US20130310705A1 - Methods for evaluating the integrity of a uterine cavity - Google Patents

Abstract

Methods, systems and devices for evaluating the integrity of a uterine cavity. A method comprises introducing transcervically a probe into a patient's uterine cavity, providing a flow of a fluid (e.g., CO2) through the probe into the uterine cavity and monitoring the rate of the flow to characterize the uterine cavity as perforated or non-perforated based on a change in the flow rate. If the flow rate drops to zero or close to zero, this indicates that the uterine cavity is intact and not perforated. If the flow rate does not drop to zero or close to zero, this indicates that a fluid flow is leaking through a perforation in the uterine cavity into the uterine cavity or escaping around an occlusion balloon that occludes the cervical canal.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS
• This application is a continuation of U.S. patent application Ser. No. 13/688,712 (Attorney Docket No. 37646-704.301), filed Nov. 29, 2012, which is a continuation of U.S. patent application Ser. No. 12/616,343 (Attorney Docket No. 37646-704.201), filed Nov. 11, 2009, the entire contents of which are incorporated herein in its entirety.
BACKGROUND
• 1. Field of the Invention
• The present invention relates to electrosurgical methods and devices for global endometrial ablation in a treatment of menorrhagia. More particularly, the present invention relates to applying radiofrequency current to endometrial tissue by means of capacitively coupling the current through an expandable, thin-wall dielectric member enclosing an ionized gas.
• A variety of devices have been developed or proposed for endometrial ablation. Of relevance to the present invention, a variety of radiofrequency ablation devices have been proposed including solid electrodes, balloon electrodes, metalized fabric electrodes, and the like. While often effective, many of the prior electrode designs have suffered from one or more deficiencies, such as relatively slow treatment times, incomplete treatments, non-uniform ablation depths, and risk of injury to adjacent organs.
• For these reasons, it would be desirable to provide systems and methods that allow for endometrial ablation using radiofrequency current which is rapid, provides for controlled ablation depth and which reduce the risk of injury to adjacent organs. At least some of these objectives will be met by the invention described herein.
• 2. Description of the Background Art
• U.S. Pat. Nos. 5,769,880; 6,296,639; 6,663,626; and 6,813,520 describe intrauterine ablation devices formed from a permeable mesh defining electrodes for the application of radiofrequency energy to ablate uterine tissue. U.S. Pat. No. 4,979,948 describes a balloon filled with an electrolyte solution for applying radiofrequency current to a mucosal layer via capacitive coupling. US 2008/097425, having common inventorship with the present application, describes delivering a pressurized flow of a liquid medium which carries a radiofrequency current to tissue, where the liquid is ignited into a plasma as it passes through flow orifices. U.S. Pat. No. 5,891,134 describes a radiofrequency heater within an enclosed balloon. U.S. Pat. No. 6,041,260 describes radiofrequency electrodes distributed over the exterior surface of a balloon which is inflated in a body cavity to be treated. U.S. Pat. No. 7,371,231 and US 2009/054892 describe a conductive balloon having an exterior surface which acts as an electrode for performing endometrial ablation. U.S. Pat. No. 5,191,883 describes bipolar heating of a medium within a balloon for thermal ablation. U.S. Pat. No. 6,736,811 and U.S. Pat. No. 5,925,038 show an inflatable conductive electrode.
BRIEF SUMMARY
• The present invention provides methods, systems and devices for evaluating the integrity of a uterine cavity. The uterine cavity may be perforated or otherwise damaged by the transcervical introduction of probes and instruments into the uterine cavity. If the uterine wall is perforated, it would be preferable to defer any ablation treatment until the uterine wall is healed. A method of the invention comprises introducing transcervically a probe into a patient's uterine cavity, providing a flow of a fluid (e.g., CO2 through the probe into the uterine cavity and monitoring the rate of the flow to characterize the uterine cavity as perforated or non-perforated based on a change in the flow rate. If the flow rate drops to zero or close to zero, this indicates that the uterine cavity is intact and not perforated. If the flow rate does not drop to zero or close to zero, this indicates that a fluid flow is leaking through a perforation in the uterine cavity into the uterine cavity or escaping around an occlusion balloon that occludes the cervical canal.
• Embodiments herein provide a method of characterizing a patient's uterus, comprising introducing a flow of a fluid into a uterine cavity of a patient; and monitoring the flow to characterize the uterine cavity as at least one of perforated or non-perforated based on a change in a rate of the flow. Introducing may be, for example, transcervically introducing a probe into the uterine cavity, and introducing the flow through the probe.
• Monitoring may include providing a signal, responsive to the rate of flow, that characterizes the uterine cavity as at least one of perforated or non-perforated. As an example, monitoring may include generating a signal responsive to the rate of flow not dropping below a predetermined level, the signal characterizing the uterine cavity as perforated. In embodiments, the predetermined level is 0.05 slpm.
• In embodiments, monitoring comprises generating a signal responsive to the rate of flow dropping below a predetermined level, the signal characterizing the uterine cavity as non-perforated. The predetermined level may be, for example, 0.05 slpm.
• In further embodiments, monitoring comprises monitoring a rate of flow after a predetermined first interval after initiation of the flow. The first interval may be, as examples, at least 5 seconds, at least 15 seconds, or at least 30 seconds.
• Monitoring may additionally include monitoring a rate of flow over a second predetermined interval after the first interval. The second interval may be a least 1 second, at least 5 seconds, or at least 10 seconds, as examples.
• In additional embodiments, monitoring includes providing a signal, responsive to the rate of flow, that characterizes the uterine cavity as at least one of perforated or non-perforated, and wherein the signal is at least one of visual, aural and tactile.
