Claims
- 1. A method of performing a surgical procedure, comprising the steps of:
advancing a delivery catheter to a procedure specific area; activating a laser fiber assembly disposed within the delivery catheter; and advancing the laser fiber assembly to create a treatment specific hole at the procedure specific area.
- 2. The method according to claim 1, wherein the laser fiber assembly further comprises a Ho:YAG laser.
- 3. The method according to claim 1, further comprising the step of articulating the delivery catheter, prior to activating the laser fiber assembly, wherein a distal portion of the delivery catheter assumes an angular configuration.
- 4. The method according to claim 1, wherein the delivery catheter further comprises an inner sheath.
- 5. A method of performing a surgical procedure other than arthroscopy and endoscopy, comprising the steps of:
advancing a delivery catheter to a procedure specific area; activating a laser fiber assembly disposed within the delivery catheter; and advancing the laser fiber assembly to create a treatment specific hole at the procedure specific area.
- 6. The method according to claim 5, wherein the laser fiber assembly further comprises a Ho:YAG laser.
- 7. The method according to claim 5, further comprising the step of extending an inner sheath disposed within the delivery catheter, prior to activating the laser fiber assembly, wherein a distal portion of the inner sheath assumes an angular configuration.
- 8. The method according to claim 5, further comprising the step of articulating the delivery catheter, prior to activating the laser fiber assembly, wherein a distal portion of the delivery catheter assumes an angular configuration.
- 9. A method of performing a surgical procedure, comprising the steps of:
advancing a delivery catheter to a procedure specific area; activating a laser fiber assembly disposed within the delivery catheter, wherein at least one fastener is positioned at the distal portion of the laser fiber assembly; advancing the laser fiber assembly and the at least one fastener through at least one material at the procedure specific area to create a treatment specific hole in at least one material; and retracting the laser fiber assembly such that the at least one fastener remains inserted in the at least one material.
- 10. The method according to claim 9, wherein the laser fiber assembly further comprises a Ho:YAG laser.
- 11. The method according to claim 9, further comprising the step of articulating the delivery catheter, prior to activating the laser fiber assembly, wherein a distal portion of the delivery catheter assumes an angular configuration.
- 12. The method according to claim 9, wherein the delivery catheter further comprises an inner sheath.
- 13. A method of performing a surgical procedure, comprising the steps of:
advancing a delivery catheter through a vessel to a procedure specific area within the vessel; activating a laser fiber assembly disposed within the delivery catheter, wherein at least one fastener is positioned at a distal portion of the laser fiber assembly; advancing the laser fiber assembly and the fastener through a surgical component and the vessel to create a treatment specific hole in the surgical component and the vessel through which the fastener extends; and retracting the laser fiber assembly such that the at least one fastener remains attached to the surgical component and the vessel.
- 14. The method according to claim 13, wherein the laser fiber assembly further comprises a Ho:YAG laser.
- 15. The method according to claim 13, further comprising the step of extending an inner sheath disposed within the delivery catheter, prior to activating the laser fiber assembly, wherein a distal portion of the inner sheath assumes an angular configuration.
- 16. The method according to claim 13, wherein the laser fiber assembly is advanced before the at least one fastener is advanced.
- 17. A method of performing a surgical procedure, comprising the steps of:
advancing a delivery catheter through a vessel to a procedure specific area within a vessel; extending the delivery catheter such that an inner sheath of the delivery catheter extends from the delivery catheter, wherein an end portion of the inner sheath assumes an angular configuration; advancing the inner sheath from within the delivery catheter such that the delivery catheter contacts a surgical component at a location opposite to a point of contact of the inner sheath; further advancing the inner sheath such that the inner sheath contacts the surgical component; activating a laser fiber assembly disposed within the inner sheath, wherein at least one fastener is positioned at a distal portion of the laser fiber assembly; advancing the laser fiber assembly and the at least one fastener through the surgical component and the vessel to create a treatment specific hole in the surgical component and the vessel through which the fastener extends; and retracting the laser fiber assembly and the inner sheath such that the at least one fastener remains attached to the surgical component and the vessel.
- 18. The method according to claim 17, wherein the laser fiber assembly further comprises a Ho:YAG laser.
- 19. The method according to claim 17, wherein the laser fiber assembly is advanced before the at least one fastener is advanced through the surgical component and the vessel.
- 20. A method of performing a surgical procedure, comprising the steps of:
threading a suture through a passageway of a delivery catheter, wherein the delivery catheter contains a laser fiber assembly; activating the laser fiber assembly; and advancing the laser fiber assembly into the passageway to transect the suture.
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] The present application is a continuation-in-part of, and is entitled to the benefit of the earlier filing date and priority of, U.S. Non-Provisional application Ser. No. 09/783,313, filed on Feb. 15, 2001, which is entitled to the benefit of the earlier filing date and priority of U.S. Provisional Application Serial No. 60/182,543, filed on Feb. 15, 2000. An embodiment of the present invention relates to, and is entitled to the benefit of the earlier filing date and priority of U.S. Provisional Application Serial No. 60/371,500, filed on Apr. 11, 2002.
Provisional Applications (2)
|
Number |
Date |
Country |
|
60182543 |
Feb 2000 |
US |
|
60371500 |
Apr 2002 |
US |
Continuation in Parts (1)
|
Number |
Date |
Country |
Parent |
09783313 |
Feb 2001 |
US |
Child |
10411135 |
Apr 2003 |
US |