Surgical probe with independent energy sources

Patent metadata

Field	Value
Publication number	US-12178498-B2
Application number	US-202218000786-A
Country	US
Kind code	B2
Filing date	Apr 20, 2022
Priority date	Apr 20, 2021
Publication date	Dec 31, 2024
Grant date	Dec 31, 2024

Abstract

An energy source is offset from an elongate probe axis with an extension. The amount of offset of the energy source can be controlled by varying an amount of offset of the extension. The energy source rotated and translated at the offset distance to resect tissue. In some embodiments, the probe is configured to receive a second treatment probe comprising a second energy source, in which the second energy source is rotated and translated relative to the first treatment probe, which can improve positional accuracy and stability. The energy source and the extension can be coupled to a linkage to offset the energy source, and to translate and rotate the energy source with varying amounts of offset. The linkage can be coupled to a processor and one or more of the energy source moved in accordance with a treatment profile.

First claim

What is claimed is:

1. A probe for treating a subject, comprising:
an energy source;
a sheath
an elongate shaft comprising an elongate axis, the elongate shaft configured to move the energy source with translation of the elongate shaft along the elongate axis relative to the sheath, the elongate shaft located within the sheath to allow rotation and translation of the energy source relative to the sheath with an extension deflected away from the elongate axis,
wherein the extension is coupled to the elongate shaft with a link to rotate the extension about the link to move the energy source away from the elongate axis with movement of the extension away from the elongate axis to offset the energy source from the elongate axis; and
a fluid supply channel and a fluid removal channel within the sheath, wherein the fluid supply channel comprises an irrigation channel and the fluid removal channel comprises an aspiration channel, wherein the fluid supply channel and the fluid removal channel are sized and shaped to engage each other within the sheath with one or more of the fluid supply channel or the fluid removal channel sized and shaped to receive the elongate shaft coupled to the energy source to allow rotation and translation of the energy source with the energy source deflected away from the elongate axis.

2. The probe of claim 1 , wherein the energy source comprises a water jet evacuation source.

3. The probe of claim 1 , wherein the fluid supply channel is sized and shaped to receive the elongate shaft to provide fluid supply to a surgical site along the fluid supply channel with the elongate shaft placed within the fluid supply channel.

4. The probe of claim 1 , wherein the fluid removal channel is sized and shaped to receive the elongate shaft to remove fluid from a surgical site along the fluid removal channel with the elongate shaft placed within the fluid removal channel.

5. The probe of claim 1 , wherein the fluid supply channel comprises a first tube and the fluid removal channel comprises a second tube and the first tube and the second tube are sized and shaped to engage each other to provide rotational stability while the elongate shaft rotates and translates.

6. The probe of claim 5 , further comprising a resilient structure coupled to the sheath, the first tube, and the second tube to urge the first tube and the second tube toward each other and provide rotational stability.

7. The probe of claim 5 , wherein the first tube comprises a first portion and the second tube comprises a second portion sized and shaped to engage the first portion with a nested configuration.

8. The probe of claim 5 , wherein the first tube comprises a first portion with a first surface profile and the second tube comprises a second portion with a second surface profile sized and shaped to engage the first surface profile.

9. The probe of claim 8 , wherein the first surface profile and the second surface profile comprise a curved protrusion and a curved recess to engage each other along an axially extending length of the curved protrusion and the curved recess.

10. The probe of claim 8 , wherein the first portion and the second portion comprise a plurality of engagement structures sized and shaped to engage each other.

11. The probe of claim 10 , wherein the plurality of engagement structures comprises a plurality of protrusions and a plurality of recesses sized and shaped to fit together in an interlocking configuration.

12. The probe of claim 11 , wherein the plurality of engagement structures extends axially along the first tube and the second tube to provide torsional stability to the elongate shaft.

13. The probe of claim 8 , wherein the first tube comprises a third surface profile sized and shaped to engage an interior of the sheath and the second tube comprises a fourth surface profile sized and shaped to engage the interior of the sheath.

14. The probe of claim 1 , wherein the sheath comprises stiffness to add rigidity and stabilize the energy source with movement of the elongate shaft and movement of the energy source relative to the sheath.

15. The probe of claim 1 further comprising a spine coupled to the sheath to add stiffness to the probe.

16. The probe of claim 15 , wherein the spine extends distally beyond the energy source.

17. The probe of claim 16 , wherein the spine comprises a tube comprising one or more of the fluid supply channel or the fluid removal channel coupled to one or more openings distal to the energy source to provide a fluid or remove material generated by the energy source.

18. The probe of claim 1 , wherein the energy source comprises one or more of an electrode, a loop electrode, a monopolar electrode, a bipolar electrode, a radiofrequency source, a microwave source, a plasma source, a heat source, a laser source, a mechanical energy source, a mechanical sheer source, a vibrational energy source, an ultrasound energy source, cavitating ultrasound source, a water jet, a fixed pressure water jet, a variable pressure water jet, a water jet evacuation source, an eductor pump, a steam source, a morcellator, photo-ablation energy source, an ionizing radiation energy source, a radioisotope, an ionized plasma source, or a cryogenic energy source.

Assignees

• Procept Biorobotics Corp

Inventors

• Mantri Surag
• Staid Kevin Patrick
• Badia James Luis
• Ho Friedrich
• Taylor Scott D
• Bentley Peter

Classifications

• A61B2217/007

  with irrigation system · CPC title

• A61B2217/005

  with suction drainage system · CPC title

• A61B34/30

  Surgical robots · CPC title

• A61B2090/064

  for measuring force, pressure or mechanical tension · CPC title

• A61B2090/3937

  Visible markers · CPC title