Apparatus and methods for uniformly distributing coolant within a cryo-ablation device

Abstract

Apparatus and methods for uniformly distributing coolant within a cryo-ablation device. A nozzle apparatus includes a tubular member having a plurality of angled apertures that induce swirling of coolant streams dispersed through the angled apertures. Coolant swirling round the tubular member and along an inner surface of an inflatable balloon element inflates the balloon element and cryogenically ablate tissue. The swirling action achieved using angled apertures uniformly distributes coolant along the inner surface of the balloon such that the temperatures along an inner surface of the balloon element and ablation of tissue adjacent to the balloon element are substantially uniform.

What is claimed is: 
     
         1 . A nozzle apparatus for distributing coolant within a cryo-ablation device, comprising:
 a tubular member having an inner surface and an outer surface, the inner surface defining a lumen through which coolant may flow, the tubular member defining a plurality of angled apertures extending between the inner and outer surfaces, wherein two or more of the angled apertures are formed within a single cross-sectional plane at a first location such that coolant flowing through the lumen is dispersed from the tubular member through the plurality of apertures in a spiral at the first location and into a space defined by the cryo-ablation device.   
     
     
         2 . The nozzle apparatus of  claim 1 , where in two or more angled apertures are formed within a single cross-sectional plane at a second location spaced axially from the first location such that coolant flowing through the lumen is dispersed from the tubular member through the plurality of apertures in a first spiral at the first location and a second spiral at the second location along the tubular member. 
     
     
         3 . The nozzle apparatus of  claim 1 , the tubular member being configured to uniformly distribute coolant within a substantially annular band at the first location within the cryo-ablation device. 
     
     
         4 . The nozzle apparatus of  claim 1 , wherein the tubular member is coil-shaped. 
     
     
         5 . The nozzle apparatus of  claim 1 , each angled aperture defining an axis and the tubular member defining a central axis, wherein an acute angle of about 10 degrees to about 75 degrees is defined between an axis defined by an angled aperture and a line extending radially from the central axis to the angled aperture. 
     
     
         6 . The nozzle apparatus of  claim 5 , the acute angle being sufficiently large such that no line extending radially from the central axis of the tubular member to an angled aperture extends completely through the angled aperture. 
     
     
         7 . The nozzle apparatus of  claim 1 , the tubular member defining about four to about ten angled apertures. 
     
     
         8 . The nozzle apparatus of  claim 1 , the plurality of angled apertures having a common inclination such that streams of coolant dispersed from the tubular member through the plurality of angled apertures swirl around the outer surface of the tubular member in the same direction. 
     
     
         9 . An inflatable cryo-ablation apparatus, comprising:
 a first inflatable element having an inner surface and an outer surface, the inner surface defining an inner space; and   a tubular member having an inner surface and an outer surface, the inner surface of the tubular member defining a lumen through which coolant may flow, the tubular member defining a plurality of angled apertures extending between the inner and outer surfaces such that coolant flowing through the lumen is dispersed from the tubular member through the plurality of apertures and into the inner spaced defined by the first inflatable element, wherein for each angled aperture, an acute angle is defined between an axis extending through the angled aperture and a radial line extending from a central axis of the tubular member and through the angled aperture, wherein for each aperture the axis extending therethrough extends along a single cross-sectional plane.   
     
     
         10 . The inflatable cryo-ablation apparatus of  claim 9 , the tubular member being configured to initiate swirling of streams of coolant dispersed from the tubular member through the plurality of angled apertures and in the inner space defined by the first inflatable element. 
     
     
         11 . The inflatable cryo-ablation apparatus of  claim 9 , the tubular member being configured to uniformly distribute coolant within a substantially annular band within the first inflatable element. 
     
     
         12 . The inflatable cryo-ablation apparatus of  claim 9 , wherein the tubular member is a coil-shaped. 
     
     
         13 . The inflatable cryo-ablation apparatus of  claim 9 , wherein two or more of the angled apertures are formed within a single cross-sectional plane 
     
     
         14 . The inflatable cryo-ablation apparatus of  claim 9 , wherein the acute angle is about 10 to about 75 degrees. 
     
     
         15 . The inflatable cryo-ablation apparatus of  claim 13 , wherein the acute angle is sufficiently large such that no line extending radially from the central axis of the tubular member to an angled aperture extends completely through the angled aperture. 
     
     
         16 . The inflatable cryo-ablation apparatus of  claim 9 , the tubular member defining about four to about ten angled apertures. 
     
     
         17 . The inflatable cryo-ablation apparatus of  claim 9 , the plurality of angled apertures having a common inclination such that streams of coolant dispersed from the tubular member through the plurality of angled apertures swirl in the same direction around the outer surface of the tubular member and within the inner space defined by the first inflatable element. 
     
     
         18 . The inflatable cryo-ablation apparatus of  claim 9 , further comprising a second inflatable element, the first inflatable element being positioned between the tubular member and the second inflatable element, wherein the tubular member, the first inflatable element and the second inflatable element are configured such that streams of coolant dispersed from the tubular element through the plurality of apertures swirl around the tubular member and within the inner space defined by the first inflatable element to inflate the first inflatable element and the second inflatable element. 
     
     
         19 . The inflatable cryo-ablation apparatus of  claim 9 , the tubular member and the first inflatable member being configured such that a temperature along a circumferential section of the inner surface of the first inflatable element exposed to swirling coolant dispersed through the plurality of angled apertures is substantially constant. 
     
     
         20 . The inflatable cryo-ablation apparatus of  claim 9 , the tubular member and the first inflatable member being configured such that a circumferential section of the inner surface of the first inflatable element is exposed to substantially the same amount of coolant.