• In embodiments, prior to introducing the flow, a member is positioned within the cervical canal that substantially prevents a flow of the fluid out of the uterine cavity. Introducing may include transcervically introducing a probe into the uterine cavity, and introducing the flow through the probe, with the member positioned about an exterior of the probe. The member may be expanded in the cervical canal.
• In embodiments, the fluid is a gas or a liquid.
• In additional embodiments, introducing includes transcervically introducing a probe into the uterine cavity, and introducing the flow through the probe. The probe has a working end with an energy-delivery surface for ablating uterine cavity tissue. Responsive to the uterine cavity being characterized as perforated, energy delivery surface is disabled. Alternatively or additionally, responsive to the uterine cavity being characterized as non perforated, activation of the energy delivery surface may be enabled or even caused to happen automatically.
• In embodiments, a method of endometrial ablation is provided, the method including introducing an ablation probe into a uterine cavity of a patient; flowing a fluid from a fluid source through the probe into the uterine cavity; monitoring the rate of the flow of the fluid into the uterine cavity to characterize the cavity as at least one of perforated or non-perforated based on a change in the flow rate; and responsive the to the uterine cavity being characterized as non perforated, activating the ablation probe to ablate an interior of the uterine cavity.
BRIEF DESCRIPTION OF THE DRAWINGS
• In order to better understand the invention and to see how it may be carried out in practice, some preferred embodiments are next described, by way of non-limiting examples only, with reference to the accompanying drawings, in which like reference characters denote corresponding features consistently throughout similar embodiments in the attached drawings.
• FIG. 1 is a perspective view of an ablation system corresponding to the invention, including a hand-held electrosurgical device for endometrial ablation, RF power source, gas source and controller.
• FIG. 2 is a view of the hand-held electrosurgical device ofFIG. 1 with a deployed, expanded thin-wall dielectric structure.
• FIG. 3 is a block diagram of components of one electrosurgical system corresponding to the invention.
• FIG. 4 is a block diagram of the gas flow components of the electrosurgical system ofFIG. 1.
• FIG. 5 is an enlarged perspective view of the expanded thin-wall dielectric structure, showing an expandable-collapsible frame with the thin dielectric wall in phantom view.
• FIG. 6 is a partial sectional view of the expanded thin-wall dielectric structure ofFIG. 5 showing (i) translatable members of the expandable-collapsible frame a that move the structure between collapsed and (ii) gas inflow and outflow lumens.
• FIG. 7 is a sectional view of an introducer sleeve showing various lumens of the introducer sleeve taken along line7-7 ofFIG. 6.
• FIG. 8A is an enlarged schematic view of an aspect of a method of the invention illustrating the step introducing an introducer sleeve into a patient's uterus.
• FIG. 8B is a schematic view of a subsequent step of retracting the introducer sleeve to expose a collapsed thin-wall dielectric structure and internal frame in the uterine cavity.
• FIG. 8C is a schematic view of subsequent steps of the method, including, (i) actuating the internal frame to move the a collapsed thin-wall dielectric structure to an expanded configuration, (ii) inflating a cervical-sealing balloon carried on the introducer sleeve, and (iii) actuating gas flows and applying RF energy to contemporaneously ionize the gas in the interior chamber and cause capacitive coupling of current through the thin-wall dielectric structure to cause ohmic heating in the engaged tissue indicated by current flow paths.
• FIG. 8D is a schematic view of a subsequent steps of the method, including: (i) advancing the introducer sleeve over the thin-wall dielectric structure to collapse it into an interior bore shown in phantom view, and (ii) withdrawing the introducer sleeve and dielectric structure from the uterine cavity.
• FIG. 9 is a cut-away perspective view of an alternative expanded thin-wall dielectric structure similar to that ofFIGS. 5 and 6 show an alternative electrode configuration.
• FIG. 10 is an enlarged cut-away view of a portion of the expanded thin-wall dielectric structure ofFIG. 9 showing the electrode configuration.
• FIG. 11 is a schematic view of a patient uterus depicting a method corresponding to the invention including providing a flow of a fluid media into the uterine cavity and monitoring the flow rate to characterize the patient's uterine cavity as intact and non-perforated.
• FIG. 12 is a perspective view of the ablation device ofFIGS. 1-2 with a subsystem for checking the integrity of a uterine cavity.
• FIG. 13 represents a block diagram of a subsystem of the invention for providing and monitoring a fluid flow into the patient's uterine cavity.
• FIG. 14 represents a diagram indicating the steps of an algorithm for providing and monitoring a fluid flow into the patient's uterine cavity.
DETAILED DESCRIPTION
• In general, an electrosurgical ablation system is described herein that comprises an elongated introducer member for accessing a patient's uterine cavity with a working end that deploys an expandable thin-wall dielectric structure containing an electrically non-conductive gas as a dielectric. In one embodiment, an interior chamber of the thin-wall dielectric structure contains a circulating neutral gas such as argon. An RF power source provides current that is coupled to the neutral gas flow by a first polarity electrode disposed within the interior chamber and a second polarity electrode at an exterior of the working end. The gas flow, which is converted to a conductive plasma by an electrode arrangement, functions as a switching mechanism that permits current flow to engaged endometrial tissue only when the voltage across the combination of the gas, the thin-wall dielectric structure and the engaged tissue reaches a threshold that causes capacitive coupling across the thin-wall dielectric material. By capacitively coupling current to tissue in this manner, the system provides a substantially uniform tissue effect within all tissue in contact with the expanded dielectric structure. Further, the invention allows the neutral gas to be created contemporaneously with the capacitive coupling of current to tissue.
