Balloon with integral segmented dilation elements
View Patent ↗A balloon and method of making a balloon catheter is provided. The balloon for the balloon catheter may be made by slicing through an integral dilation element on a parison ( 10 ). The parison may then be stretched to spread the slices to form wider gaps ( 20 ). The gaps define separate dilation element segments ( 14 ), which may make the balloon more flexible.
1. A method of forming a balloon for a balloon catheter, comprising:
extruding a parison having a uniform shape along an entire length thereof, said parison comprising a central opening and a dilation element extending from an exterior surface of said parison;
cutting through a portion of said dilation element;
heating and stretching at least a portion of said parison, segments of said dilation element defined by said cutting thereby separating from each other to form gaps between said segments; and
heating said parison inside a mold and pressurizing said central opening, said parison thereby expanding against said mold to form a balloon.
2. The method according to claim 1 , wherein said cutting comprises making a single blade slice through said portion, a width of said cutting thereby being approximately the same as a width of a cutting blade.
3. The method according to claim 2 , wherein said width of said cutting blade is about 0.005″ to about 0.015″.
4. The method according to claim 1 , wherein said cutting comprises cutting about 25% to about 75% through a total height of the dilation element.
5. The method according to claim 1 , wherein said parison comprises more than one of said dilation element circumferentially spaced around said exterior surface, wherein all of said cutting comprises cutting longitudinally aligned cuts along said more than one of said dilation element.
6. The method according to claim 1 , wherein said parison comprises more than one of said dilation element circumferentially spaced around said exterior surface, wherein all of said cutting comprises cutting longitudinally staggered cuts along said more than one of said dilation element, none of said cuts thereby being longitudinally aligned with another cut on one of said circumferentially spaced dilation elements.
7. The method according to claim 1 , wherein said heating and stretching are done simultaneously with said heating of said parison and pressurizing said central opening.
8. The method according to claim 1 , wherein said parison is stretched a single time after said cutting.
9. The method according to claim 1 , wherein said stretching comprises stretching said portion of said parison less than twice a length of said portion before said stretching.
10. The method according to claim 1 , further comprising preforming said parison before said cutting to form an increased diameter middle region and reduced diameter end regions.
11. The method according to claim 1 , wherein said cutting comprises making a single blade slice through said portion, a width of said cutting thereby being approximately the same as a width of a cutting blade, and said cutting further comprising cutting about 25% to about 75% through a total height of the dilation element, said stretching comprising stretching said portion of said parison less than twice a length of said portion before said stretching.
12. The method according to claim 11 , wherein said parison comprises more than one of said dilation element circumferentially spaced around said exterior surface, wherein all of said cutting comprises cutting longitudinally staggered cuts along said more than one of said dilation element, none of said cuts thereby being longitudinally aligned with another cut on one of said circumferentially spaced dilation elements, said heating and stretching being done simultaneously with said heating of said parison and pressurizing said central opening and said parison being stretched a single time after said cutting, and further comprising preforming said parison before said cutting to form an increased diameter middle region and reduced diameter end regions.
13. The method according to claim 1 , wherein said width of said cutting blade is about 0.005″ to about 0.015″ and said cutting comprises cutting about 25% to about 75% through a total height of the dilation element, said parison being stretched a single time after said cutting, and further comprising preforming said parison before said cutting to form an increased diameter middle region and reduced diameter end regions.
14. The method according to claim 13 , wherein said heating and stretching are done simultaneously with said heating of said parison and pressurizing said central opening, and said stretching comprising stretching said portion of said parison less than twice a length of said portion before said stretching.
15. The method according to claim 1 , wherein each of said gaps is less than 0.060″ after said parison is expanded against said mold.
16. The method according to claim 15 , wherein each of said gaps is 0.010″ to 0.050″ after said parison is expanded against said mold.
17. The method according to claim 1 , wherein said dilation element segments comprise a neck portion and a head portion, at least part of said neck portion extending across each of said gaps after said parison is expanded against said mold.
18. The method according to claim 1 , wherein said parison is stretched a single time after said cutting, and said heating and stretching are done simultaneously with said heating of said parison and pressurizing said central opening.
19. The method according to claim 1 , wherein said mold comprises cavities receiving said dilation element during said heating and pressurizing.
20. The method according to claim 1 , wherein said cutting comprises mounting said parison on a mandrel in a computer-controlled cutting machine, and said cuts are made with a blade attached to a head in said cutting machine.