The present technology relates generally to systems and methods for forming a tubular braid of filaments. In particular, some embodiments of the present technology relate to systems for forming a braid through the movement of vertical tubes, each housing a filament, in a series of discrete radial and arcuate paths around a longitudinal axis of a mandrel.
Braids generally comprise many filaments interwoven together to form a cylindrical or otherwise tubular structure. Such braids have a wide array of medical applications. For example, braids can be designed to collapse into small catheters for deployment in minimally invasive surgical procedures. Once deployed from a catheter, some braids can expand within the vessel or other bodily lumen in which they are deployed to, for example, occlude or slow the flow of bodily fluids, to trap or filter particles within a bodily fluid, or to retrieve blood clots or other foreign objects in the body.
Some known machines for forming braids operate by moving spools of wire such that the wires paid out from each spool cross over/under one another. However, these braiding machines are not suitable for most medical applications that require braids constructed of very fine wires that have a low tensile strength. In particular, as the wires are paid out from the spools they can be subject to large impulses that may break the wires. Other known braiding machines secure a weight to each wire to tension the wires without subjecting them to large impulses during the braiding process. These machines then manipulate the wires using hooks other means for gripping the wires to braid the wires over/under each other. One drawback with such braiding machines is that they tend to be very slow, since the weights need time to settle after each movement of the filaments. Moreover, since braids have many applications, the specifications of their design—such as their length, diameter, pore size, etc.—can vary greatly. Accordingly, it would be desirable to provide a braiding machine capable of forming braids with varying dimensions, using very thin filaments, and at high speed.
Many aspects of the present disclosure can be better understood with reference to the following drawings. The components in the drawings are not necessarily to scale. Instead, emphasis is placed on illustrating clearly the principles of the present disclosure.
The present technology is generally directed to systems and methods for forming a braided structure from a plurality of filaments. In some embodiments, a braiding system according to present technology can include an upper drive unit, a lower drive unit coaxially aligned with the upper drive unit along a central axis, and a plurality of tubes extending between the upper and lower drive units and constrained within the upper and lower drive units. Each tube can receive the end of an individual filament attached to a weight. The filaments can extend from the tubes to a mandrel aligned with the central axis. In certain embodiments, the upper and lower drive units can act in synchronization to move the tubes (and the filaments contained within those tubes) in three distinct motions: (i) radially inward toward the central axis, (ii) radially outward away from the central axis, and (iii) rotationally about the central axis. In certain embodiments, the upper and lower drive units simultaneously move a first set of the tubes radially outward and move a second set of the tubes radially inward to “pass” the filaments contained with those tubes. The upper and lower drive units can further move the first of tubes—and the filaments held therein—past the second set of tubes to form, for example, an “over/under” braided structure on the mandrel. Because the wires are contained within the tubes and the upper and lower drive units act in synchronization upon both the upper and lower portion of the tubes, the tubes can be rapidly moved past each other to form the braid. This is a significant improvement over systems that do not move both the upper and lower portions of the tubes in synchronization. Moreover, the present systems permit for very fine filaments to be used to form the braid since tension is provided using a plurality of weights. The filaments are therefore not subject to large impulse forces during the braiding process that may break them.
As used herein, the terms “vertical,” “lateral,” “upper,” and “lower” can refer to relative directions or positions of features in the braiding systems in view of the orientation shown in the Figures. For example, “upper” or “uppermost” can refer to a feature positioned closer to the top of a page than another feature. These terms, however, should be construed broadly to include semiconductor devices having other orientations, such as inverted or inclined orientations where top/bottom, over/under, above/below, up/down, and left/right can be interchanged depending on the orientation.
The frame 110 can generally comprise a metal (e.g., steel, aluminum, etc.) structure for supporting and housing the components of the system 100. More particularly, for example, the frame 110 can include an upper support structure 116 that supports the upper drive unit 120, a lower support structure 118 that supports the lower drive unit 130, a base 112, and a top 114. In some embodiments, the drive units 120, 130 are directly attached (e.g., via bolts, screws, etc.) to the upper and lower support structures 116, 118, respectively. In some embodiments, the base 112 can be configured to support all or a portion of the tubes 140. In the embodiment illustrated in
The system 100 operates to braid filaments 104 loaded to extend radially from the mandrel 102 to the tubes 140. As shown, each tube 140 can receive a single filament 104 therein. In other embodiments, only a subset of the tubes 140 receive a filament. In some embodiments, the total number of filaments 104 is one half the total number of tubes 140 that house the filament 104. That is, the same filament 104 can have two ends, and two different tubes 140 can receive the different ends of the same filament 104 (e.g., after the filament 104 has been wrapped around or otherwise secured to the mandrel 102). In other embodiments, the total number of filaments 104 is the same as the number of tubes 140 that house a filament 104.
