Exemplary embodiments of the present invention relate to a portable surgical system for regulating intra-operative environments over surgical sites; and to methods for implementing and using the same.
Over 25% of the global disease burden requires surgical therapy, which could prevent over 18 million deaths per year. These range from obstetric complications to traumas to infections to cancer and beyond. Yet 2 billion people have no meaningful access to safe surgical care, and 2-3 billion more have access only to unsterile surgeries in contaminated environments, leading to disproportionate rates of surgical infections. Innovations in this field typically focus upon making operating rooms and operating room ventilation systems more mobile, such as in tent format. However, such systems remain costly to purchase and to maintain. Moreover, such systems are difficult to transport rapidly to remote areas. At the same time, over 85,000 medical providers are infected by patient bodily fluids annually, with 90% of infected providers worldwide having been exposed while working in low-resource settings. While personal protective equipment mitigates these risks to some extent, there is a definite trade-off between the level of protection and both the cost as well as the user comfort, which is well-documented to correspond to user compliance. Thus, there is a need for systems and methods minimizing the intraoperative exposure to infectious risks, keeping of a clean operative environment, while maintaining the functionalities needed for performing safe surgical procedures.
Exemplary embodiments of the present invention aim to address both challenges of patient and provider intraoperative exposure to infectious risks by implementing an ultraportable system for intraoperative isolation and regulation of surgical site environments. The systems and methods enable the providing of self-contained, passive and active, bilateral barrier against exchange of contaminants between incisions and the greater surgical area. The systems may be enabled to provide a clean operating environment, proper airflow, proper pressurization, and proper disposal of contaminants. The system provides the access and functionalities necessary to performing safe surgical procedures.
The above information disclosed in this Background section is only for enhancement of understanding of the background of the invention and therefore it may contain information that does not form any part of the prior art.
Exemplary embodiments of the present invention provide a portable surgical system for regulating intra-operative environments over surgical sites.
In an exemplary embodiment it is disclosed a portable surgical system including a flexible enclosure separating a surgical environment inside the enclosure from an user environment outside the enclosure. The enclosure may include one or more areas of high optical clarity for viewing the inside of the enclosure. While the surgical system is deployed in use, only the surgical site is included within the surgical enclosure, and the remainder of the patient body is essentially excluded from the surgical environment inside the enclosure. The portable surgical system may further include an environmental control system configured to supply air to the enclosure such as to create essentially sterile conditions inside the enclosure and one or more ports for accessing the surgical site. The enclosure may further include an exhaust system configured to eliminate air from the enclosure. The exhaust system includes one or more exhaust-channels disposed on the side and along the enclosure. The exhaust-channels may further include a plurality of holes disposed on one or more lines along the exhaust-channels, the holes being configured to allow air to flow from the enclosure into the exhaust-channels and further into the environment outside the enclosure.
In an exemplary embodiment the exhaust-channels may include one or more exhaust-valves configured to adjust the airflow magnitude into the exhaust-channels. The exhaust-channels may include one or more exhaust-valves configured to adjust the airflow magnitude into the exhaust-channels. In an exemplary embodiment the environmental control system is configured to adjust the airflow magnitude into the air-supply-tube via a supply-valve. In an exemplary embodiment, the air-supply-tube may include one or more flow-guides, wherein each of the flow-guides is disposed on top of a corresponding perforation such as to guide the flow of air from the air-supply-tube into the enclosure. Each of the flow-guides may include a mini-valve configured to control the magnitude of the airflow through the corresponding perforation on which the flow-guides is disposed on. The environmental control system may to control the mini-valves via electrically controlled actuators.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory and are intended to provide further explanation of the invention as claimed.
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the principles of the invention.
The invention is described more fully hereinafter with reference to the accompanying drawings, in which embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure is thorough, and will fully convey the scope of the invention to those skilled in the art. In the drawings, the size and relative sizes of layers and regions may be exaggerated for clarity. Like reference numerals in the drawings denote like elements.
It will be understood that when an element or layer is referred to as being “on” or “connected to” another element or layer, it can be directly on or directly connected to the other element or layer, or intervening elements or layers may be present. In contrast, when an element or layer is referred to as being “directly on” or “directly connected to” another element or layer, there are no intervening elements or layers present. It will be understood that for the purposes of this disclosure, “at least one of X, Y, and Z” can be construed as X only, Y only, Z only, or any combination of two or more items X, Y, and Z (e.g., XYZ, XY, YY, YZ, ZZ).
The portable surgical system may include a plurality of ports, such as arm ports 8 and material ports 10 shown in
In the preferred embodiment shown in
The portable surgical system may include a surgical enclosure, a frame, and an environmental control system.
A. Structure of Surgical Enclosure
In an exemplary embodiment the surgical enclosure may be disposable, such as the enclosure 1 shown in
The panel of incise drape 11 may be incorporated into the bottom of the operating-section as shown in
Embodiments of the invention are described herein with reference to figures and illustrations that are schematic illustrations of idealized embodiments (and intermediate structures) of the invention. As such, variations from the shapes of the illustrations as a result, for example, of manufacturing techniques and/or tolerances, are to be expected. Thus, embodiments of the invention should not be construed as limited to the particular shapes of regions illustrated herein but are to include deviations in shapes that result, for example, from manufacturing.
