jun 2015 | US |
Child | 15186891 | US |