# Patent

## Title
Ultrasonic medical device operating in a transverse mode

## Abstract

An ultrasonic medical device comprises an ultrasonic vibration generator that generates vibration along its longitudinal axis. The ultrasonic vibration is transmitted through an ultrasonic coupler and a series of transformer sections that amplify the ultrasonic vibration. A flexible member is coupled to the distal end of the transformer sections, and is thus supplied with a longitudinal vibration at its base by the transformer sections. The flexible member is designed so that it converts the longitudinal vibration into a standing wave that runs along the length of the flexible member. The standing wave produces a series of nodes and anti-nodes along the length of the flexible member. Each of the anti-nodes produces cavitation in fluids in contact with the probe. The cavitation of the fluids causes destruction of adjacent tissue. In this manner, the entire length of the flexible member becomes a working surface that may be utilized for destroying tissue.

## Background
RELATED APPLICATIONS
This is a continuation of application Ser. No. 09/618,352, filed Jul. 19, 2000, which claims the benefit of Provisional Application Ser. No. 60/178,901, filed Jan. 28, 2000, and claims the benefit of Provisional Application Ser. No. 60/157,824, filed Oct. 5, 1999, the entirety of all these applications are hereby incorporated herein by reference.


BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates generally to medical devices, and more particularly to an ultrasonic medical device for destroying tissue in a controlled fashion within a human body.
2. Description of Related Art
Medical instruments utilizing ultrasonic energy to destroy tissue in a human body are known in the art. One drawback of existing ultrasonic medical instruments which remove tissue is that typically doctors have considered them to be slow in comparison to methods such as surgical excision. Part of the reason for this perceived slowness is explained by the fact that most existing ultrasonic devices rely on a longitudinal vibration of the tip of the probe. In other words, the tip of the probe is vibrated in a direction in line with the longitudinal axis of the probe. This produces a tissue destroying affect only at the tip of the probe.
One solution that has been proposed is to vibrate the tip of the probe in a transverse direction—i.e. perpendicular to the longitudinal axis of the probe—in addition to vibrating the tip in the longitudinal direction. For example, U.S. Pat. No. 4,961,424 to Kubota et al. discloses an ultrasonic treatment device to destroy and emulsify concretions or tissue in a human body. The Kubota et al. device produces both a longitudinal and transverse motion at the tip of the probe. The Kubota et al. patent, however, still relies solely on the tip of the probe to act as a working surface. Therefore, it improves the efficiency of the tip, but still relies on the tip of the probe to perform all cutting actions.
Although Kubota et al. describe providing a transverse motion at the tip of the probe, a transverse motion along the length of the probe has generally been discouraged. For example, U.S. Pat. No. 4,474,180 to Angulo discloses an ultrasonic kidney stone disintegration instrument with a damping material applied to the wire probe to inhibit lateral vibrations of the wire in the region of the connection to the ultrasonic transducer.
Another proposed method of improving the speed of ultrasonic tissue remove is oscillating the tip of the probe in addition to longitudinally vibrating the tip of the probe. For example, U.S. Pat. No. 4,504,264 to Kelman discloses an ultrasonic treatment device which improves the speed of ultrasonic tissue removal. In the Kelman device, the tip of the probe is vibrated longitudinally and also oscillated, so that the cutting efficiency of the probe tip is improved. Again, however, only the tip of the probe performs a cutting action.
BRIEF SUMMARY OF THE INVENTION
The object of the present invention is to provide an ultrasonic medical device capable of destroying and emulsifying tissue through cavitation in the human body with a higher efficiency by means of a flexible probe operating in a transverse mode. As used herein, a transverse mode of operation is used to describe a flexible probe with a plurality of nodes and anti-nodes along the length of the probe.
In accordance with this object, an ultrasonic medical device comprises an ultrasonic vibration generator that generates vibration along its longitudinal axis. The ultrasonic vibration is transmitted through an ultrasonic coupler and a series of transformer sections that amplify the ultrasonic vibration. A flexible member is coupled to the distal end of the transformer sections, and is thus supplied with a longitudinal vibration at its base by the transformer sections. The flexible member is designed so that it converts the longitudinal vibration into a standing wave that runs along the length of the flexible member. The standing wave produces a series of nodes and anti-nodes along the length of the flexible member. Each of the anti-nodes produces cavitation in fluids in contact with the probe. The cavitation of the fluids causes destruction of adjacent tissue. Thus, in this manner, the entire length of the flexible member becomes a working surface that may be utilized for destroying tissue.
Therefore, in contrast to the prior art designs that only utilize a tip of a probe as a surface, the entire length of the flexible member forms a cutting surface in the present invention.



BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 shows a schematic view of an ultrasonic probe constructed in accordance with the principles of the invention;
FIG. 2 shows the flexible member of the ultrasonic probe operating in a transverse mode;
FIG. 3 shows a probe assembly for use in an ultrasonic probe constructed in accordance with the principles of the invention;
FIG. 4 shows a cross-sectional view of the handle assembly of an ultrasonic probe constructed in accordance with the principles of the invention;
FIGS. 5A-5D show possible various cross-sectional profiles of a flexible member for use in the present invention; and
FIG. 6 shows the ultrasonic probe and an associated sheath.



DETAILED DESCRIPTION OF THE INVENTION
As seen in FIGS. 1 and 3, the ultrasonic probe has a handle section 10 and a probe section 12. The handle is formed by an ultrasonic driver 14 and an ultrasonic coupling horn 16. The ultrasonic driver has a longitudinal axis. The driver produces an ultrasonic vibration in the range of 20-80 kHz. The nominal driver amplitude is 50 microns at 100 volt peak to peak sinusoidal excitation. The vibration is along the direction of the longitudinal axis. In the embodiment illustrated, the transducer is PZT-4. However, the driver can utilize a variety of methods to produce an ultrasonic vibration, such as piezoelectric, magnetostrictive, pneumatic, or hydraulic, as are known to those skilled in the art. A control unit (not illustrated) controls the ultrasonic driver. The control unit allows an operator to adjust the frequency and amplitude of the vibration which is produced by the driver. In the exemplary embodiment illustrated here, the probe is designed to operate at a frequency of 20 kHz. However, the probe may be designed to operate at frequencies in the range of 20 kHz to 80 kHz, as described in detail in the theory of operation section.
The ultrasonic driver is coupled to a coupling horn 16, and the ultrasonic vibration is transmitted from the driver to the coupling horn. The coupling horn is connected to the probe section 12. The probe section has a series of transformer sections 18, 20. The transformer sections are a series of shafts constructed from any suitable material, such as Ti-6Al-4v titanium. The transformer sections transmit vibrations from the coupling horn to a flexible member 22 at the distal end of the probe section. In the process of transmission, the amplitude of the vibration is amplified by the transformer sections. The diameter of the transformer sections are chosen so as to produce a suitable amount of longitudinal vibration at the end of the transformer section. The gain of the transformer sections is controlled by the ratio of the area of the sections. In the exemplary embodiment described herein, the transformer sections are designed to produce a gain of about 4-5 over the transducer. This is achieved by setting the diameter of the transformer sections 18, 20 at 0.150 and 0.080 inches, respectively. The length of the transformer sections 18, 20 are 1.500 and 7.554 inches, respectively. The transformer section 18 has a threaded portion 24 to mate with the coupling horn 16, and has a portion 26 which is adapted so that it may be grasped with a wrench or another tool to tighten the connection.
A flexible member 22 is attached to the end of the last transformer section, and is driven by the last transformer section. The flexible member is a thin, wire like probe, typically less than 1 mm in diameter. In the embodiment shown, the flexible member has a circular cross-section with a diameter of 0.020 inches. The flexible member may have other cross-sections, such as a rectangular or oval cross-section. The flexible portion of the probe can be multiple wavelengths in length. In the embodiment shown, the flexible member is 4.046 inches long, which corresponds to a device operating with a frequency of approximately 20 kHz. The preferred material is 6Al-4v titanium; however, any other materials may be used as long as the operating parameters fall within the operation limits set by the strength of the material, as discussed in detail below.