The portable surgical systems disclosed herein may include alternate or additional sections which could be added based on procedural needs, such as to accommodate additional instrument trays or users. The above embodiments presented in this disclosure merely serve as exemplary embodiments and it will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the spirit or scope of the invention.
B. Structure of Frame
In an exemplary embodiment, illustrated in
In another exemplary embodiment the portable surgical system may include a frame 15 and tethers 14 as illustrated in
In an exemplary embodiment the portable surgical system may include a collapsible, rigid frame 16 and a flexible plastic enclosure 1 as illustrated in
In an alternate embodiment, the frame of
C. Ports
The various embodiments of the portable surgical system may have surgical enclosures which include a plurality of ports. The enclosure may include two major types of ports. The first type of port on the enclosure is arm ports 8, as shown in
The number of arm ports is dependent on procedural need. The preferred embodiments illustrated in
The second type of port on the enclosure is a materials port 10, as shown in
D. Environmental Control System
The portable surgical system includes an environmental control system. In a preferred embodiment, as the one shown in
In an alternative exemplary embodiment, the air supply system includes both an electrical fan 21 as well as a manual pump 27 as illustrated in
The external air supply system connects to the enclosure. In an exemplary embodiment, the air is supplied through an inlet and thereby blows through the entire enclosure cranially to caudally. Airflow adequacy may be checked by timing of inflation of the surgical enclosure 1 or by the rising of a windsock in the enclosure embodiment shown in
In a preferred exemplary embodiment the inlet is connected to a flexible tube, such as the overhead flexible tube 2 shown in
In a preferred exemplary embodiment, the flexible tube may include a plurality of perforations 3 disposed such as to create parallel, uniform streams of laminar air outflow into the enclosure. Uniform airflow is accomplished in our preferred embodiment, as described by the design and manufacturing implementations detailed in
Inventors in this application came to the realization that nearly uniform air flow may be accomplished when the perforation density along the tube decreases according to the inverse of an elliptically shaped function. Starting from the observation that the pressure within an inviscid flow will rise along a streamline if the velocity of the airflow decreases, inventors of this application have found that in a perforated tube of constant cross sectional area, the velocity within a tube will drop as it passes perforations from which flow is emanating, as long as the flow is of nearly constant density which will be the case for flows of air substantially below the speed of sound. Further, inventors have come to the realization that the pressure in a perforated tube rises as the distance from the source increases and, as a result, the rate of flow from each perforation rises with distance from the source assuming the perforations are of constant cross sectional area. As shown in
An exemplary embodiment of the invention discloses a flexible tube 2 (as shown by
The perforations are disposed along the flexible tube such that the axial positions of the perforations along the flexible tube may follow a mathematical relation (x1, x2, x3, x4, . . . xk)=Φ(V, d, D, ρ, k, L), where V is the air velocity from the source, D is the diameter of the tube, d is the diameter of the perforations, and ρ is an air density, L is the length of the perforated section, and k the number of perforations in a row. The mathematical relation Φ(V, d, D, ρ, k, L) is determined as explained hereinafter.
The positions of the perforations along the flexible tube may be expressed by a plurality of mathematical expressions: x1=Φ1(V, d, D, ρ, k, L); x2=Φ2(V, d, D, ρ, k, L); x3=Φ3(V, d, D, ρ, k, L); xk=Φk(V, d, D, ρ, k, L); where V is the air velocity from the source, D is the diameter of the tube, d is the diameter of the perforations, and p is an air density. The mathematical expressions Φ1(V, d, D, ρ, k, L), Φ2(V, d, D, ρ, k, L) . . . Φk(V, d, D, ρ, k, L) are determined as explained hereinafter and may be closed form expressions of (V, d, D, ρ, k, L).
The specific form of the perforation density needed for uniform air flow can be determined by an iterative computation.
The iterative computation may include a plurality of iterations, wherein each iteration includes a plurality of steps as described in
In a first step of the first iteration (see 40 in
where V is the axial air velocity at the source, D is the diameter of the tube, d is the diameter of the perforations, k is the number of perforations, and j is the index of the perforation or hole.
In a second step of the first iteration (see 41 in
Where ρ is the air density, d is the diameter of the perforations, D is the diameter of the tube. The equations above provide the velocities inside tube (i.e. v_tube1; v_tube2; v_tube3; . . . ; v_tubek).
In a third step of the first iteration (see 42 in
Then this value of the pressure P is used to estimate the pressures within the tube 42 at each of the many holes numbered j=1 to k as follows:
These pressures at each hole are computed and stored in a vector (ρ1, ρ2, ρ3 . . . pk).
In a fourth step of the first iteration (see 43 in
One may use the relationship above k times (for each hole number from 1 to k) to calculate exit velocity estimates at each perforation or hole (i.e. v_u1, v_u2, v_u3 . . . v_uk). The updated exit velocity estimates v_uj are different from the initially assumed distribution (i.e. v1, v2, v3, . . . vk).