• In general, this disclosure may use the terms “plasma”, “conductive gas” and “ionized gas” interchangeably. A plasma consists of a state of matter in which electrons in a neutral gas are stripped or “ionized” from their molecules or atoms. Such plasmas can be formed by application of an electric field or by high temperatures. In a neutral gas, electrical conductivity is non-existent or very low. Neutral gases act as a dielectric or insulator until the electric field reaches a breakdown value, freeing the electrons from the atoms in an avalanche process thus forming a plasma. Such a plasma provides mobile electrons and positive ions, and acts as a conductor which supports electric currents and can form spark or arc. Due to their lower mass, the electrons in a plasma accelerate more quickly in response to an electric field than the heavier positive ions, and hence carry the bulk of the current.
• FIG. 1 depicts one embodiment of anelectrosurgical ablation system100 configured for endometrial ablation. Thesystem100 includes a hand-heldapparatus105 with aproximal handle106 shaped for grasping with a human hand that is coupled to anelongated introducer sleeve110 havingaxis111 that extends to adistal end112. Theintroducer sleeve110 can be fabricated of a thin-wall plastic, composite, ceramic or metal in a round or oval cross-section having a diameter or major axis ranging from about 4 mm to 8 mm in at least a distal portion of the sleeve that accesses the uterine cavity. Thehandle106 is fabricated of an electrically insulative material such as a molded plastic with a pistol-grip having first and second portions,114aand114b, that can be squeezed toward one another to translate an elongatedtranslatable sleeve115 which is housed in abore120 in theelongated introducer sleeve110. By actuating the first and second handle portions,114aand114b, a workingend122 can be deployed from a first retracted position (FIG. 1) in the distal portion ofbore120 inintroducer sleeve110 to an extended position as shown inFIG. 2. InFIG. 2, it can be seen that the first and second handle portions,114aand114b, are in a second actuated position with the workingend122 deployed from thebore120 inintroducer sleeve110.
• FIGS. 2 and 3 shows thatablation system100 includes anRF energy source130A andRF controller130B in acontrol unit135. TheRF energy source130A is connected to the hand-helddevice105 by aflexible conduit136 with a plug-inconnector137 configured with a gas inflow channel, a gas outflow channel, and first and second electrical leads for connecting to receivingconnector138 in thecontrol unit135. Thecontrol unit135, as will be described further below inFIGS. 3 and 4, further comprises a neutralgas inflow source140A,gas flow controller140B and optional vacuum ornegative pressure source145 to provide controlled gas inflows and gas outflows to and from the workingend122. Thecontrol unit135 further includes aballoon inflation source148 for inflating anexpandable sealing balloon225 carried onintroducer sleeve110 as described further below.
• Referring toFIG. 2, the workingend122 includes a flexible, thin-wall member orstructure150 of a dielectric material that when expanded has a triangular shape configured for contacting the patient's endometrial lining that is targeted for ablation. In one embodiment as shown inFIGS. 2,5 and6, thedielectric structure150 comprises a thin-wall material such as silicone with a fluid-tightinterior chamber152.
• In an embodiment, an expandable-collapsible frame assembly155 is disposed in the interior chamber. Alternatively, the dielectric structure may be expanded by a neutral gas without a frame, but using a frame offers a number of advantages. First, the uterine cavity is flattened with the opposing walls in contact with one another. Expanding a balloon-type member may cause undesirable pain or spasms. For this reason, a flat structure that is expanded by a frame is better suited for deployment in the uterine cavity. Second, in embodiments herein, the neutral gas is converted to a conductive plasma at a very low pressure controlled by gas inflows and gas outflows—so that any pressurization of a balloon-type member with the neutral gas may exceed a desired pressure range and would require complex controls of gas inflows and gas outflows. Third, as described below, the frame provides an electrode for contact with the neutral gas in theinterior chamber152 of thedielectric structure150, and theframe155 extends into all regions of the interior chamber to insure electrode exposure to all regions of the neutral gas and plasma. Theframe155 can be constructed of any flexible material with at least portions of the frame functioning as spring elements to move the thin-wall structure150 from a collapsed configuration (FIG. 1) to an expanded, deployed configuration (FIG. 2) in a patient's uterine cavity. In one embodiment, theframe155 comprisesstainless steel elements158a,158band160aand160bthat function akin to leaf springs. The frame can be a stainless steel such as 316 SS, 17A SS, 420 SS, 440 SS or the frame can be a NiTi material. The frame preferably extends along a single plane, yet remains thin transverse to the plane, so that the frame may expand into the uterine cavity. The frame elements can have a thickness ranging from about 0.005″ to 0.025″. As can be seen inFIGS. 5 and 6, the proximal ends162aand162bofspring elements158a,158bare fixed (e.g., by welds164) to thedistal end165 ofsleeve member115. The proximal ends166aand166bofspring elements160a,160bare welded todistal portion168 of a secondarytranslatable sleeve170 that can be extended frombore175 intranslatable sleeve115. The secondarytranslatable sleeve170 is dimensioned for a loose fit inbore175 to allow gas flows withinbore175.FIGS. 5 and 6 further illustrate the distal ends176aand176bofspring elements158a,158bare welded todistal ends178aand178bofspring elements160aand160bto thus provide aframe155 that can be moved from a linear shape (seeFIG. 1) to an expanded triangular shape (FIGS. 5 and 6).
• As will be described further below, thebore175 insleeve115 and bore180 in secondarytranslatable sleeve170 function as gas outflow and gas inflow lumens, respectively. It should be appreciated that the gas inflow lumen can comprise any single lumen or plurality of lumens in eithersleeve115 orsleeve170 or another sleeve, or other parts of theframe155 or the at least one gas flow lumen can be formed into a wall ofdielectric structure150. InFIGS. 5,6 and7 it can be seen that gas inflows are provided throughbore180 insleeve170, and gas outflows are provided inbore175 ofsleeve115. However, the inflows and outflows can be also be reversed betweenbores175 and180 of the various sleeves.FIGS. 5 and 6 further show that arounded bumper element185 is provided at the distal end ofsleeve170 to insure that no sharp edges of the distal end ofsleeve170 can contact the inside of the thindielectric wall150. In one embodiment, thebumper element185 is silicone, but it could also comprise a rounded metal element.FIGS. 5 and 6 also show that a plurality ofgas inflow ports188 can be provided along a length of insleeve170 inchamber152, as well as aport190 in the distal end ofsleeve170 andbumper element185. The sectional view ofFIG. 7 also shows the gas flow passageways within the interior ofintroducer sleeve110.
