Force sensor temperature compensation
A force sensor apparatus is provided including a tube portion having a plurality of radial ribs and at least one fiber optic strain gauge positioned over each rib of the plurality of radial ribs. A proximal end of the tube portion is operably couplable to a shaft of a surgical instrument that is operably couplable to a manipulator arm of a robotic surgical system, and a distal end of the tube portion is proximally couplable to a wrist joint coupled to an end effector. A thermal shunt shell is over an outer surface of the tube portion.
1. A method to reduce thermal differences between strain gauges located at surface locations of a tube that includes a proximal end portion operably couplable to a shaft of a surgical instrument and that includes a distal end portion operably couplable to a wrist joint of the surgical instrument, the wrist joint being operably couplable to an end effector, the method comprising:
thermally coupling strain gauges located at opposing surface locations of the tube by providing thermal pathways through multiple radial ribs comprised of a high thermal diffusivity material that run through a centerline of the tube between the strain gauges at the opposing surface locations.
2. The method of claim 1 , wherein:
each of the radial ribs is separated from an adjacent rib by 90 degrees measured about the centerline of the tube.
3. The method of claim 1 , wherein:
the multiple radial ribs include four ribs in diametrically opposite pairs at skewed supplementary angles about the centerline of the tube.
4. The method of claim 1 , wherein:
the multiple radial ribs include three ribs separated by 120 degrees about the centerline of the tube.
5. The method of claim 1 , wherein:
the multiple radial ribs include four ribs paired at skewed angles about the centerline of the tube.
6. The method of claim 1 , wherein:
the multiple radial ribs comprise a high thermal diffusivity material selected from a group consisting of an aluminum alloy, a copper alloy, and a silver alloy.
7. The method of claim 1 , wherein:
the radial ribs are disposed to provide passage for one or more of actuation cables, wires, and/or rods between the shaft and the wrist joint.
8. The method of claim 1 , wherein:
the method further includes thermally shielding the strain gauges within an outer tube that extends about the tube and about a thermally insulating region between the outer tube and the tube.
9. The method of claim 1 , wherein:
the method further includes thermally shielding the strain gauges within an outer tube that extends about the tube and about an evacuated gap region between the outer tube and the tube.
10. The method of claim 1 , wherein:
the method further includes thermally shielding the strain gauges within an outer tube that extends about the tube and about an insulating fluid filled gap between the outer tube and the tube.
11. The method of claim 1 , wherein:
the method further includes thermally shielding the strain gauges within an outer tube that extends about the tube; and
the outer tube includes a light reflective outer surface or coating.
12. The method of claim 1 , wherein:
the method further includes thermally shielding the strain gauges within an outer tube that is isolated from the tube by at least one elastomer ring located between the outer tube and the tube.
13. The method of claim 1 , wherein:
the method further includes thermally shielding the strain gauges within an outer tube that extends about the tube; and
the outer tube comprises a high thermal diffusivity material selected from a group consisting of an aluminum alloy, a copper alloy and a silver alloy.
14. A method to reduce thermal differences between strain gauges located at outer surface locations of a tube that includes a proximal end portion operably couplable to a shaft of a surgical instrument and that includes a distal end portion operably couplable to a wrist joint of the surgical instrument, the wrist joint being operably couplable to an end effector, the method comprising:
thermally shielding the strain gauges by providing a thermal shunt shell that extends about the tube, the strain gauges, and a thermally insulating region, and by providing thermal pathways through multiple radial ribs comprised of a high thermal diffusivity material, the thermal pathways running through an interior region of the tube;
wherein the thermally insulating region is located between the thermal shunt shell and the tube; and
wherein the thermally insulating region is located between the shaft of the surgical instrument and the wrist joint of the surgical instrument.
15. The method of claim 14 , wherein:
the thermally insulating region includes an evacuated gap region between the thermal shunt shell and the tube.
16. The method of claim 14 , wherein:
the thermally insulating region includes an insulating fluid filled gap between the thermal shunt shell and the tube.
17. The method of claim 14 , wherein:
the thermal shunt shell includes a light reflective outer surface or coating.
18. The method of claim 14 , wherein:
the method further includes providing an insulating coating over the thermal shunt shell.
19. The method of claim 14 , wherein:
the method further includes using at least one elastomer ring located between the thermal shunt shell and the tube to thermally isolate the strain gauges from the thermal shunt shell.
20. The method of claim 14 , wherein:
the thermal shunt shell includes a high thermal diffusivity material.