By mass conservation, the sum of the exit velocities must obey the relationship
In a fifth step of the first iteration the exit velocity estimates calculated in the fourth step are used to calculate a set of velocities (v2-1, v2-2, v2-3, v2-4, . . . v2-k) to be used as starting point for a second iteration. The set of velocities are calculated as follows:
The set of velocities v2-j preserve the proportions among the calculated exit velocities v_uj but their magnitudes are adjusted to satisfy mass conservation by scaling each value. The scaling is performed by dividing each exit velocities by the sum Σj=1k(νj ρπd2/4) and multiplying it by the known mass flow supply which is (V ρπD2/4).
The resulting exit velocity distribution (v2-1, v2-2, v2-3, v2-4, . . . v2-k) is used as an updated estimate for a second iteration. The second through fifth steps (41 through 43 in
The density of the perforations 44 is determined by making it proportional to the inverse of the exit velocities. In an exemplary embodiment the position coordinates of the k perforations along the tube is denoted as x1, x2, x3, x4, . . . xk where xk is the distance between perforation k and a reference point on the tube between the air source and the first perforation. The positions xj (with j between 1 and k) may be calculated from the set of equations:
Where α is determined by setting the distance between the first and last perforation to the desired length: (xk−x1)=L.
The above equations enable the skilled artisans to derive the mathematical expressions x1=Φ1(V, d, D, ρ, k, L); x2=Φ2(V, d, D, ρ, k, L); x3=Φ3(V, d, D, ρ, k, L); . . . xk=Φk(V, d, D, ρ, k, L), thereby providing the positions and density of the perforations as function of parameters (V, d, D, ρ, k, L). The functions Φn(V, d, D, ρ, k, L) may be expressed by closed form expressions.
Alternatively, the set of parameters may be associated the resulting positions, (V, d, D, ρ, k, L)→(x1, x2, x3, x4, . . . xk), determined by the above algorithm thereby forming the function (x1, x2, x3, x4, . . . xk)=Φ(V, d, D, ρ, k, L). The function Φ(V, d, D, ρ, k, L) may be expressed by a closed form expression.
The positions and density of the perforations computed in the CPU 38 is implemented by a cutting die 45 which is located at positions over the clear plastic tube according to the desired perforation positions/density (i.e. x1, x2, x3, x4, . . . xk). The resulting perforations distribution will essentially follow an inverse of an elliptical function. By making the density of perforations an inverse of an elliptically shaped function, the resulting air distribution within the surgical area is uniform throughout providing an advantage in quality of the surgical outcome.
In an exemplary embodiment of the invention a method for manufacturing a portable surgical system may include: (1) running on a CPU the iterative computation described above; (2) receiving, from the CPU, at a machine for cutting perforations into the tube material a set of numbers corresponding to the positions (x1, x2, x3, x4, . . . xk) of the perforations; (3) cutting the perforations into the tube materials at positions (x1, x2, x3, x4, . . . xk) received from CPU.
As an illustration, the resulting velocity distribution and perforation density distribution are graphically depicted in
In another exemplary embodiment the above uniform air distribution can also be achieved via an alternative configuration of the perforations in the flexible tube as shown in
Another alternative embodiment of the air handling system inside the enclosure instead runs airflow longitudinally caudally to cranially, along center of top.
The portable surgical system may include a flexible tube 2 (as depicted in
The collapsible tube may be made of flexible material such as to switch from open to close state, and vice versa, based on airflow. The airflow passes from air supply system first through an inflow tube valve 2 comprising a sealed tube of collapsible plastic. When there is net positive airflow through the tube toward the manifold in this configuration, the transmural pressure is positive relative to the enclosure, and the tube is forced open. When there is no airflow or reversed airflow, the transmural pressure drops relative to the enclosure, causing longitudinal collapse of the tube. This tube valve reduces further flow in the setting of enclosure excess pressurization as the enclosure positive pressure produces transmural pressure favoring valve collapses; prevents flow reversal as enclosure positive pressure seals off air outflow through the valve; and also serves as an indicator of adequate airflow indicator by virtue of its inflation. The airflow then proceeds to a manifold 3, implemented as above in the horizontal manifold system. The relative lengths of the valve and manifold are determined by procedural needs for pressure and airflow; but the manifold should preferably extend at least the full length of the operating-section.
E. Method for Setup of Surgical Enclosure with Respect to Standard Surgical Workflow
An exemplary embodiment of the present invention also discloses a method for using the ultraportable surgical system comprising the steps described in
At the end of the procedure following any appropriate skin closure and dressing application, users remove the tray and any items from inside the enclosure, clear any blood or bodily fluids within the enclosure, doff gloves then remove arms from the arm ports, turn off the environmental control system, remove the air supply tubing from the air handling inlet, pull the enclosure off of the frame as well as off of the patient, and dispose of the enclosure.
For embodiment systems not utilizing incise drapes, setup methodology is described in
Although only a few embodiments have been described in detail above, those skilled in the art can recognize that many variations from the described embodiments are possible without departing from the spirit of the invention.