Each filament 104 is tensioned by a weight secured to a lower portion of the filament 104. For example,
Referring again to
In some embodiments, the drive units 120, 130 are substantially identical and include one or more mechanical connections so that they move identically (e.g., in synchronization). For example, jackshafts 113 can mechanically couple corresponding components of the inner and outer drive mechanisms of the drive units 120, 130. Similarly, in some embodiments, one of the drive units 120, 130 can be an active unit while the other of the drive units 120, 130 can be a slave unit driven by the active unit. In other embodiments, rather than a mechanical connection, an electronic control system coupled to the drive units 120, 130 is configured to move the tubes 140 in an identical sequence, spatially and temporally. In certain embodiments, where the tubes 140 are arranged conically with respect to the central axis L, the drive units 120, 130 can have the same components but with varying diameters.
In the embodiment illustrated in
In some embodiments, the mandrel 102 can have lengthwise grooves along its length to, for example, grip the filaments 104. The mandrel 102 can further include components for inhibiting rotation of the mandrel 102 relative to the central axis L during the braiding process. For example, the mandrel 102 can include a longitudinal keyway (e.g., channel) and a stationary locking pin slidably received in the keyway that maintains the orientation of the mandrel 102 as it is raised. The diameter of the mandrel 102 is limited on the large end only by the dimensions of the drive units 120, 130, and on the small end by the quantities and diameters of the filaments 104 being braided. In some embodiments, where the diameter of the mandrel 102 is small (e.g., less than about 4 mm), the system 100 can further include one or weights coupled to the mandrel 102. The weights can put the mandrel 102 under significant tension and prevent the filaments 104 from deforming the mandrel 102 longitudinally during the braiding process. In some embodiments, the weights can be configured to further inhibit rotation of the mandrel 102 and/or replace the use of a keyway and locking pin to inhibit rotation.
The system 100 can further include a bushing (e.g., ring) 117 coupled to the frame 110 via an arm 115. The mandrel 102 extends through the bushing 117 and the filaments 104 each extend through an annular opening between the mandrel 102 and the bushing 117. In some embodiments, the bushing 117 has an inner diameter that is only slightly larger than an outer diameter of the mandrel 102. Therefore, during operation, the bushing 117 forces the filaments 104 against the mandrel 102 such that the braid 105 pulls tightly against the mandrel 102. In some embodiments, the bushing 117 can have an adjustable inner diameter to accommodate filaments of different diameters. Similarly, in certain embodiments, the vertical position of the bushing 117 can be varied to adjust the point at which the filaments 104 converge to form the braid 105.
The outer assembly 350 includes (i) outer slots (e.g., grooves) 354, (ii) outer drive members (e.g., plungers) 356 aligned with and/or positioned within corresponding outer slots 354, and (iii) an outer drive mechanism configured to move the outer drive members 356 radially inward through the outer slots 354. The number of outer slots 354 can be equal to the number of tubes 140 in the system 100, and the outer slots 354 are configured to receive a subset of the tubes 140 therein. In certain embodiments, the outer assembly 350 includes 48 outer slots 354. In other embodiments, the outer assembly 350 can have a different number of outer slots 354 such as 12 slots, 24 slots, 96 slots, or any other preferably even number of slots. The outer assembly 350 further includes a lower plate 351b opposite the upper plate. In some embodiments, the lower plate 351b can be attached to the upper support structure 116 of the frame 110.