• It can be understood fromFIGS. 1,2,5 and6 that actuation of first and second handle portions,114aand114b, (i) initially causes movement of the assembly ofsleeves115 and170 relative to bore120 ofintroducer sleeve110, and (ii) secondarily causes extension ofsleeve170 frombore175 insleeve115 to expand theframe155 into the triangular shape ofFIG. 5. The dimensions of the triangular shape are suited for a patient uterine cavity, and for example can have an axial length A ranging from 4 to 10 cm and a maximum width B at the distal end ranging from about 2 to 5 cm. In one embodiment, the thickness C of the thin-wall structure150 can be from 1 to 4 mm as determined by the dimensions ofspring elements158a,158b,160aand160bofframe assembly155. It should be appreciated that theframe assembly155 can comprise round wire elements, flat spring elements, of any suitable metal or polymer that can provide opening forces to move thin-wall structure150 from a collapsed configuration to an expanded configuration within the patient uterus. Alternatively, some elements of theframe155 can be spring elements and some elements can be flexible without inherent spring characteristics.
• As will be described below, the working end embodiment ofFIGS. 2,5 and6 has a thin-wall structure150 that is formed of a dielectric material such as silicone that permits capacitive coupling of current to engaged tissue while theframe assembly155 provides structural support to position the thin-wall structure150 against tissue. Further, gas inflows into theinterior chamber152 of the thin-wall structure can assist in supporting the dielectric wall so as to contact endometrial tissue. The dielectric thin-wall structure150 can be free from fixation to theframe assembly155, or can be bonded to an outward-facing portion or portions offrame elements158aand158b. Theproximal end182 of thin-wall structure150 is bonded to the exterior of the distal end ofsleeve115 to thus provide a sealed, fluid-tight interior chamber152 (FIG. 5).
• In one embodiment, thegas inflow source140A comprises one or more compressed gas cartridges that communicate withflexible conduit136 through plug-inconnector137 and receivingconnector138 in the control unit135 (FIGS. 1-2). As can be seen inFIGS. 5-6, the gas inflows fromsource140A flow throughbore180 insleeve170 to openterminations188 and190 therein to flow intointerior chamber152. Avacuum source145 is connected throughconduit136 andconnector137 to allow circulation of gas flow through theinterior chamber152 of the thin-wall dielectric structure150. InFIGS. 5 and 6, it can be seen that gas outflows communicate withvacuum source145 throughopen end200 ofbore175 insleeve115. Referring toFIG. 5, it can be seen thatframe elements158aand158bare configured with a plurality ofapertures202 to allow for gas flows through all interior portions of the frame elements, and thus gas inflows fromopen terminations188,190 inbore180 are free to circulated throughinterior chamber152 to return to an outflow path throughopen end200 ofbore175 ofsleeve115. As will be described below (seeFIGS. 3-4), thegas inflow source140A is connected to a gas flow orcirculation controller140B which controls apressure regulator205 and also controlsvacuum source145 which is adapted for assisting in circulation of the gas. It should be appreciated that the frame elements can be configured with apertures, notched edges or any other configurations that allow for effective circulation of a gas throughinterior chamber152 of the thin-wall structure150 between the inflow and outflow passageways.
• Now turning to the electrosurgical aspects of the invention,FIGS. 5 and 6 illustrate opposing polarity electrodes of thesystem100 that are configured to convert a flow of neutral gas inchamber152 into a plasma208 (FIG. 6) and to allow capacitive coupling of current through awall210 of the thin-wall dielectric structure150 to endometrial tissue in contact with thewall210. The electrosurgical methods of capacitively coupling RF current across aplasma208 anddielectric wall210 are described in U.S. patent application Ser. No. 12/541,043; filed Aug. 13, 2009 (Atty. Docket No. 027980-000110US) and U.S. application Ser. No. 12/541,050 (Atty. Docket No. 027980-000120US), referenced above. InFIGS. 5 and 6, thefirst polarity electrode215 is withininterior chamber152 to contact the neutral gas flow and comprises theframe assembly155 that is fabricated of an electrically conductive stainless steel. In another embodiment, the first polarity electrode can be any element disposed within theinterior chamber152, or extendable intointerior chamber152. Thefirst polarity electrode215 is electrically coupled tosleeves115 and170 which extends through theintroducer sleeve110 to handle106 andconduit136 and is connected to a first pole of the RFsource energy source130A andcontroller130B. Asecond polarity electrode220 is external of theinternal chamber152 and in one embodiment the electrode is spaced apart fromwall210 of the thin-wall dielectric structure150. In one embodiment as depicted inFIGS. 5 and 6, thesecond polarity electrode220 comprises a surface element of anexpandable balloon member225 carried byintroducer sleeve110. Thesecond polarity electrode220 is coupled by a lead (not shown) that extends through theintroducer sleeve110 andconduit136 to a second pole of theRF source130A. It should be appreciated thatsecond polarity electrode220 can be positioned onsleeve110 or can be attached to surface portions of the expandable thin-wall dielectric structure150, as will be described below, to provide suitable contact with body tissue to allow the electrosurgical ablation of the method of the invention. Thesecond polarity electrode220 can comprise a thin conductive metallic film, thin metal wires, a conductive flexible polymer or a polymeric positive temperature coefficient material. In one embodiment depicted inFIGS. 5 and 6, theexpandable member225 comprises a thin-wall compliant balloon having a length of about 1 cm to 6 cm that can be expanded to seal the cervical canal. Theballoon225 can be inflated with a gas or liquid by anyinflation source148, and can comprise a syringe mechanism controlled manually or bycontrol unit135. Theballoon inflation source148 is in fluid communication with aninflation lumen228 inintroducer sleeve110 that extends to an inflation chamber of balloon225 (seeFIG. 7).
• Referring back toFIG. 1, thecontrol unit135 can include adisplay230 and touch screen orother controls232 for setting and controlling operational parameters such as treatment time intervals, treatment algorithms, gas flows, power levels and the like. Suitable gases for use in the system include argon, other noble gases and mixtures thereof. In one embodiment, afootswitch235 is coupled to thecontrol unit135 for actuating the system.