F. Supporting Studies
Inventors have implemented various embodiments, such as the ones described herein among others, by manufacturing and testing fully self-contained portable surgical systems. In Teodorescu et al (2016) inventors have demonstrated an early proof of concept and bench tested a functional prototype enclosure (
The features of the invention disclosed herein, as specified by actual surgical end-users, distinguish it from prior art by enhancing usability, ergonomics, independence from external resources, and reliability under field conditions. The inclusion within the enclosure of only the surgical site, excluding the remainder of the patient body from the sterile field, particularly high-contaminant regions such as the oropharynx or the genitals, improves the efficacy of the system. The invention's ability to isolate the surgical wound's contaminant production, such as blood and bodily fluids, and contain these through the life cycle of the product, is also a key feature.
It will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the spirit or scope of the invention. Thus, it is intended that the present invention cover the modifications and variations of this invention provided they come within the scope of the appended claims and their equivalent.
G. The Sterile Sleeves
The portable surgical system may further include sleeves for accessing the inside of the enclosure. As mentioned in the section C regarding “Ports” the second form for the arm port may include sleeves such as shown in
The sleeve material may include one or more layers of materials, such as, but not limited to: fabric, rubber, thermoplastics or a combination that may include fabric, plastic, surgical glove material, latex, polyurethane, polycarbonate, acetal copolymer polyoxymethlene, acetal homopolymer polyoxymethylene, acrylic, nylon, polypropylene, polystyrene, or thermoplastics that are sufficiently non-brittle to act as a cloth-like material. The layers may be configured to focus on ergonomics, ease of use, or functional properties. These layer's functional properties could include: material's ability to reduce heat retention, increase heat retention, wick up moisture, decrease friction, increase friction, or other properties that would benefit the comfort or functionality of the sleeve. For example, one or more of the layers may be made of a material such as to create a comfortable feel when touching a patient and such as to absorb/wick up moisture from inside the enclosure.
In an exemplary embodiment, the sleeve material may have the structure (and may be fabricated by the processes) described in the international patent application PCT/US19/32148 filed on May 14, 2019 and titled “Sterile Sleeves for Portable Surgical Systems” which is incorporated herein in its entirety for all purposes as if fully set forth herein.
An exemplary embodiment is described hereinafter with reference to
The sleeve may further include a mechanism 220 (
The sleeve may further include a removable sterile cover 205 (shown in
A method of using the portable surgical system is described hereinafter with reference to
H. The Exhaust and the Fluids and Debris Elimination System
The portable surgical system may include an exhaust system and a fluids and debris elimination system which are described hereinafter with reference to
(a). The Exhaust System
The exhaust system may include a set of exhaust channels 102 (as shown in
The channel outlets may include active components such as electromagnetically or mechanically controlled valves, filtering mechanisms, gates, or other devices designed to control fluid flow.
In an exemplary embodiment, the channels 102 may include a plurality of holes 104 (as shown by
In some exemplary embodiments, the holes 104 may be disposed at locations where they will be in direct proximity to a region of interest within the enclosure 1. The region of interest may be the surgical operating area within the enclosure 1. In some exemplary embodiments, the holes 104 may be disposed at locations where they will be away from the region of interest within the enclosure 1. The holes 104 may be disposed in close proximity to the region of interest such as to remove fluids surrounding the region of interest, to increase fluid flow over the region of interest, or to direct the fluid flow in a desired direction or velocity. The holes may be disposed to be away from the region of interest such as to decrease fluid flow over the region of interest or to direct the fluid flow in a desired direction or velocity. In other embodiments, the holes 104 may be designed to have different diameters, resistance to flow, or varying spacing such as to more finely tune the flow entering the exhaust channel 102. In an exemplary embodiment, the system is designed to maintain substantially constant efflux.
The total cross-sectional area of holes 104 (i.e. the sum of the cross-sections of all holes 104) may be chosen to be greater than the total cross-sectional area of the channel outlets (such as the outlets 502 or 503 in
The exhaust channel 102 may be configured to exhaust the airflow 401 (see
An essentially uniform airflow (as shown by 501 in
In an exemplary embodiment of the invention, an exhaust channels 102 (as shown by
The perforations are disposed along the channel such that the axial positions of the perforations along the flexible tube may follow a mathematical relation (x1, x2, x3, x4, . . . xk)=Φ(V, d, S, ρ, k, L), where V is the desired airflow velocity exiting the channel through the outlets, S is the cross-section area of the channel, d is the diameter of the perforations, and ρ is an air density, L is the length of the perforated section, and k the number of perforations in a row. The mathematical relation Φ(V, d, S, ρ, k, L) is determined via the same consideration as the ones explained with reference to the perforations in the flexible tube see e.g.
In an exemplary embodiment, an exhaust channel 102 further includes a channel outlet 502 which is in line with the channel 102 and with the airflow through the channel 102 (as shown in
The exhaust system may be configured such as to cause an efflux of fluid flow 501. The exhaust system may be configured such as to essentially prevent the influx of fluid, particulates and undesirable substances into the enclosure from the outer environment via the outlets. The exhaust system may be configured such that the positive pressure, coupled with the direction of flow changes, as well as with the particular geometries of the exhaust, essentially prevent the influx of fluid, particulates and undesirable substances into the enclosure from the outer environment via the outlets 502 or 503. The outlets 502 or 503 may be disposed in line with the fluid flow or orthogonal to the fluid flow in order to resist or permit fluid flow, increase or decrease static or dynamic fluid pressures, change direction of the exhausted fluids, improve user convenience, or to further resist the influx of undesired substances.
