US2016270837A1PendingUtilityA1
Atrial septal aneurysm transseptal access system
Est. expiryJun 21, 2033(~7 yrs left)· nominal 20-yr term from priority
C12N 15/1093C40B 40/02C07K 2319/735A61B 2217/005A61B 2018/0212A61B 18/0218A61B 18/02A61B 2018/0038A61B 17/3478A61B 2018/0275C12N 2710/16645C12N 2810/855C07K 2319/03G01N 33/6854
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Claims
Abstract
A transseptal access stability system (TASS) and method of use thereof is disclosed. The TASS includes a venous sheath for reducing the likelihood of complications that may arise when performing transseptal punctures. The TASS uses either suction force or cryo-based energy for securing the fossa ovale against the rim of the orifice of the venous sheath. A method of performing a transseptal puncture using the presently disclosed TASS also is disclosed.
Claims
exact text as granted — not AI-modified1 . A transseptal access stability system comprising a cardiac catheter, wherein the cardiac catheter comprises:
a venous sheath comprising an orifice defined by a rim at a distal end thereof, wherein the rim is configured to secure a fossa ovale thereto, and wherein the venous sheath is fluidly coupled to at least one of a vacuum source and a cryoenergy source at a proximal end thereof; and a hollow dilator having a transseptal needle operationally positioned therein, wherein the dilator and needle are axially positioned through the venous sheath and wherein the dilator and the needle each have a distal end configured to protrude from the orifice at the distal end of the venous sheath and are adapted to be advanced and retracted to puncture a interatrial septum through the fossa ovale.
2 . The transseptal access stability system of claim 1 , wherein the venous sheath is curved at the distal end by an angle α.
3 . The transseptal access stability system of claim 2 , wherein angle α has a range from about 0 degrees to about 160 degrees.
4 . The transseptal access stability system of claim 2 , wherein angle α is fixed.
5 . The transseptal access stability system of claim 2 , wherein angle α is adjustable.
6 . The transseptal access stability system of claim 5 , wherein angle α is adjustable by a steering mechanism coupled to the proximal end of the venous sheath.
7 . The transseptal access stability system of claim 1 , wherein the proximal end of the venous sheath is coupled to a hemostatic valve in fluid communication with the venous sheath and the at least one of a vacuum source and a cryoenergy source.
8 . The transseptal access stability system of claim 1 , wherein the proximal end of the venous sheath is coupled to a pressure gauge in fluid communication with the venous sheath and the at least one of a vacuum source and a cryoenergy source.
9 . The transseptal access stability system of claim 1 , wherein the venous sheath is fluidly coupled to at least one of a vacuum source and a cryoenergy source via a side port at the proximal end thereof.
10 . The transseptal access stability system of claim 1 , further comprising a regulator in fluid communication with at least one of the vacuum source and the cryoenergy source for controlling a pressure within the venous sheath or a flow of coolant from the cryoenergy source.
11 . The transseptal access stability system of claim 1 , wherein the venous sheath comprises a plurality of channels and wherein the plurality of channels are fluidly coupled to at least one of a vacuum source and a cryoenergy source at a proximal end thereof.
12 . The transseptal access stability system of claim 11 , further comprising a porous end cap coupled to the distal end of the venous sheath, and wherein the porous end cap has a plurality of pores in fluid communication with the plurality of channels.
13 . The transseptal access stability system of claim 9 , wherein each pore comprising the plurality of pores has a geometry selected from the group consisting of a straight-walled hole, an idealized taper, a trumpet geometry, a wine glass geometry, and a champagne flute geometry, and wherein each port can be the same or different.
14 . The transseptal access stability system of claim 1 , wherein the venous sheath comprises a 9.5 Fr sheath.
15 . The transseptal access stability system of claim 1 , further comprising a J-wire.
16 . A method for performing a transseptal puncture on a subject in need of treatment thereof, the method comprising:
(a) providing a transseptal access stability system (TASS) of claim 1 including a J-wire; (b) accessing the femoral venous of the subject and inserting a J-wire into the vein thereof; (c) advancing the venous sheath with the assembled dilator of the TASS over the J-wire and into the vein; (d) once positioned in the heart of the subject, removing the J-wire and leaving the venous sheath and the dilator in place; (e) inserting the needle into the dilator; (f) positioning the venous sheath/dilator/needle assembly against the septum of the fossa ovale; (g) advancing the venous sheath over the dilator/needle until the venous sheath is in direct contact with the septal tissue; (h) applying suction force to the venous sheath; (i) performing the transseptal puncture by puncturing the interatrial septum with the needle; and (j) releasing the suction force and advancing the venous sheath and the dilator across the punctured septum.
17 . A kit comprising:
(a) a transseptal access stability system of claim 1 ; and (b) a J-wire.
18 . The kit of claim 17 , further comprising instructions for use of the kit for performing a transseptal puncture on a subject in need of treatment thereof.Cited by (0)
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