IP Library Granted Patent US 10,368,954
Granted Patent B2
US 10,368,954 · App. 14/631,810 · Granted Aug 6, 2019

Method of decoupling rotation of a surgical instrument shaft supporting an end effector from rotation of a drive shaft drivingly coupled with a mechanism of the end effector

Inventors: Gabriel F. Brisson (Albany, CA); William Burbank (Sandy Hook, CT)
Assignee: Intuitive Surgical Operations, Inc.
A61B34/70A61B17/00A61B34/30A61B34/71A61B17/28A61B17/29A61B34/32A61B34/37A61B2017/00367A61B2017/00398A61B2017/00477A61B2017/2901A61B2017/293A61B2017/2903A61B2017/2929A61B2017/2932A61B2017/2936A61B2017/2938A61B2017/2943A61B2034/2059A61B2034/301A61B2034/302A61B2034/303A61B2034/715A61B2090/067
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Quick Facts
Patent No.
US 10,368,954
App. No.
14/631,810
Granted
Aug 6, 2019
Kind
B2
Abstract

Surgical assemblies and related methods are disclosed that provide for decoupling of instrument shaft roll and end effector actuation. A surgical assembly includes a base, an instrument shaft rotationally mounted to the base, an end effector supported at a distal end of the instrument shaft and including an actuation mechanism driven by a rotational motion, a drive shaft rotationally coupled with the actuation mechanism and configured to provide the rotational motion to the actuation mechanism, and a differential rotationally coupled to the drive shaft and receiving a first input motion and a second input motion. The differential combines the first and second input motions to generate an output motion that rotates the drive shaft. The first input motion is rotationally coupleable to an actuation source. The second input motion is coupled to rotation of the instrument shaft relative to the base.

Claims (65)

1. A method of decoupling rotation of a surgical instrument shaft supporting an end effector from rotation of a drive shaft drivingly coupled with a rotational input of a mechanism of the end effector, the method comprising:

rotating the end effector relative to a base by rotating the surgical instrument shaft relative to the base around an instrument shaft axis;

rotating a first input link of a differential relative to the base, the rotation of the first input link relative to the base being associated with a desired rotation of the rotational input relative to the end effector, the differential comprising a planetary gear assembly having a sun gear, planet gears coupled to a carrier, and a ring gear;

rotating a second input link of the differential relative to the base in response to the rotation of the surgical instrument shaft relative to the base;

rotating, via the differential, an output link of the differential relative to the base in response to the rotation of the first input link relative to the base and the rotation of the second input link relative to the base; and

rotating the drive shaft relative to the end effector in response to the rotation of the output link of the differential relative to the base.

2. The method of claim 1 , wherein the rotation of the first input link rotates the carrier, the rotation of the second input link rotates the sun gear, and the rotation of the drive shaft is generated by rotation of the ring gear.

3. The method of claim 2 , wherein:

the rotation of the carrier is generated via an input shaft of the differential; and

the sun gear rotates around the input shaft.

4. The method of claim 3 , wherein the input shaft is oriented transverse to the surgical instrument shaft.

5. The method of claim 1 , comprising returning the end effector mechanism to a predetermined configuration upon a disconnect between an actuation source controlling rotation of the first input link of the differential and the first input link.

6. The method of claim 1 , wherein the mechanism of the end effector comprises a clamping mechanism, a stapling mechanism, or a cutting mechanism.

7. The method of claim 1 , wherein the end effector is pivotally mounted to a distal portion of the surgical instrument shaft.

8. The method of claim 1 , wherein:

the surgical instrument shaft is rotationally mounted to the base;

the surgical instrument shaft has a distal end and a proximal end;

the surgical instrument shaft axis extends through the distal end and the proximal end; and

the end effector rotates around the instrument shaft axis during the rotation of the end effector relative to the base.