(b). The Debris and Fluids Elimination
In an exemplary embodiment, the debris and fluids elimination system includes one or more debris elimination channels 103 as shown in
The channels 103 may include a set of openings or perforations allowing blood, debris, bodily fluid, and other substances accumulated in the enclosure to enter into the channels 103. The fluid and debris elimination channels 103 may be disposed in the lower part of the enclosure (see e.g.
I. Redirecting Flow in the Flexible Tube
The flexible tube 2 of the environmental control system (described in this application at section D “Environmental Control System”) may be disposed with respect to channels 102 and 103 as shown in
A flow guide 120 may further include a mini-valve 130 for adjusting the airflow through the flow guide 120. In one embodiment the mini-valve 130 may include a cylindrical surface gliding over the openings 122 such as to adjust the opening size (as shown in
In an exemplary embodiment a flow guide 120 may include an outer cylinder 123 concentric with an the cylinder with perforations not too dissimilar to perforation 122. The perforation of the outer cylinder 123 may be configured to match in size with 122. If varied amounts of airflow are required, the outer concentric cylinder can be rotated to expose differing levels of overlapping perforations 122 and 123, effectively creating controlled volumes of airflow that are correlated to the amount of area of overlap. A higher level of perforation overlap of 122 and 123 would allow for more unobstructed airflow, whereas a lower levels of perforation overlap would result in a decreased airflow. The outer concentric cylinder could rotate via manual mechanical means with the user rotating and adjusting the level of overlap. Also, the level of overlap between 122 and 123 may be controlled by the environmental control unit 4. Such control may be permitted using actuators, motors, servos, piezo electronics, springs, memory alloys, or any combination of the above.
In another embodiment, the flow guiding system may direct airflow downwards from tube 2 with static openings and barriers 371 to the direction of flow in tube 2 which direct airflow through exit hole 121, as exemplified in
The shape, size, and orientation of a flow guiding system highly affects airflow. The flow guides may include a system configured to dynamically change the geometric properties of elements of the flow guiding system and the flexible tube 2. The flow guiding system may include materials that are deformable and which may be used in, around, or otherwise augmenting the structure of a flow guiding system or flexible tube 2. Materials that may be used include ductile metals, shape memory alloys, piezoelectric materials, photovoltaic materials, electroactive polymers, magnetorestrictive materials, magnetic shape memory alloys, smart inorganic polymers, pH-sensitive polymers, temperature-responsive polymers, halochromic materials, chromogenic systems, ferrofluids, photomechanical materials, polycaprolactone, self-heating materials, dielectric elastomers, magnetocaloric materials, thermoelectric materials, chemo responsive materials, or other materials that may deform through physical means such as bending, torsion, compressing, shearing, tension, or fatigue.
In a preferred embodiment, a flow guide 120 may include a memory shape alloy, for example Nitinol, lining the perimeter of perforations 122, allowing for the constriction or dilation of the perforations 122 when an electric current is passed through the alloy. This will serve to decrease airflow during constriction or increase airflow during dilation. Similarly the perforations included in airflow perforations 104, the bottom of the flow guide 120, the exit hole of 102, or augment exits 502 and 503 may include components made of memory shape alloys. For each of these perforations, they can be similarly controlled through introduced electrical current to allow for the deformation of the perforations as described above. In another embodiment, another such material that may be used is a temperature responsive polymer, whereby each of the perforations, openings and holes described above may be covered or lined with the temperature responsive polymer. Increasing airflow through openings may be achieved increasing the released heat, since introducing heat to the temperature responsive polymer causes it to deform and to dilate the openings. Many of the above materials may be used in similar manners such that when subjected to their responsive stimulus would cause them to act in similar ways. As described above, these stimuli may be introduced either directly from user intervention or through means of control from the environmental control unit.
The flow guides 120 and flexible tube 2 may also be geometrically modified or influenced using dynamic structures. Such dynamic structures reference geometries that are not reliant on solely material properties for changing geometries, but instead the particular means of constructing with a particular material that yields a structure that can affect the geometry of the flow guides 120 and flexible tube 2. Such structures may include inflatable air bladders that restrict, dilate, reorient, or otherwise modify the geometries of the flow guides 120 and the flexible tube 2. Such structures may exist in or around the flow guides 120 and flexible tube 2. Inflation methods may utilize a concurrent source of fluid flow from the environmental control unit or external solutions. Some external inflation modes may include compressed gas, a user blowing into the compartment, heating a material for expansion, or other reaction that causes material expansion or contraction.
