Surgical method and apparatus for positioning a diagnostic or therapeutic element within the body and pressure application probe for use with same

• US 6,416,505 B1
• Filed: 05/05/1998
• Issued: 07/09/2002
• Est. Priority Date: 05/05/1998
• Status: Expired due to Term

• Current Assignee: Boston Scientific Scimed (Boston Scientific Corporation)
• Original Assignee: Scimed Life Systems Incorporated (Boston Scientific Corporation)
• Inventors: Fleischman, Sidney D., Whayne, James G., Thompson, Russell B.
• Primary Examiner(s): PEFFLEY, MICHAEL F
• Application Number:
  US09/072,835
• Time in Patent Office: 1,526 Days
• Field of Search: 606/1, 606/41, 606/42, 606/45-52, 606/108, 606/185, 607/100-102, 607/115, 607/116
• US Class Current: 606/1
• CPC Class Codes: A61B 18/1482 having a long rigid shaft for accessing the inner body transcutaneously in minimal invasive surgery, e.g. laparoscopy
• CPC Class Codes: A61B 2018/00136 with polymer
• CPC Class Codes: A61B 2018/0016 Energy applicators arranged in a two- or three dimensional array
• CPC Class Codes: A61B 2018/00351 Heart
• CPC Class Codes: A61B 2018/00577 Ablation
• CPC Class Codes: A61B 2018/00797 measured by multiple temperature sensors
• CPC Class Codes: A61B 2018/00821 measured by a thermocouple
• CPC Class Codes: A61B 2018/124 switching the output to different electrodes, e.g. sequentially
• CPC Class Codes: A61B 2018/1253 monopolar

Abstract

A surgical method and apparatus for positioning a diagnostic or therapeutic element within the body. The apparatus may be catheter-based or a probe including a relatively short shaft.

Claims

1. A pressure application probe for use with a surgical device, the surgical device including an elongate structure, defining a distal region, a distal region outer diameter not greater than about 5 mm and a predetermined length sufficient to allow a physician to manipulate the distal region when the elongate structure is inserted into a body cavity through an incision, and at least one energy transmission device on the distal region, the pressure application probe comprising:

an elongate main body portion defining a distal end, a proximal end and a length of at least four inches; and

a unitary substantially c-shaped engagement device adapted to releasably engage the surgical device elongate structure and including a pair of ends defining an opening therebetween, a mid-portion secured to the main body portion and an interior region defining a size corresponding to the diameter of the distal region of the surgical device elongate structure.

2. A pressure application probe as claimed in claim 1, wherein the engagement device is covered with electrically insulating material.

3. A pressure application probe as claimed in claim 1, wherein the elongate main body portion defines first and second longitudinal ends and the substantially c-shaped engagement device defines a first substantially c-shaped engagement device and is associated with the first longitudinal end of the main body portion, the pressure application probe further comprising:

a second engagement device associated with the second longitudinal end of the main body portion and adapted to releasably engage the surgical device elongate structure.

4. A pressure application probe as claimed in claim 1, wherein the pair of ends comprises a pair of free ends and the distal opening between the free ends of the c-shaped engagement device is wider than the distal region of the surgical device elongate structure.

5. A pressure application probe as claimed in claim 1, wherein the main body portion defines a length corresponding to the length of the surgical device elongate structure.

6. A pressure application probe as claimed in claim 1, wherein the main body portion defines a length sufficient to allow a physician to manipulate the distal end when the main body portion is inserted into the thoracic cavity through an incision.

7. A pressure application probe as claimed in claim 1, wherein the main body portion is malleable.

8. A pressure application probe as claimed in claim 1, wherein the elongate main body portion defines a length of at least 8 inches.

9. A pressure application probe as claimed in claim 1, wherein the elongate main body portion defines a length of at least 12 inches.

10. A pressure application probe as claimed in claim 1, wherein the ends of the c-shaped engagement device point distally.

11. A surgical apparatus, comprising:

an energy transmission probe including a handle and a support member connected to the handle, the support member defining an exterior surface and having a having a proximal portion that is one of rigid and malleable and a distal portion, and at least one energy transmission device on the distal portion of the support member; and

a pressure application probe including an elongate main body portion and an engagement device adapted to releasably engage the exterior surface of the support member and transmit distally directed force to the support member.

12. A surgical apparatus as claimed in claim 11, wherein the support member comprises relatively short shaft.

13. A surgical apparatus as claimed in claim 12, wherein the relatively short shaft defines a distal end, the support member further comprising a bendable spline assembly associated with the distal end of the relatively short shaft.

14. A surgical apparatus as claimed in claim 11, wherein the at least one energy transmission device comprises a plurality of energy transmission devices.

15. A surgical apparatus as claimed in claim 11, wherein the engagement device comprises a generally c-shaped member.

16. A surgical apparatus as claimed in claim 11, wherein the engagement device is covered with electrically insulating material.

17. A surgical apparatus as claimed in claim 11, wherein the support member and engagement device are respectively constructed such that the pressure application probe can be moved relative to the energy transmission probe when the pressure application probe and energy transmission probe are engaged.

18. A surgical apparatus as claimed in claim 11, wherein the energy transmission probe and pressure application probe are separate structural elements that can be readily separated from one another.

19. A surgical apparatus as claimed in claim 11, wherein the pressure application probe includes a malleable elongate main body portion.

20. A pressure application probe for use with a surgical device, the surgical device including a shaft defining a distal end and a predetermined length sufficient to allow a physician to manipulate the distal end when the shaft is inserted into a body cavity through an incision, a support member associated with the distal end of the shaft and at least one energy transmission device on the support member, the pressure application probe comprising:

an elongate main body portion defining a length substantially equal to the length of the surgical device shaft; and

a unitary substantially c-shaped engagement device adapted to releasably engage the support member and having a pair of ends defining an opening therebetween and a mid-portion secured to the main body portion.

21. A method of forming a lesion in tissue, comprising the steps of:

providing an energy transmission probe including a support member and at least one energy transmission device on the support member;

inserting the energy transmission probe directly into a bodily cavity through an incision in a patient;

positioning the energy transmission probe within the patient such that the energy transmission device is adjacent tissue;

providing a pressure application probe;

inserting the pressure application probe into the patient;

engaging the support member with the pressure application probe; and

transmitting energy to the tissue through the at least one energy transmission device.

22. A method as claimed in claim 21, wherein the step of positioning the energy transmission probe within the patient comprises inserting the support member through a first port and the step of inserting the pressure application probe into the patient comprises inserting the pressure application probe through a second port.

23. A method as claimed in claim 21, further comprising the step of:

applying pressure to the support member with the pressure application probe.

24. A method as claimed in claim 21, further comprising the step of:

reorienting the support member with the pressure application probe.

25. A method as claimed in claim 21, wherein the step of inserting the energy transmission probe directly into a patient includes performing one of a thoracostomy, thoracotomy or median sternotomy prior to inserting the energy transmission probe into