In the embodiment illustrated in
As further shown in
The outer cam ring 352 includes an inner surface 365 having a periodic (e.g., oscillating) shape including a plurality of peaks 367 and troughs 369. In the illustrated embodiment, the inner surface 365 has a smooth sinusoidal shape, while in other embodiments, the inner surface 365 can have other periodic shapes such as a saw-tooth shape, trapezoidal, linear trapezoidal, or any cut pattern containing a transition between a peak and a valley (for example, any of the patterns illustrated in
As further shown in
In operation, the outer drive members 356 are driven radially inward by rotation of the periodic inner surface 365 of the outer cam ring 352, and returned radially outward by the biasing members 398. The inner surface 365 is configured such that when the peaks 367 are radially aligned with a first set (e.g., alternating ones) of the outer drive members 356, the troughs 369 are radially aligned with a second set (e.g., the other alternating ones) of the outer drive members 356. Accordingly, as seen in
The inner assembly 370 includes (i) inner slots (e.g., grooves) 374, (ii) inner drive members (e.g., plungers) 376 aligned with and/or positioned within corresponding ones of the inner slots 374, and (iii) an inner drive mechanism configured to move the inner drive members 376 radially outward through the inner slots 374. As shown, the number of inner slots 374 can be equal to the number of outer of outer slots 354 (e.g., 48 inner slots 374) such that the inner slots 374 can be aligned with the outer slots 354. The inner assembly 370 can further include a lower plate 371b that is rotatably coupled to an inner support member 373. For example, in some embodiments, the rotatable coupling comprises a plurality of bearings disposed in a circular groove formed between the inner support member 373 and the lower plate 371b.
In the embodiment illustrated in
The inner assembly 370 further includes an inner assembly motor 375 configured to rotate the inner assembly 370 relative to the outer assembly 350. This rotation allows for the inner slots 374 to be rotated into alignment with different outer slots 354. The operation of the inner assembly motor 375 can be generally similar to that of the outer cam ring motor 358 and the inner cam ring motor 378.
As further shown in
The inner cam ring 372 includes an outer surface 385 having a periodic (e.g., oscillating) shape including a plurality of peaks 387 and troughs 389. In the illustrated embodiment, the outer surface 385 includes a plurality of linear ramps, while in other embodiments, the outer surface 385 can have other periodic shapes such as a smooth sinusoidal shape, saw-tooth shape, etc. (for example, any of the patterns illustrated in
As further shown in
In operation, similar to the outer drive members 356, the inner drive members 376 are driven radially outward by rotation of the periodic outer surface 385 of the inner cam ring 372, and returned radially inward by the biasing members 398. The outer surface 385 is configured such that when the peaks 387 are radially aligned with a first set (e.g., alternating ones) of the inner drive members 376, the troughs 389 are radially aligned with a second set (e.g., the other alternating ones) of the inner drive members 376. Accordingly, as seen in
As illustrated in
Notably, each of the drive members in the system 100 is actuated by the rotation of a cam ring that provides a consistent and synchronized actuation force to all of the drive members. In contrast, in conventional systems where filaments are actuated individually or in small sets by separately controlled actuators, if one actuator is out of synchronization with another, there is a possibility of tangling of filaments. Moreover, because the number of inner slots 374 and outer slots 354 is the same, half the tubes can be passed from the inner slots 374 to the outer slots 354, and vice versa, simultaneously. Likewise, the use of a single cam ring for actuating all of the outer drive members, and a single cam ring for actuating all of the inner drive members, significantly simplifies the design. In other configurations, the inner and outer cams can each contain multiple individually controlled plates: one cam per set per inner/outer assembly. Using multiple cams per inner/outer assembly allows increased control of tube movement and timing. These alternative configurations would also allow for both sets to be entirely loaded into either the inner or outer ring all at once, if necessary (as shown in, for example,
The lower drive unit 130 has components and functions that are substantially the same as or identical to the upper drive unit 120 described in detail above with reference to
In general, the upper drive unit 120 is configured to drive a first set of the tubes 140 in three distinct movements: (i) radially inward (e.g., from the outer slots 354 to the inner slots 374) via rotation of the outer cam ring 352 of the outer assembly 350; (ii) radially outward (e.g., from the inner slots 374 to the outer slots 354) via rotation of the inner cam ring 372 of the inner assembly 370; and (iii) circumferentially relative to a second set of the tubes 140 via rotation of the inner assembly 370. Moreover, as explained in more detail below with reference to
Referring first to
Referring next to
Referring next to
Next, as shown in
Finally, referring to
The steps illustrated in
As described above, cam rings in accordance with the present technology can have various periodic shapes for driving the drive members radially inward or outward.