In an exemplary embodiment, the walls within flow guide 120 and divider 129 may be two layered to allow for the entrapment of air. Using a separate channel, the environmental control unit may control the amount of air introduced into the compartment within flow guide 120 and dividers 129. Inflating structures 120 and 129 causes the expansion of the structures which causes the constriction of openings 122 and 121 and also decreases the volume within flexible tube 2, thereby resulting in an increased downstream resistance to airflow and causing an overall reduction in flow. The air source for the inflating structures may the same as for the surgical enclosure 1 or may be a separate air source.
In another embodiment, the flow guiding system and the flow guides 120 may include layers of material made of a memory shape alloy, such as Nitinol, wherein the layers are lining perforations 122. When an electrical current is introduced to the memory shape alloy, the layer of material will peel and curve away from the perforation 122 such that there is no longer any material preventing the inflow of air through flow guide 120. This dynamic structure may include multiple instances of this memory shape alloy such that differing levels of occlusion can be obtained. For instance, utilizing the passive shear strength of a Nitinol thread or rod, depending on the diameter, the Nitinol thread or rod will resist deflection. With this resistance to deflection, when multiple elements of Nitinol are included in the layer of material that occludes perforations 122, a differing number of Nitinol elements can be activated through electrical current. The deflection of any number of Nitinol elements would sum together and work against the summed strength of Nitinol elements that are not active, allowing the ratio of activation of nitinol elements to correlate to the level of deflection away from the perforation 122 and thereby allowing for finer control of level of obfuscation of the airway. This results in the ability to control the amount of airflow that passes through flow guide 120. In this embodiment, the nitinol activation could be either manually controlled by the user or controlled through the environmental control unit in any of the aforementioned described methods of control.
All of the above means for modifying geometries may also be used in reference to exhaust channels 102 and fluids elimination channels 103 to alter either exit fluid flow or the collection of waste products. These modifications can be made via physical user interaction with the surgical enclosure or via the environmental control unit. Any of the aforementioned environmental factors that are monitored by the sensors (e.g. pressures/airflows inside the enclosures, flexible tube and channels) as received and configured on the environmental control unit can be used as feedback to determine how the geometries of the components 120, 2, 102, and 103 should be altered to maintain an ideal steady state.
J. Monitoring and Controlling the Environment Inside the Surgical Enclosure
The surgical system may include a plurality of sensors for measuring the environmental conditions inside the surgical enclosure, outside the enclosure, the exhaust channels, the airflow supply tubes and channels and the fluids elimination channels. The sensors may include pressure sensors, airflow sensors, humidity sensors, and temperature sensors. The sensors may measure a plurality of environmental parameters such as: pressures at various locations of the enclosure, inside flexible tube 2, and in the channels 102 and 103; air-flow at various locations of the enclosure, inside the flexible tube 2, and in the channels 102 and 103; humidity; temperatures; and other environmental parameters as needed.
Information obtained from the sensors may be supplied to a computer system controlling the environmental control unit, valves and filters disposed on the channel outlets, and other controls. In response to the information received from the sensors, the computer system is configured to control the environmental control unit so as to adjust the airflow, temperature and humidity inside the surgical enclosure to the desired environmental parameters. In response to the information received from the sensors, the computer system is configured to control the valves and filters at the channel outlets such as to adjust the airflow and to eliminate out of the channels undesirable fluids and debris.
Additionally, the environmental control unit may be controlled in combination with user definable settings. These settings can be determined by continuous or discrete user definable set-points, or user selectable states. User definable states may include on, off, inflation, maintenance flow, high pressure, low pressure, dehumidify, cool, heat, brighten, or any other state that is intended to affect the measure of which is measured by one of the aforementioned sensors. By providing these set-points or states, the environmental control unit will be provided with user preferences that can be achieved by the control algorithm encoded in the computer system.
Flow may also be controlled via information received from flow sensors that correlate to laminar or turbulent flow. This information would provide the means for mechanically altering the output flow characteristics by modulating fan speed, fan blade pitch, fan blade shape, airfoil pitch, airfoil shape, baffle shape, baffle pitch, baffle permeability, aperture diameter, distance of fan to outlet, orientation of fan to outlet, shape of the outlet, or any combination of the aforementioned. By modulating these mechanical factors an effect on the flow downstream will be observed by the sensors so that the desired flow characteristics can be controlled for.
The environmental conditions inside the surgical enclosure 1 (e.g. pressures and airflow) may be adjusted to the desired state by modulating the sizes of holes 122, 121, 104, 502, 503, the diameters of 2 and 301, one or more of the geometry modifying mechanisms described above. For example, by decreasing the diameters of 104 and or 502 and 503, backpressure can build up inside the enclosure allowing for an increase of pressure within the main enclosure compartment 101, more rigidity in the walls of 1, and higher flow recirculation within the main compartment. The opposite would occur if diameters of 104 and/or 502 and 503 are increased. By increasing the size of the holes 121, 122, an increase of flow into the main chamber 101 will occur. If the holes 104, 502, and/or 503 remain the same, the effect would be similar to decreasing the diameters of 104, 502, and/or 503. The overall pressure within the compartment 101 is a result of the ratio of overall area shared across holes 122 and 121 with respect to holes 104, 502, and 503. If holes 104 are reduced in diameter but maintains an overall open area that is greater than 502 and 503, the velocity of the flow is increased when exiting the main chamber 101 and entering exhaust chamber 102. This state is useful if certain larger particulates need to be evacuated from the inside of main chamber 101. The opposite would occur if the diameters of 104 increase.