• The box diagrams ofFIGS. 3 and 4 schematically depict thesystem100, subsystems and components that are configured for an endometrial ablation system. In the box diagram ofFIG. 3, it can be seen thatRF energy source130A and circuitry is controlled by acontroller130B. The system can include feedback control systems that include signals relating to operating parameters of the plasma ininterior chamber152 of thedielectric structure150. For example, feedback signals can be provided from at least onetemperature sensor240 in theinterior chamber152 of thedielectric structure150, from a pressure sensor within, or in communication, withinterior chamber152, and/or from a gas flow rate sensor in an inflow or outflow channel of the system.FIG. 4 is a schematic block diagram of the flow control components relating to the flow of gas media through thesystem100 and hand-helddevice105. It can be seen that apressurized gas source140A is linked to adownstream pressure regulator205, an inflowproportional valve246,flow meter248 and normally closedsolenoid valve250. Thevalve250 is actuated by the system operator which then allows a flow of a neutral gas fromgas source140A to circulate throughflexible conduit136 and thedevice105. The gas outflow side of the system includes a normallyopen solenoid valve260, outflowproportional valve262 and flowmeter264 that communicate with vacuum pump orsource145. The gas can be exhausted into the environment or into a containment system. A temperature sensor270 (e.g., thermocouple) is shown inFIG. 4 that is configured for monitoring the temperature of outflow gases.FIG. 4 further depicts anoptional subsystem275 which comprises avacuum source280 andsolenoid valve285 coupled to thecontroller140B for suctioning steam from auterine cavity302 at an exterior of thedielectric structure150 during a treatment interval. As can be understood fromFIG. 4, the flow passageway from theuterine cavity302 can be throughbore120 in sleeve110 (seeFIGS. 2,6 and7) or another lumen in a wall ofsleeve110 can be provided.
• FIGS. 8A-8D schematically illustrate a method of the invention wherein (i) the thin-wall dielectric structure150 is deployed within a patient uterus and (ii) RF current is applied to a contained neutral gas volume in theinterior chamber152 to contemporaneously create aplasma208 in the chamber and capacitively couple current through the thindielectric wall210 to apply ablative energy to the endometrial lining to accomplish global endometrial ablation.
• More in particular,FIG. 8A illustrates apatient uterus300 withuterine cavity302 surrounded byendometrium306 andmyometrium310. The externalcervical os312 is the opening of the cervix314 into thevagina316. The internal os or opening320 is a region of the cervical canal that opens to theuterine cavity302.FIG. 8A depicts a first step of a method of the invention wherein the physician has introduced a distal portion ofsleeve110 into theuterine cavity302. The physician gently can advance thesleeve110 until its distal tip contacts thefundus324 of the uterus. Prior to insertion of the device, the physician can optionally introduce a sounding instrument into the uterine cavity to determine uterine dimensions, for example from theinternal os320 tofundus324.
• FIG. 8B illustrates a subsequent step of a method of the invention wherein the physician begins to actuate the first and second handle portions,114aand114b, and theintroducer sleeve110 retracts in the proximal direction to expose thecollapsed frame155 and thin-wall structure150 within theuterine cavity302. Thesleeve110 can be retracted to expose a selected axial length of thin-wall dielectric structure150, which can be determined bymarkings330 on sleeve115 (seeFIG. 1) which indicate the axial travel ofsleeve115 relative tosleeve170 and thus directly related to the length of deployed thin-wall structure150.FIG. 2 depicts thehandle portions114aand114bfully approximated thus deploying the thin-wall structure to its maximum length.
• FIG. 8C illustrates several subsequent steps of a method of the invention.FIG. 8C first depicts the physician continuing to actuate the first and second handle portions,114aand114b, which further actuates the frame155 (seeFIGS. 5-6) to expand theframe155 and thin-wall structure150 to a deployed triangular shape to contact the patient'sendometrial lining306. The physician can slightly rotate and move the expandingdielectric structure150 back and forth as the structure is opened to insure it is opened to the desired extent. In performing this step, the physician can actuate handle portions,114aand114b, a selected degree which causes a select length of travel ofsleeve170 relative tosleeve115 which in turn opens theframe155 to a selected degree. The selected actuation ofsleeve170 relative tosleeve115 also controls the length of dielectric structure deployed fromsleeve110 into the uterine cavity. Thus, the thin-wall structure150 can be deployed in the uterine cavity with a selected length, and the spring force of the elements offrame155 will open thestructure150 to a selected triangular shape to contact or engage theendometrium306. In one embodiment, the expandable thin-wall structure150 is urged toward and maintained in an open position by the spring force of elements of theframe155. In the embodiment depicted inFIGS. 1 and 2, thehandle106 includes a locking mechanism with finger-actuatedsliders332 on either side of the handle that engage a grip-lock element against a notch inhousing333 coupled to introducer sleeve110 (FIG. 2) to locksleeves115 and170 relative tointroducer sleeve110 to maintain the thin-wall dielectric structure150 in the selected open position.
• FIG. 8C further illustrates the physician expanding theexpandable balloon structure225 frominflation source148 to thus provide an elongated sealing member to seal thecervix314 outward from theinternal os320. Following deployment of the thin-wall structure150 andballoon225 in thecervix314, thesystem100 is ready for the application of RF energy to ablateendometrial tissue306.FIG. 8C next depicts the actuation of thesystem100, for example, by actuatingfootswitch235, which commences a flow of neutral gas fromsource140A into theinterior chamber152 of the thin-wall dielectric structure150. Contemporaneous with, or after a selected delay, the system's actuation delivers RF energy to the electrode arrangement which includes first polarity electrode215 (+) offrame155 and the second polarity electrode220 (−) which is carried on the surface ofexpandable balloon member225. The delivery of RF energy delivery will instantly convert the neutral gas ininterior chamber152 intoconductive plasma208 which in turn results in capacitive coupling of current through thedielectric wall210 of the thin-wall