In some embodiments, for example, lower pick counts improve flexibility, while higher pick counts increases longitudinal stiffness of the braid 105. Thus, the system 100 advantageously permits for the pick count (and other characteristics of the braid 105) to be varied within a specific length of the braid 105 to provide variable flexibility and/or longitudinal stiffness. For example,
Several aspects of the present technology are set forth in the following examples.
1. A braiding system, comprising:
2. The braiding system of example 1 wherein—
3. The braiding system of example 1 or 2 wherein the inner and outer drive mechanisms are configured to rotate the inner and outer cams to substantially simultaneously (a) drive the first set of the tubes from the outer slots to the inner slots and (b) drive the second set of the tubes from the inner slots to the outer slots.
4. The braiding system of any one of examples 1-3 wherein—
5. The braiding system of example 4 wherein—
6. The braiding system of example 5 wherein the first and second sets of the outer drive members include the same number of outer drive members.
7. The braiding system of any one of examples 4-6 wherein—
8. The braiding system of any one of examples 4-7 wherein the first and second sets of the inner drive members include the same number of inner drive members.
9. The braiding system of any one of examples 4-8 wherein—
10. The braiding system of any one of examples 1-9 wherein the inner and outer assemblies are substantially coplanar, and wherein the inner assembly is rotatable relative to the outer assembly.
11. A method of forming a tubular braid, the method comprising:
12. The method of example 11 further comprising, after substantially simultaneously driving the inner and outer cams, rotating the inner assembly to rotate the second set of elongate members relative to the first set of elongate members.
13. The method of example 11 or 12 wherein rotating the inner assembly includes rotating the inner assembly in a first direction to rotate the first set of elongate members relative to the second set of elongate members, and wherein the method further comprises:
14. The method of any one of examples 11-13 wherein—
15. A braiding system, comprising:
16. The braiding system of example 15 wherein the upper drive unit constrains the upper portions of the elongate members, and wherein the lower drive unit constrains the lower portions of the elongate members.
17. The braiding system of example 15 or 16 wherein the upper and lower drive units are further configured to move the elongate members along an arcuate path with respect to the longitudinal axis.
18. The braiding system of any one of examples 15-17 wherein the upper and lower drive units are substantially identical.
19. The braiding system of any one of examples 15-18 wherein the upper and lower drive units are mechanically synchronized to move together.
20. The braiding system of any one of examples 15-19 wherein—
The above detailed descriptions of embodiments of the technology are not intended to be exhaustive or to limit the technology to the precise form disclosed above. Although specific embodiments of, and examples for, the technology are described above for illustrative purposes, various equivalent modifications are possible within the scope of the technology as those skilled in the relevant art will recognize. For example, although steps are presented in a given order, alternative embodiments may perform steps in a different order. The various embodiments described herein may also be combined to provide further embodiments.
From the foregoing, it will be appreciated that specific embodiments of the technology have been described herein for purposes of illustration, but well-known structures and functions have not been shown or described in detail to avoid unnecessarily obscuring the description of the embodiments of the technology. Where the context permits, singular or plural terms may also include the plural or singular term, respectively.
Moreover, unless the word “or” is expressly limited to mean only a single item exclusive from the other items in reference to a list of two or more items, then the use of “or” in such a list is to be interpreted as including (a) any single item in the list, (b) all of the items in the list, or (c) any combination of the items in the list. Additionally, the term “comprising” is used throughout to mean including at least the recited feature(s) such that any greater number of the same feature and/or additional types of other features are not precluded. It will also be appreciated that specific embodiments have been described herein for purposes of illustration, but that various modifications may be made without deviating from the technology. Further, while advantages associated with some embodiments of the technology have been described in the context of those embodiments, other embodiments may also exhibit such advantages, and not all embodiments need necessarily exhibit such advantages to fall within the scope of the technology. Accordingly, the disclosure and associated technology can encompass other embodiments not expressly shown or described herein.
This application is a 35 U.S.C. § 371 U.S. National Phase application of International Patent Application No. PCT/US2018/055780, titled “BRAIDING MACHINE AND METHODS OF USE,” filed Oct. 13, 2018, which claims the benefit of U.S. Provisional Patent Application No. 62/572,462, titled “BRAIDING MACHINE AND METHODS OF USE,” filed Oct. 14, 2017, the contents of which are hereby incorporated by reference in their entireties.
Filing Document | Filing Date | Country | Kind |
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PCT/US2018/055780 | 10/13/2018 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2019/075444 | 4/18/2019 | WO | A |
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