Reducing the velocity of airflow out of main chamber 101 into exhaust chamber 102 serves to prevent the evacuation of particles or elements that may need to remain inside main chamber 101. The ratio of openings 502 and 503 with respect openings 121 and 122 must remain such that the total area of the openings 121 and 122 is larger than the area of the openings 502 and 503 to maintain a pressurized main chamber 101. If it is desired to deflate the main chamber 101, a change in this ratio to have the area of the openings 502 and 503 be greater than openings 121 and 122 will yield this result. If the ratio of the area of the openings 121 and 122 remain larger than the area of the openings of 502 and 503 and the openings 121 and 122 decrease in area, this will achieve a higher pressure within flexible tube 2 and air inlet tube 301. This may be desired if the airflow is too high within the main chamber 101, or if the air pressure within flexible tube 2 or air inlet 301 is required to increase in order to maintain structural rigidity or to prevent occlusion from lack of internal pressure. This would provide a means to maintain the same amount of internal pressure in main chamber 101 while still increasing the internal pressures found within flexible tube 2 and air inlet 301.
In an exemplary embodiment, a flow guide 120 may further include a valve 123 for adjusting the airflow through the flow guide 120. In one embodiment the valve 123 may include a cylindrical surface gliding over the openings 122 such as to adjust the opening size (as shown in
In one embodiment, each of the flow guides 120 is paired with a valve which is actuated by means of a control such as actuators connected to one or a plurality of sensors 364 inside the enclosure 1 by means of one or several cable(s) 363.
In one embodiment, the sensors can be part of the enclosure wall and connect to a control unit 366 wirelessly. In another embodiment, the sensors 364 in the enclosure 1 sidewall may connect through wires replacing the flexible tubes 363 to the control unit 366 as in
In an exemplary embodiment, the control unit 366 is not hardware connected directly to the surgical enclosure sensors yet is instead an application receiving and sending data to the surgical enclosure, which may be run on separate hardware remotely, such as a portable computer, mobile phone, tablet, desktop computer, or server. In an alternate embodiment, the control unit 366 is not connected by means of a wire to sensors in the enclosure or to valves in the enclosure and instead includes its own microprocessor and wireless antenna to process information from sensors within the enclosure 1 and transmit inputs to control individual valves 123. The information from sensors as well as the state of individual control valves 123 may be shared with and processed remotely by a computer offsite, or with a mobile application running on a portable computer such as a tablet, mobile phone, or laptop computer.
The control unit 366 or a computer program functioning as a control unit for the valves 123 of the surgical enclosure may, in one embodiment, comprise predictive algorithms known to those skilled in the art such as a convolutional neural network, generative adversarial network, support vector machine, similarity learning, decision trees, or a combination of supervised and unsupervised algorithms in order to optimize airflow based on perceived visual signals, temperature signals, and/or pressure signals within the surgical enclosure 1. The surgical enclosure may relay this information to a server through a network connection, which server may then aggregate information from past surgeries and calculate an optimal airflow model which will be transmitted back to the enclosure. In another embodiment, the enclosure may run a control algorithm on site, through a connected hardware control unit 366 running an airflow control algorithm, algorithm which may be updated remotely with the latest trained model from a server aggregating data from prior surgeries from other surgical enclosures. In an embodiment, the surgical enclosure is single use, whereas the control unit 366 is of multiple uses, and may be assigned to one or several surgeons as the user. The dynamic adjustments of valves 123 within the surgical site may be performed either using a training set specific to the user or using aggregated data from many users stored on a server.
In another embodiment, the control unit 366 does not contain an active learning algorithm and instead optimizes flow using a PLC, or one or several PID controllers receiving signals from pressure sensors within the enclosure corresponding to individual air streams, or a combination thereof. In another embodiment, valves 361 are actuated through an iris electromechanical mechanism.
In another embodiment, the variable amount of airflow through valves 123 (via openings 122) can be used to recreate the air velocities of equidistant different diameter fixed holes of the embodiment in
In one embodiment, the environmental control unit 4 is configured to control the valves and outlets of the surgical system in response to the environmental parameters measured by the system of sensors. The system of sensors may include a sampling tube 302 working in conjunction with one or more sensors as shown in
While accurate, measurements do not need to be taken through a sample tube 302 and instead may be collected from sensors either directly located on the surgical enclosure 1, leading to higher measurement accuracy, or located within environmental control unit 4, which results in less direct measurements. Both locations provide for sufficient data to allow for the environmental control unit to employ its control logic to maintain the environment within the surgical enclosure 1. By receiving data from the environmental sensors, the environmental control unit 4 can follow a similar feedback control scheme as shown in
The surgical system may include environmental conditioners including one or more of the following: fans; pumps; filters; heating elements; cooling elements; humidifying elements; dehumidifying elements; elements for removing odors, particulates or microbial populations; elements that introduces odor, particulates, or microbial populations; or any combination above.