structure150 resulting in ohmic heating of the engaged tissue.FIG. 8C schematically illustrates the multiplicity of RFcurrent paths350 between theplasma208 and thesecond polarity electrode220 through thedielectric wall210. By this method, it has been found that ablation depths of three mm to six mm or more can be accomplished very rapidly, for example in 60 seconds to 120 seconds dependent upon the selected voltage and other operating parameters. In operation, the voltage at which the neutral gas inflow, such as argon, becomes conductive (i.e., converted in part into a plasma) is dependent upon a number of factors controlled by thecontrollers130B and140B, including the pressure of the neutral gas, the volume ofinterior chamber152, the flow rate of the gas through thechamber152, the distance betweenelectrode210 and interior surfaces of thedielectric wall210, the dielectric constant of thedielectric wall210 and the selected voltage applied by the RF source130, all of which can be optimized by experimentation. In one embodiment, the gas flow rate can be in the range of 5 ml/sec to 50 ml/sec. Thedielectric wall210 can comprise a silicone material having a thickness ranging from a 0.005″ to 0.015 and having a relative permittivity in the range of 3 to 4. The gas can be argon supplied in a pressurized cartridge which is commercially available. Pressure in theinterior chamber152 ofdielectric structure150 can be maintained between 14 psia and 15 psia with zero or negative differential pressure betweengas inflow source140A and negative pressure orvacuum source145. The controller is configured to maintain the pressure in interior chamber in a range that varies by less than 10% or less than 5% from a target pressure. TheRF power source130A can have a frequency of 450 to 550 KHz, and electrical power can be provided within the range of 600 Vrms to about 1200 Vrms and about 0.2 Amps to 0.4 Amps and an effective power of 40 W to 100 W. In one method, thecontrol unit135 can be programmed to delivery RF energy for a preselected time interval, for example, between 60 seconds and 120 seconds. One aspect of a treatment method corresponding to the invention consists of ablating endometrial tissue with RF energy to elevate endometrial tissue to a temperature greater than 45 degrees Celsius for a time interval sufficient to ablate tissue to a depth of at least 1 mm. Another aspect of the method of endometrial ablation of consists of applying radiofrequency energy to elevate endometrial tissue to a temperature greater than 45 degrees Celsius without damaging the myometrium.
• FIG. 8D illustrates a final step of the method wherein the physician deflates theexpandable balloon member225 and then extendssleeve110 distally by actuating thehandles114aand114bto collapseframe155 and then retracting the assembly from theuterine cavity302. Alternatively, the deployed workingend122 as shown inFIG. 8C can be withdrawn in the proximal direction from the uterine cavity wherein theframe155 and thin-wall structure150 will collapse as it is pulled through the cervix.FIG. 8D shows the completed ablation with the ablated endometrial tissue indicated at360.
• In another embodiment, the system can include an electrode arrangement in thehandle106 or within the gas inflow channel to pre-ionize the neutral gas flow before it reaches theinterior chamber152. For example, the gas inflow channel can be configured with axially or radially spaced apart opposing polarity electrodes configured to ionize the gas inflow. Such electrodes would be connected in separate circuitry to an RF source. The first and second electrodes215 (+) and220 (−) described above would operate as described above to provide the current that is capacitively coupled to tissue through the walls of thedielectric structure150. In all other respects, the system and method would function as described above.
• Now turning toFIGS. 9 and 10, analternate working end122 with thin-wall dielectric structure150 is shown. In this embodiment, the thin-wall dielectric structure150 is similar to that ofFIGS. 5 and 6 except that thesecond polarity electrode220′ that is exterior of theinternal chamber152 is disposed on asurface portion370 of the thin-wall dielectric structure150. In this embodiment, thesecond polarity electrode220′ comprises a thin-film conductive material, such as gold, that is bonded to the exterior of thin-wall material210 along twolateral sides354 ofdielectric structure150. It should be appreciated that the second polarity electrode can comprise one or more conductive elements disposed on the exterior ofwall material210, and can extend axially, or transversely toaxis111 and can be singular or multiple elements. In one embodiment shown in more detail inFIG. 10, thesecond polarity electrode220′ can be fixed on anotherlubricious layer360, such as a polyimide film, for example KAPTON®. The polyimide tape extends about thelateral sides354 of thedielectric structure150 and provides protection to thewall210 when it is advanced from or withdrawn intobore120 insleeve110. In operation, the RF delivery method using the embodiment ofFIGS. 9 and 10 is the same as described above, with RF current being capacitively coupled from theplasma208 through thewall210 and endometrial tissue to thesecond polarity electrode220′ to cause the ablation.
• FIG. 9 further shows anoptional temperature sensor390, such as a thermocouple, carried at an exterior of thedielectric structure150. In one method of use, thecontrol unit135 can acquire temperature feedback signals from at least onetemperature sensor390 to modulate or terminate RF energy delivery, or to modulate gas flows within the system. In a related method of the invention, thecontrol unit135 can acquire temperature feedback signals fromtemperature sensor240 in interior chamber152 (FIG. 6 to modulate or terminate RF energy delivery or to modulate gas flows within the system.
• In another embodiment of the invention,FIGS. 11-14 depict systems and methods for evaluating the integrity of the uterine cavity which may be perforated or otherwise damaged by the transcervical introduction of probes and instruments into a uterine cavity. If the uterine wall is perforated, it would be preferable to defer any ablation treatment until the uterine wall is healed. A method of the invention comprises introducing transcervically a probe into a patient's uterine cavity, providing a flow of a fluid (e.g., CO2) through the probe into the uterine cavity and monitoring the rate of the flow to characterize the uterine cavity as perforated or non-perforated based on a change in the flow rate. If the flow rate drops to zero or close to zero, this indicates that the uterine cavity is intact and not perforated. If the flow rate does not drop to zero or close to zero, this indicates that a fluid flow is leaking through a perforation in theuterine cavity302 into the uterine cavity or escaping around an occlusion balloon that occludes the cervical canal.