9. A method of decoupling rotation of a surgical instrument shaft supporting an end effector from rotation of a drive shaft drivingly coupled with a rotational input of a mechanism of the end effector, the method comprising:

rotating the end effector relative to a base by rotating the surgical instrument shaft relative to the base around an instrument shaft axis;

rotating a first input link of a differential relative to the base, the rotation of the first input link relative to the base being associated with a desired rotation of the rotational input relative to the end effector;

rotating a second input link of the differential relative to the base in response to the rotation of the surgical instrument shaft relative to the base;

rotating, via the differential, an output link of the differential relative to the base in response to the rotation of the first input link relative to the base and the rotation of the second input link relative to the base;

rotating the drive shaft relative to the end effector in response to the rotation of the output link of the differential relative to the base; and

returning the end effector mechanism to a predetermined configuration upon a disconnect between an actuation source controlling rotation of the first input link of the differential and the first input link.

10. The method of claim 9 , wherein:

the rotation of the first input link relative to the base comprises rotating the first input link relative to the base around the instrument shaft axis in a first direction; and

the rotation of the output link relative to the base comprises rotating the output link relative to the end effector around the instrument shaft axis in the first direction.

11. The method of claim 10 , wherein:

the rotation of the first input link relative to the base around the instrument shaft in the first direction reorients the first input link relative to the base by a first rotational amount; and

the rotation of the output link relative to the end effector around the instrument shaft in the first direction reorients the output link relative to end effector by the first rotational amount.

12. The method of claim 9 , wherein the mechanism of the end effector comprises a clamping mechanism, a stapling mechanism, or a cutting mechanism.

13. The method of claim 9 , wherein the end effector is pivotally mounted to a distal portion of the surgical instrument shaft.

14. The method of claim 9 , wherein:

the surgical instrument shaft is rotationally mounted to the base;

the surgical instrument shaft has a distal end and a proximal end;

the surgical instrument shaft axis extends through the distal end and the proximal end; and

the end effector rotates around the instrument shaft axis during the rotation of the end effector relative to the base.

15. A method of decoupling rotation of a surgical instrument shaft supporting an end effector from rotation of a drive shaft drivingly coupled with a rotational input of a mechanism of the end effector, the method comprising:

rotating the end effector relative to a base by rotating the surgical instrument shaft relative to the base around an instrument shaft axis;

moving a first cable relative to the base, the movement of the first cable being associated with a desired rotation of the rotational input relative to the end effector;

moving a second cable in response to the rotation of the surgical instrument shaft relative to the base;

moving a first pulley and a second pulley in response to the movement of the second cable;

engaging the first cable with each of the first pulley and the second pulley; and

rotating the drive shaft in response to the movement of the first cable.

16. The method of claim 15 , wherein the second cable engages an approximately 180 degree sector of each of the first pulley and the second pulley.

17. The method of claim 15 , wherein:

the surgical instrument shaft is rotationally mounted to the base;

the surgical instrument shaft has a distal end and a proximal end;

the surgical instrument shaft axis extends through the distal end and the proximal end; and

the end effector rotates around the instrument shall axis during the rotation of the end effector relative to the base.

18. A method of decoupling rotation of a surgical instrument shaft supporting an end effector from rotation of a drive shaft drivingly coupled with a rotational input of a mechanism of the end effector, the method comprising:

rotating the end effector relative to a base by rotating the surgical instrument shaft relative to the base around an instrument shaft axis;

moving a first cable in response to the rotation of the surgical instrument shaft relative to the base;

moving a second cable relative to the base, the movement of the second cable being associated with a desired rotation of the rotational input relative to the end effector;

moving a first pulley and a second pulley in response to the movement of the second cable;

engaging the first cable with each of the first pulley and the second pulley; and

rotating the drive shaft in response to the movement of the first cable.

19. The method of claim 18 , wherein the first cable engages an approximately 180 degree sector of each of the first pulley and the second pulley.

20. The method of claim 18 , wherein:

the surgical instrument shaft is rotationally mounted to the base;

the surgical instrument shaft has a distal end and a proximal end;

the surgical instrument shaft axis extends through the distal end and the proximal end; and

the end effector rotates around the instrument shaft axis during the rotation of the end effector relative to the base.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 13, 2019
From: BRISSON, GABRIEL F.; BURBANK, WILLIAM
To: INTUITIVE SURGICAL OPERATIONS, INC.
Reel/Frame 049163/0609 →
Continuity (4)
Division 13297168 · Nov 15, 2011
Provisional Application 61491798 · May 31, 2011
Provisional Application 61413885 · Nov 15, 2010
Related Publication 20150173732A1 · Jun 25, 2015
Cited By (1)
US 12,193,669