Smart blade technology to control blade instability
A method of determining instability of an ultrasonic blade includes monitoring a phase angle φ between voltage Vg(t) and current Ig(t) signals applied to an ultrasonic transducer, coupled to an ultrasonic blade via an ultrasonic waveguide, inferring the blade temperature based on the phase angle φ, comparing the inferred temperature to an ultrasonic blade instability trigger point threshold, and adjusting a power level applied to the ultrasonic transducer to modulate the temperature of the blade. The method may also include determining a frequency/temperature relationship of an ultrasonic blade that exhibits a displacement or modal instability and compensating for a thermal induced instability of the ultrasonic blade. The method may be implemented in an ultrasonic surgical instrument or by a control circuit in a power generator for the ultrasonic surgical instrument.
1. A method of determining instability of an ultrasonic blade, the method comprising:
monitoring a phase angle φ between a drive voltage Vg(t) signal and a drive current Ig(t) signal applied to an ultrasonic transducer, wherein the ultrasonic transducer is coupled to the ultrasonic blade via an ultrasonic waveguide;
inferring an ultrasonic blade temperature based on the phase angle φ between the drive voltage Vg(t) signal and the drive current Ig(t) signal applied to the ultrasonic transducer;
comparing the inferred temperature of the ultrasonic blade to an ultrasonic blade instability trigger point threshold; and
adjusting a power level applied to the ultrasonic transducer to modulate the temperature of the ultrasonic blade.
2. The method of claim 1 , further comprising determining a frequency/temperature relationship of an ultrasonic blade that exhibits a displacement or modal instability.
3. The method of claim 2 , wherein determining a frequency/temperature relationship of an ultrasonic blade that exhibits a displacement or modal instability comprises:
sweeping a frequency of the drive voltage V g (t) signal of the ultrasonic transducer; and
determining the ultrasonic blade instability trigger point threshold at the temperature.
4. The method of claim 2 , wherein determining a frequency/temperature relationship of an ultrasonic blade that exhibits a displacement or modal instability comprises:
sweeping a frequency of the drive current I g (t) signal; and
determining the ultrasonic blade instability trigger point threshold at the temperature.
5. The method of claim 2 , wherein determining a frequency/temperature relationship of an ultrasonic blade that exhibits a displacement or modal instability comprises:
sweeping a frequency of the drive voltage V g (t) signal and the drive current I g (t) signal, of the ultrasonic transducer; and
determining the ultrasonic blade instability trigger point threshold at the temperature.
6. An ultrasonic surgical instrument comprising:
an ultrasonic electromechanical system comprising an ultrasonic transducer coupled to an ultrasonic blade via an ultrasonic waveguide; and
a generator configured to supply power to the ultrasonic transducer, wherein the generator comprises a control circuit configured to:
monitor a phase angle φ between a drive voltage Vg(t) signal and a drive current Ig(t) signal applied to the ultrasonic transducer,
infer an ultrasonic blade temperature based on the phase angle φ between the drive voltage Vg(t) signal and the drive current Ig(t) signal applied to the ultrasonic transducer;
compare the inferred temperature of the ultrasonic blade to an ultrasonic blade instability trigger point threshold; and
adjust a level of the power supplied by the generator and applied to the ultrasonic transducer to modulate the temperature of the ultrasonic blade.
7. The ultrasonic surgical instrument of claim 6 , wherein the control circuit is further configured to determine a frequency/temperature relationship of an ultrasonic blade that exhibits a displacement or modal instability.
8. The ultrasonic surgical instrument of claim 7 , wherein the control circuit is further configured to:
sweep a frequency of the drive voltage V g (t) signal of the ultrasonic transducer; and
determine the ultrasonic blade instability trigger point threshold at the temperature.
9. The ultrasonic surgical instrument of claim 7 , wherein the control circuit is further configured to:
sweep a frequency of the drive current I g (t) signal; and
determine the ultrasonic blade instability trigger point threshold at the temperature.
10. The ultrasonic surgical instrument of claim 7 , wherein the control circuit is further configured to:
sweep a frequency of the drive voltage V g (t) signal and the drive current I g (t) signal, of the ultrasonic transducer; and
determine the ultrasonic blade instability trigger point threshold at the temperature.
11. The ultrasonic surgical instrument of claim 6 , wherein the control circuit is further configured to compensate for a thermal induced instability of the ultrasonic blade.
12. The ultrasonic surgical instrument of claim 6 , wherein the ultrasonic blade instability trigger point threshold is a temperature causing thermal expansion of the ultrasonic blade.
13. The ultrasonic surgical instrument of claim 6 , wherein the ultrasonic blade instability trigger point threshold is a temperature enhancing structural flaws in an ultrasonic blade material.
14. A generator for an ultrasonic surgical instrument, the generator comprising:
a control circuit configured to:
monitor a phase angle φ between a drive voltage Vg(t) signal and a drive current Ig(t) signal applied to an ultrasonic transducer, wherein the ultrasonic transducer is coupled to an ultrasonic blade via an ultrasonic waveguide;
infer an ultrasonic blade temperature based on the phase angle φ between the drive voltage Vg(t) signal and the drive current Ig(t) signal applied to the ultrasonic transducer;
compare the inferred temperature of the ultrasonic blade to an ultrasonic blade instability trigger point threshold; and
adjust a power level applied to the ultrasonic transducer to modulate the temperature of the ultrasonic blade.
15. The generator of claim 14 , wherein the control circuit is further configured to determine a frequency/temperature relationship of an ultrasonic blade that exhibits a displacement or modal instability.
16. The generator of claim 15 , wherein the control circuit is further configured to:
sweep a frequency of the drive voltage V g (t) signal of the ultrasonic transducer; and
determine the ultrasonic blade instability trigger point threshold at the temperature.
17. The generator of claim 15 , wherein the control circuit is further configured to:
sweep a frequency of the drive current I g (t) signal; and
determine the ultrasonic blade instability trigger point threshold at the temperature.
18. The generator of claim 15 , wherein the control circuit is further configured to:
sweep a frequency of the drive voltage V g (t) signal and the drive current I g (t) signal, of the ultrasonic transducer; and
determine the ultrasonic blade instability trigger point threshold at the temperature.
19. The generator of claim 14 , wherein the control circuit is further configured to compensate for a thermal induced instability of the ultrasonic blade.
20. An ultrasonic surgical system, comprising:
a processor and a non-transitory memory, wherein the non-transitory memory comprises instructions that, when executed by the processor, cause the processor to:
monitor a phase angle φ between a drive voltage Vg(t) signal and a drive current Ig(t) signal applied to an ultrasonic transducer, wherein the ultrasonic transducer is coupled to an ultrasonic blade via an ultrasonic waveguide;
infer an ultrasonic blade temperature based on the phase angle φ between the drive voltage Vg(t) signal and the drive current Ig(t) signal applied to the ultrasonic transducer;
compare the inferred temperature of the ultrasonic blade to an ultrasonic blade instability trigger point threshold;
adjust a power level applied to the ultrasonic transducer to modulate the temperature of the ultrasonic blade; and
determine a frequency/temperature relationship of an ultrasonic blade that exhibits a displacement or modal instability.