The present disclosure relates to cryoprobes for use in cryosurgical systems for treatment of benign or cancerous tissues. More particularly, the present invention pertains to cryoprobes and related methods of constructing the cryoprobes to incorporate electrical heating and thermal sensing capabilities.
Cryosurgical probes are used to treat a variety of diseases. Cryosurgical probes quickly freeze diseased body tissue, causing the tissue to die after which it will be absorbed by the body, expelled by the body, sloughed off or replaced by scar tissue. Cryothermal treatment can be used to treat prostate cancer and benign prostate disease. Cryosurgery also has gynecological applications. In addition, cryosurgery may be used for the treatment of a number of other diseases and conditions including, but certainly not limited to, breast cancer, liver cancer, renal cancer, glaucoma and other eye diseases.
A variety of cryosurgical instruments variously referred to as cryoprobes, cryosurgical probes, cryosurgical ablation devices, cryostats and cryocoolers have been used for cryosurgery. These devices typically use the principle of Joule-Thomson expansion to generate cooling. They take advantage of the fact that most fluids, when rapidly expanded, become extremely cold. In these devices, a high pressure gas mixture is expanded through a nozzle inside a small cylindrical shaft or sheath typically made of steel. The Joule-Thomson expansion cools the steel sheath to a cold temperature very rapidly. The cryosurgical probes then form ice balls which freeze diseased tissue. A properly performed cryosurgical procedure allows cryoablation of the diseased tissue without undue destruction of surrounding healthy tissue.
Cryosurgery often involves a cycle of treatments in which the targeted tissue is frozen, allowed to thaw, and then refrozen. Thawing can occur naturally or can be accelerated by use of a heat source. Double and even triple freeze/thaw cycles are now commonly used in cryosurgery. When comparing a single freeze/thaw cycle with treatment regimens involving multiple freeze/thaw cycles, it has been observed that the additional freeze/thaw cycles can lead to an increase the damage/destruction of the targeted tissue, thus providing for a more beneficial and efficacious treatment.
The present disclosure is directed to a cryoprobe including heating capabilities within the cryoprobe tip for use in a cryosurgical system. A heating element can be operably secured to an inner surface of the cryoprobe tips, wherein the heating element can then be connected to an electrical current source such that heat is generated at the cryoprobe tip as the electrical current flows through the heating element. In some embodiments, the heating element can comprise a resistive element laminated between layers of insulation while in other, alternative embodiments, the heating element can comprise a small diameter resistance wire attached directly to an inner surface within the cryoprobe tip. In some embodiments, a thermocouple can be secured within the cryoprobe tip so as to take temperature measurements during both freezing and thawing cycles. In some embodiments, the heating element can be operably secured within the cryoprobe tip using an expanding or rotating mandrel.
In one aspect of the present disclosure, a cryoprobe for use in a cryosurgical system includes a resistive heating element. The heating element can be secured to an inner surface of a cryoprobe tip and subsequently connected to an electrical current source. A thermocouple can be secured in combination with the heating element so as to measure temperature during freezing and thawing cycles. In some embodiments, the thermocouple can be operably connected to a thermal cutoff so as to break the electrical circuit between the electrical current source and the heating element if the cryoprobe tip exceeds a selected temperature. In some embodiments, the cryoprobe can further include a Joule-Thompson expansion element and related fluid channels so that it can alternately be used for both freezing and heating.
In another aspect of the present disclosure, representative methods for securing resistive heating elements within a cryoprobe tip can include the use of an expandable mandrel. In one embodiment, the expandable mandrel can include a substantially cylindrical body having a plurality of longitudinal grooves and a rounded end that can conform to the inner geometry of a cryoprobe tip. The expandable mandrel can further include a connector for connecting to a pneumatic pressure source. Alternatively, the expandable mandrel can comprise a pair of substantially half-cylinder portions having longitudinal grooves and a rounded end. The half-cylinder portions can create an opening extending longitudinally through the mandrel.
In yet another aspect of the present disclosure, an expandable mandrel can be used to secure heating elements to the inner surfaces of cryoprobe tips. Heating elements can be positioned within longitudinal grooves an on outer surface of the expandable mandrel and coated with an adhesive. The expandable mandrel can then be inserted into the cryoprobe tip and expanded to press the heating elements against the inner surface of the cryoprobe tip until the adhesive cures. In one representative embodiment, the expandable mandrel can comprise a flexible material capable of being expanded using pneumatic pressure. In another representative embodiment, the expandable mandrel can comprise a pair of body members capable of being outwardly biased by an insertion pin that is rotated though a center opening defined between the body members. Once the heating elements are secured to the inner surface of the cryoprobe tip, the biasing means can be removed such that the expandable mandrel can be removed.
The above summary of the various representative embodiments of the invention is not intended to describe each illustrated embodiment or every implementation of the invention. Rather, the embodiments are chosen and described so that others skilled in the art may appreciate and understand the principles and practices of the invention. The figures in the detailed description that follows more particularly exemplify these embodiments.
These as well as other objects and advantages of this invention, will be more completely understood and appreciated by referring to the following more detailed description of the presently preferred exemplary embodiments of the invention in conjunction with the accompanying drawings of which:
A representative closed loop cryosurgical system 100 that can be used with cryoprobes according to the present disclosure is illustrated in
With reference to
Each cryoprobe 114 has a tip 116 that constitutes the region of the cryoprobe 114 that performs the actual cryogenic treatment. The tip 116 contains the Joule-Thompson expansion element 119, such as a capillary tube, through which refrigerant can be expanded to create the cold temperatures used to freeze diseased tissue. During a cooling cycle, an iceball is formed at tip 116 that is subsequently positioned against diseased tissue such that tissue is frozen and dies.