• InFIG. 11, it can be seen how a pressurizedfluid source405 andcontroller410 for controlling and monitoring flows is in fluid communication withlumen120 of introducer sleeve110 (seeFIG. 7). In one embodiment, the fluid source can be a pressurized cartridge containing CO2 or another biocompatible gas. InFIG. 12, it can be seen thatfluid source405 communicates with aflexible conduit412 that is connected to a “pig-tail”tubing connector414 extending outward fromhandle106 of the hand-held probe. A tubing in the interior ofhandle component114aprovides aflow passageway415 to thelumen120 in the introducer sleeve. In another embodiment, thefluid source405 and flexible conduit408 can be integrated intoconduit136 ofFIG. 1.
• InFIG. 11, it can be seen that the flow of fluid is introduced into theuterine cavity302 after theballoon225 in the cervical canal has been inflated and after the working end anddielectric structure150 has been expanded into its triangular shape to occupy the uterine cavity. Thus, the CO2 gas flows around the exterior surfaces of expandeddielectric structure150 to fill the uterine cavity. Alternatively, the flow of CO2 can be provided after theballoon225 in the cervical canal is inflated but before thedielectric structure150 is expanded.
• FIG. 13 is a block diagram that schematically depicts the components ofsubsystem420 that provides the flow of CO2 to and through the hand-heldprobe105. It can be seen that pressurizedfluid source405 communicates with adownstream pressure regulator422, aproportional valve424,flow meter440, normally closedsolenoid valve450 and one-way valve452. Thevalve450 upon actuation by the system operator allows a flow of CO2 gas fromsource405 at a predetermined flow rate and pressure through the subsystem and into theuterine cavity302.
• In one embodiment of the method of operation, the physician actuates the system and electronically opensvalve450 which can provide a CO2 flow through the system. Thecontroller410 monitors the flow meter orsensor440 over an interval that can range from 1 second to 60 seconds, or 5 second to 30 seconds to determine the change in the rate of flow and/or a change in the rate of flow. In an embodiment, the flow sensor comprises a Honeywell AWM5000 Series Mass Airflow Sensor, for example Model AWM5101, that measure flows in units of mass flow. In one embodiment, the initial flow rate is between 0.05 slpm (standard liters per minute) and 2.0 slpm, or between 0.1 slpm and 0.2 slpm. Thecontroller410 includes a microprocessor or programmable logic device that provides a feedback signal from the flow sensors indicating either (i) that the flow rate has dropped to zero or close to zero to thus characterize the uterine cavity as non-perforated, or (ii) that the flow rate has not dropped to a predetermined threshold level within a predetermined time interval to thus characterize the uterine cavity as perforated or that there is a failure inocclusion balloon225 or its deployment so that the cervical canal is not occluded. In one embodiment, the threshold level is 0.05 slpm for characterizing the uterine cavity as non-perforated. In this embodiment, the controller provides a signal indicating a non-perforated uterine cavity if the flow drops below 0.05 slpm between the fifth second of the flow and the flow time-out, which can be, for example, 30 seconds.
• FIG. 14 depicts aspects of an algorithm used bycontroller410 to accomplish a uterine cavity integrity check, with the first step comprising actuating a footswitch or hand switch. Upon actuation, a timer is initialized for 1 to 5 seconds to determine that afluid source405 is capable of providing a fluid flow, which can be checked by a pressure sensor between thesource405 andpressure regulator422. If no flow is detected, an error signal is provided, such as a visual display signal on the control unit135 (FIG. 1).
• As can be understood fromFIG. 14, after thefluid source405 is checked, the controller opens thesupply solenoid valve450 and a timer is initialized for a 1 to 5 second test interval to insure fluid flows through thesubsystem420 ofFIG. 13, with either or both aflow meter440 or a pressure sensor. At the same time asvalve450 is opened, a timer is initialized for cavity integrity test interval of 30 seconds. Thecontroller410 monitors theflow meter440 and provides a signal characterizing the uterine cavity as non-perforated if, at any time after the initial 5 second check interval and before the end of the timed-out period (e.g., the 30 second time-out), the flow rate drops below a threshold minimum rate, in one embodiment, to below 0.05 slpm. If the interval times out after 30 seconds and the flow rate does not drop below this threshold, then a signal is generated that characterizes that the uterine cavity is perforated. This signal also can indicate a failure of theocclusion balloon225.
• Referring toFIG. 14, in one embodiment, in response or otherwise as a result of the signal that the uterine cavity is not perforated, thecontroller410 can automatically enable and activate the RF ablation system described above to perform an ablation procedure. Thecontroller410 can provide a time interval from 1 to 15 seconds to allow CO2 gas to vent from theuterine cavity302 before activating RF energy delivery. In another embodiment, the endometrial ablation system may include theoptional subsystem275 for exhausting fluids or gas from the uterine cavity during an ablation treatment (seeFIG. 4 and accompanying text). Thissubsystem275 can be actuated to exhaust CO2 from theuterine cavity302 which include openingsolenoid valve285 shown inFIG. 4.
• The system can further include an override to repeat the cavity integrity check, for example, after evaluation and re-deployment of theocclusion balloon225.
• Although particular embodiments of the present invention have been described above in detail, it will be understood that this description is merely for purposes of illustration and the above description of the invention is not exhaustive. Specific features of the invention are shown in some drawings and not in others, and this is for convenience only and any feature may be combined with another in accordance with the invention. A number of variations and alternatives will be apparent to one having ordinary skills in the art. Such alternatives and variations are intended to be included within the scope of the claims. Particular features that are presented in dependent claims can be combined and fall within the scope of the invention. The invention also encompasses embodiments as if dependent claims were alternatively written in a multiple dependent claim format with reference to other independent claims.