The environmental control unit may use one or more types feedback control systems including logic control systems such as those built off of relays and cam timers for ladder logic, microcontrollers, computational processing units, programmable logic controllers, programmable logic devices, complex programmable logic devices, field-programmable gate arrays, programmable integrated chipsets, systems on a chip, application specific integrated circuits, ODROIDs, application-specific standard parts, or any combination thereafter. Methods of control may include proportional control, PID control, cascade control, model predictive control, fuzzy logic. Open-loop control may be used in cases where the user or system decides that a specific control scheme is not desired and the user will instead set the environmental control unit to a user defined setting for the included environmental conditioners.
K. Dynamically Deploying Structural Supports
A portable surgical system may require additional supports to prevent collapse or occlusion of potential airflow features. Materials that maintain their shape such as spring steel, memory shape alloy, or shape memory polymers may be used in the construction of the walls, seams, or otherwise included along the structure of a feature within the surgical enclosure 1. For instance memory alloys such as Nitinol may be included in the walls and seams of the surgical enclosure 1 with the intention of keeping the same shape of the inflated structure when the structure loses internal pressure. However, since the material is a memory alloy, in this embodiment the surgical enclosure can be folded and packed away as normal. Once the surgical system needs to be unpacked, an electrical current can be introduced to the Nitinol to allow for the memory alloy to return to its stored shape and support the inflated contours of the surgical enclosure. In a similar embodiment, these memory alloys would be incorporated into the contours of the airflow channels 2, 301, 121, 122, 104, 102, 502, 503, or any combination thereof. When activated through electrical current, the memory alloy in these locations would return to the idealized inflated state to prevent any occlusion of the material caused by wrinkles or underinflation. This would aid in the prevention of blocked airflow as well as increasing the efficiency of the system, since less pressure would be needed to keep the structure inflated and thereby reducing the energy burden on the overall system. This system can also be included in the mechanical supports explained in Section C and serves as a direct improvement to the supports. A highly compact version of the supports in Section C would be made up of memory alloy that can be activated by heat or electrical current when deployed. The memory alloy will return to the same support like structure while being able to be folded into a much smaller area, allowing for the user to customize how the supports can be packed away.
The portable surgical system may be an ultraportable inflatable surgical environment that can fit in a small container (e.g., a backpack). A portable surgical system can be ultraportable, on-demand and rapidly deployable, reducing a patient's exposure to airborne particulates and a provider's exposure to patient-derived fluids. Additional features and advantages of a portable surgical system may include: allowing a user to seal sterile clear system to patient and operates via different ports; fitting into existing workflows; including integrated environmental control systems; fully self-contained; reducing scrub gear requirements; having excellent visual quality; and including reusable components. To use a portable surgical system, a provider can lay a patient on an operating table, unfold a portable enclosure of the portable surgical system, perform preoperative procedures (e.g., skin disinfecting procedure), and place the portable enclosure on top of the patient so that a drape is attached to a surgical site of the patient.
The following publications are hereby incorporated by reference: [1] Teodorescu DL, Miller SA, Jonnalagedda S. SurgiBox: An ultraportable system to improve surgical safety for patients and providers in austere settings. IEEE Xplore GHTC 2017 (accepted, pending publication); [2] Teodorescu DL, Nagle D, Hickman M, King DR. An ultraportable device platform for aseptic surgery in field settings. ASME J Medical Devices. J. Med. Devices 10(2), 020924 (May 12, 2016); [3] Published international PCT application number PCT/US17/42266 filed on Jul. 14, 2017 and titled “Ultraportable System For Intraoperative Isolation and Regulation of Surgical Site Environment”. [4] Published international PCT application number PCT/US2019/051502 filed on Sep. 17, 2019 and titled “Data analytics and interface platform for portable surgical enclosure”. [5] Published international PCT application number PCT/US2019/032148 filed on May 14, 2019 and titled “Sterile Sleeves for Portable Surgical Systems”.
The present application is a continuation-in-part of U.S. application Ser. No. 16/317,892 filed on Jan. 15, 2019. The present application claims priority from the U.S. Provisional Patent Application No. 62/845,843 filed on May 9, 2019 and titled “System and methods of exhausting airflow and contaminants from within an environment”. The following applications are incorporated hereinafter in their entirety as if full set forth herein: PCT application PCT/US17/42266 filed on Jul. 14, 2017 and titled “Ultraportable System for Intraoperative Isolation and Regulation of Surgical Site Environments”; U.S. Provisional Patent Application No. 62/362,893 filed on Jul. 15, 2016 and titled “Modular Surgical Suite”; PCT application PCT/US19/32148 filed on May 14, 2019 and titled “Sterile Sleeves for Portable Surgical Systems”; and International PCT application PCT/US2019/051502 filed on Sep. 17, 2019 and titled “Data Analytics and Interface Platform for Portable Surgical Enclosure”.
Filing Document | Filing Date | Country | Kind |
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PCT/US2020/032280 | 5/10/2020 | WO | 00 |
Number | Date | Country | |
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62845843 | May 2019 | US |