As presently contemplated, cryoprobe 114 can also contain electrical heating and/or thermal sensing elements within tip 116, as illustrated in
Various heating elements 120 can be used with cryoprobes 114. One representative heating element 120 can comprise a wrapped thermofoil heater having an etched foil, resistive element laminated between two layers of flexible, thin insulation. Such a heating element can encircle the full inner circumference of the cryoprobe tip 116 or only partly cover it by attaching a strip to one “side” of the inner surface 118 of the cryoprobe tip 116. Alternatively, heating element 120 can comprise a small diameter (0.003 in. to 0.008 in.) resistance wire. Resistance wire can run in a longitudinal direction along the inner surface 118 of cryoprobe tip 116 with 180 degree loops at either end of the cryoprobe tip 116. Where desired, the amount of wire can be increased by attaching lengths of wire at different radial points around the circumference of the cryoprobe tip 116.
Because of the small inside diameter of cryoprobe tips 116 (typically 1.5-2.5 mm), it can be difficult to secure heating elements to the inner surface 118 of tips 116. In one presently contemplated fabrication method, heating elements 120 can be secured to the inner surface 118 of cryoprobe tips 116 with an expandable mandrel 200 as illustrated in
A first step in securing heating elements 120 to the inner surface 118 of cryoprobe tips 116 with mandrel 200 involves positioning the heating elements 120 within the external, longitudinal grooves 204. For instance, one heating element 120 can positioned so as to run along the length of a first groove 204a, loop over the rounded end 206 of mandrel 200, and run back along the length of a second groove 204b that is 180 degrees opposed to the first groove 204. A second heating element 120 can be similarly positioned within third groove 204c, looped over rounded end 206 and run back within fourth groove 204d. When looping the heating elements 120 over the rounded end 206, it is preferable that some slack be left at the end of the loop to accommodate expansion of the mandrel within the cryoprobe tip 116 as described below. By looping the heating elements 120 over the rounded end 206, a complete heating circuit can be positioned at the cryoprobe tip 116 to generate heat. The heating elements 120 can then be coated, covered and/or encased in an adhesive selected so as to not bond with the mandrel 200. A mold release compound and/or other lubricant can also be used to ensure that the heating elements 120 do not adhere to the mandrel 200.
Once the heating elements 120 have been positioned, the mandrel 200 can be inserted into the cryoprobe tip 116. A pneumatic pressure source can then be connected to mandrel 200 via connector 208 in order to expand the mandrel 200. A mandrel 200 comprised of a thin, inflatable material will inflate like a balloon until the heating elements 120 are flush with the inner surface of cryoprobe tip 116. Mandrel 200 is left in this inflated disposition within the cryoprobe tip 116 until the adhesive cures. Preferably, the adhesive is somewhat viscous so that it remains within the grooves 204 and does not leak out elsewhere within the cryoprobe 114 before it cures. The mandrel 200 can then be removed and the heating elements 120 will remain secured to the inner surface 118 of cryoprobe tip 116. Mandrel 200 can also be used to secure a thermal cutoff 122 and a thermocouple 126 to the inner surface of cryoprobe tip 116.
In an alternative attachment step, heating elements 120 can be secured to cryoprobe tip 116 using a mandrel 300 as illustrated in
As with mandrel 200, heating elements 120 can be positioned with respect to mandrel 300 such that the heating elements 120 are run through groove 304a, looped about rounded end 306, through groove 304b and coated with an adhesive. Following insertion of the mandrel 300 within the cryoprobe tip 166, mandrel 300 can be expanded by inserting a pin or other rotatable center piece to force the mandrel portions 301, 302 apart so that the heating elements 120 are held against the inner surface 118 of cryoprobe tip 116. Once the adhesive cures, mandrel 300 can be removed.
As an alternative to a conventional adhesive, an Ultra-Violet (UV) curable epoxy can be used in conjunction with both mandrel 200 and mandrel 300 to securing heating elements 120 to the inner surface 118 of cryoprobe tip 116. When a UV curable epoxy is used, mandrel 200 and mandrel 300 can each be fabricated of a transparent material. Mandrel 200 and mandrel 300 can each include a UV light source contained therein. Upon insertion and expansion of mandrel 200 or mandrel 300, the UV light source can be activated so as to cure the UV epoxy and secure the heating elements 120 to the inner surface 118 of cryoprobe tip 116.
Once the heating elements 120 are secured inside the cryoprobe tip 116, the leads 124, 128 can be connected to the control console 102. Control console 102 can selectively control the flow of electrical current through the heating elements 120 depending upon whether the treatment plan is operating in a freeze or thaw cycle. By using resistive heating elements, the use of heated gases and/or liquids and the associate flow channels necessary for their use can be avoided within the cryosurgical system 100. The use of electric resistive heating elements can also provide for faster and more responsive temperature adjustment and transitions at the cryoprobe tip 116. The thermocouple 126 can be used to measure the tip 116 temperature during both freezing and heating cycles.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiments, it will be apparent to those of ordinary skill in the art that the invention is not to be limited to the disclosed embodiments. It will be readily apparent to those of ordinary skill in the art that many modifications and equivalent arrangements can be made thereof without departing from the spirit and scope of the present disclosure, such scope to be accorded the broadest interpretation of the appended claims so as to encompass all equivalent structures and products.
The present application claims priority to U.S. Provisional Application Ser. No. 60/866,238, filed Nov. 17, 2006 and entitled “CRYOPROBE WITH HEATING AND TEMPERATURE SENSING CAPABILITIES”, which is herein incorporated by reference in its entirety.
Number | Date | Country | |
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60866238 | Nov 2006 | US |