Claims (20)

What is claimed is:

1. A method for evaluating a patient's uterus, comprising:

introducing a probe through a cervical canal into a uterine cavity of the patient;

expanding first and second expandable structures carried by the probe;

introducing a flow of a fluid into the uterine cavity through the probe, wherein the fluid comprises a gas; and

measuring a flow rate of the fluid being introduced, wherein a measured flow rate which drops to a level below a predetermined minimum level indicates that the uterus is non-perforated.

2. The method ofclaim 1, wherein the first expandable structure has a fluid-tight wall.

3. The method ofclaim 1, wherein the second expandable structure has a fluid-tight wall.

4. The method ofclaim 1, wherein the expanding step expands the first and second expandable structures independently.

5. The method ofclaim 1, further comprising generating a signal responsive to the flow rate not dropping or dropping below the predetermined level to thereby characterize the uterine cavity as perforated or non-perforated, respectively.

6. The method ofclaim 5, wherein the predetermined level is 0.05 slpm.

7. The method ofclaim 1, wherein measuring comprises measuring the flow rate over a predetermined first time interval after initiation of the flow.

8. The method ofclaim 7, wherein the first time interval is in a range from 1 second to 60 seconds.

9. A method for performing a procedure relating to uterine ablation, comprising:

introducing an ablation device through a cervical canal into a uterine cavity of a patient;

expanding at least one expandable structure carried by the probe;

introducing a flow of a fluid into the uterine cavity wherein an expanded structure confines the fluid about a distal end portion of the device in the uterine cavity; and

measuring a flow rate of the fluid being introduced, wherein a measured flow rate which drops to a level below a predetermined minimum level indicates that the uterus is non-perforated.

10. The method ofclaim 1, wherein each expandable structure has a fluid-tight wall.

11. The method ofclaim 10, wherein an expandable structure is configured to contact tissue in the cervical canal.

12. The method ofclaim 10, wherein an expandable structure is configured to contact tissue in the uterine cavity.

13. The method ofclaim 1, further comprising generating a signal responsive to the flow rate not dropping or dropping below the predetermined level to thereby characterize the uterine cavity as perforated or non-perforated, respectively.

14. The method ofclaim 5, wherein the predetermined level is 0.05 slpm.

15. The method ofclaim 9, further comprising, responsive to the uterine cavity being characterized as non-perforated, automatically delivering energy to the uterine cavity with the ablation device.

16. The method ofclaim 9, further comprising, responsive to the uterine cavity being characterized as perforated, automatically disabling energy delivery from the ablation device.

17. A method for performing a procedure relating to uterine ablation, comprising:

introducing an ablation device through a cervical canal into a uterine cavity of a patient;

expanding at least one expandable structure carried by the device to occupy at least one of the cervical canal and uterine cavity;

introducing a flow of a fluid into the uterine cavity into a space around the portion of the device in the uterine cavity; and

measuring a flow rate of the fluid being introduced, wherein a measured flow rate which drops to a level below a predetermined minimum level indicates that the uterus is non-perforated.

18. The method ofclaim 1, further comprising generating a signal responsive to the flow rate not dropping or dropping below the predetermined level to thereby characterize the uterine cavity as perforated or non-perforated, respectively.

19. The method ofclaim 17, further comprising, responsive to the uterine cavity being characterized as non-perforated, automatically delivering energy to the uterine cavity with the ablation device.

20. The method ofclaim 17, further comprising, responsive to the uterine cavity being characterized as perforated, automatically disabling energy delivery from the ablation device.

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