FIG. 4 shows a cross-sectional view of the handle assembly of an ultrasonic probe constructed in accordance with the principles of the invention. FIG. 4 shows an exemplary horn assembly 400 suitable for use in the present invention. A housing 402 has a end cap 404 and a rear portion 406. The end cap 404 has an internal threaded portion 408 which mates with an external threaded portion 410 of the rear portion 406. The rear portion 406 of the housing 402 has a recess 412 which receives an extended portion 414 of the horn 416. The end cap 404 is shaped as a ring with a opening 418. The horn 416 fits through the opening 418. A flange 420 on the horn 416 is larger than the opening 418 so that when the end cap 404 is screwed on, the horn 416 is held tightly into the housing 402.
The horn 416 has female threads 424 at one end 426 to mate with a probe assembly. Grooves 438 are provided on the horn 416. O-rings (not shown) may be placed into the grooves to provide a substantially fluid-tight seal.
A stack of piezo-ceramic drivers 428 is arranged around the horn 416. The driver stack 428 has four driver ceramics 430, and an additional feedback ceramic 432. The feedback ceramic 432 is used to measure the driver amplitude. Each driver is provided with a nickel electrode for connection to an electrical source (not shown). The electrical source provides an alternating waveform at the appropriate frequency and amplitude. Insulators 434 are provided to isolate the piezo-ceramics from the horn and from the feedback ceramic. MACORTM insulators, available from Corning, are one suitable type of insulator. The extended portion 414 of the horn 416 is threaded so that a nut 436 may be used to secure the piezo-ceramic drivers to the horn.
FIGS. 5A-5D show various cross-sectional profiles of ultrasonic probes which are suitable for use with the present invention. As will be discussed in detail later, any cross-sectional profile may be utilized so long as certain design constraints are met.
As seen in FIG. 6, proximal to the desired, active length 606 of the probe 608, the probe 608 is placed within a sheath 600 which can provide irrigation channels and aspiration channels 602, 604. Irrigation is preferably provided between the probe 608 and the sheath 600. The sheath 600 is preferably made of PTFE or Teflon tubing so as to absorb the ultrasonic energy emanating from portions of the probe located within the sheath, thereby allowing control over the amount of tissue affected by the probe. The sheathing is not restricted to the preferred materials as long as it is made of a material which is not heated by the ultrasonic energy, although the irrigation fluid can be used to cool the sheath material. The probe may be extended or retracted from the sheath to modify the amount of probe exposed, thereby modifying the active length 606 of the probe. Further details regarding one suitable sheath are described in Applicant's co-pending application Ser. No. 60/157,824, which is hereby incorporated by reference.
Theory of Operation of the Invention
Although, not intended to be bound by the following theory of operation, it is believed that the following theory describes the operation of the ultrasonic probe of the present invention. In operation, the longitudinal push delivered by the transformer sections causes a flexing or buckling of the thin member at the end of the probe. The buckling may be realized as a flexure or standing transverse wave along the length of the probe section. The flexure case is simply the first order transverse mode of vibration as will be described below.
In a fluid or fluid containing medium, each of the anti-nodes (positions corresponding to maximum transverse displacement) along the length of the probe cause cavitation of the fluid in a direction perpendicular to the longitudinal axis of the probe.
Cavitation is a void or bubble produced by the inability of the fluid to overcome the stresses induced by the motion of the probe. The collapse of the cavitation bubbles in and around cellular (or biological) material produces a shockwave that erodes or fragments the material allowing it to be removed through aspiration and suction. The mechanism of cavitation and its affect on tissues is well known in the art, and is described in such literature as U.S. Pat. No. 3,526,219 to Balamuth.
The equations of motion governing the operation of the are obtained by applying Newton's second law to the forces and accelerations acting upon an infinitesimal segment. The equation of motion for the transverse oscillations of a thin member (neglecting losses in the material and surroundings) is then given by:




  
    
      
        
          
            
              
                ∂
                4
              
              ⁢
              ξ
            
            
              ∂
              
                X
                4
              
            
          
          +
          
            
              1
              
                
                  (
                  
                    κ
                    ⁢
                    
                      
                    
                    ⁢
                    c
                  
                  )
                
                2
              
            
            ⁢
            
              
                
                  ∂
                  2
                
                ⁢
                ξ
              
              
                ∂
                
                  t
                  2
                
              
            
          
        
        =
        0
      
    
    
      2.0
    
  




Where x is the distance along the flexible portion, t is the time in seconds ξ is the transverse displacement, κ is the radius of gyration, and c is the speed of sound in the material.

In can be shown for boundary conditions which assume a flexible member of length l fixed at one end and free at the other, the general solution to this equation will have the form:





  
    
      
        ξ
        =
        
          
            cos
            ⁡
            
              (
              
                
                  ω
                  ⁢
                  
                    
                  
                  ⁢
                  t
                
                +
                
                  φ
                  n
                
              
              )
            
          
          ⁢
          
            (
            
              
                A
                ⁡
                
                  (
                  
                    
                      cosh
                      ⁢
                      
                        
                          ω
                          ⁢
                          
                            
                          
                          ⁢
                          X
                        
                        v
                      
                    
                    -
                    
                      cos
                      ⁢
                      
                        
                          ω
                          ⁢
                          
                            
                          
                          ⁢
                          X
                        
                        v
                      
                    
                  
                  )
                
              
              +
              
                B
                ⁡
                
                  (
                  
                    
                      sinh
                      ⁢
                      
                        
                          ω
                          ⁢
                          
                            
                          
                          ⁢
                          X
                        
                        v
                      
                    
                    -
                    
                      sin
                      ⁢
                      
                        
                          ω
                          ⁢
                          
                            
                          
                          ⁢
                          X
                        
                        v
                      
                    
                  
                  )
                
              
            
            )
          
        
      
    
    
      2.1
    
  




Applying the boundary conditions it can be shown that





  
    
      
        
          
            cot
            ⁡
            
              (
              
                
                  ω
                  ⁢
                  
                    
                  
                  ⁢
                  l
                
                
                  2
                  ⁢
                  v
                
              
              )
            
          
          ⁢
          
            tanh
            ⁡
            
              (
              
                
                  ω
                  ⁢
                  
                    
                  
                  ⁢
                  l
                
                
                  2
                  ⁢
                  v
                
              
              )
            
          
        
        =
        1
      
    
    
      2.2
    
  




Where ω is the angular frequency in radians per second, x is the distance along the flexible member (as before) and v is the phase velocity given by:

ν=√{square root over (ωcκ)}  2.3

Here c is the longitudinal propagation velocity given by:

c=√{square root over (Y/ρ)}  2.4

where Y is Young's modulus and ρ is the density of the material.

The solutions of equations 2.2 only occur at discrete frequencies, which for the first four overtones can be shown to be:




  
    
      
        
          f
          n
        
        =
        
          
            π
            ⁢
            
              
            
            ⁢
            c
            ⁢
            
              
            
            ⁢
            κ
            ⁢
            
              
            
            ⁢
            
              A
              n
            
          
          
            8
            ⁢
            
              l
              2
            
          
        
      
    
    
      2.5
    
  




The An terms are the solutions to equation 2.2. For the nth overtone they are (1.194)2, (2.988)2, (5)2, (7)2 . . . (2n−1)2 

For overtones of the fundamental the node positions along the flexible member can be derived from the general solution given in equation 2.1 The nodal positions are the points at which the displacements and the bending moment are zero:




  
    
      ξ
      n
    
    =
    0
  
  ,
  
    
      
        
          ∂
          2
        
        ⁢
        
          ξ
          n
        
      
      
        ∂
        
          X
          2
        
      
    
    =
    0
  




with





  
    
      
        
          
            
              ∂
              2
            
            ⁢
            
              ξ
              n
            
          
          
            ∂
            
              X
              2
            
          
        
        =
        
          
            cos
            ⁡
            
              (
              
                
                  ω
                  ⁢
                  
                    
                  
                  ⁢
                  t
                
                +
                φ
              
              )
            
          
          ⁢
          
            
              (
              
                ω
                v
              
              )
            
            2
          
          ⁢
          
            (
            
              
                A
                ⁡
                
                  (
                  
                    
                      cosh
                      ⁢
                      
                        
                          ω
                          ⁢
                          
                            
                          
                          ⁢
                          X
                        
                        v
                      
                    
                    +
                    
                      cos
                      ⁢
                      
                        
                          ω
                          ⁢
                          
                            
                          
                          ⁢
                          X
                        
                        v
                      
                    
                  
                  )
                
              
              +
              
                B
                ⁡
                
                  (
                  
                    
                      sinh
                      ⁢
                      
                        
                          ω
                          ⁢
                          
                            
                          
                          ⁢
                          X
                        
                        v
                      
                    
                    +
                    
                      sin
                      ⁢
                      
                        
                          ω
                          ⁢
                          
                            
                          
                          ⁢
                          X
                        
                        v
                      
                    
                  
                  )
                
              
            
            )
          
        
      
    
    
      2.6
    
  




Using equations 2.1 and 2.6 it can be shown that:





  
    
      
        
          tan
          ⁢
          
            
              ω
              ⁢
              
                
              
              ⁢
              X
            
            v
          
        
        =
        
          tanh
          ⁢
          
            
              ω
              ⁢
              
                
              
              ⁢
              X
            
            v
          
        
      
    
    
      2.7
    
  




which has solutions for:





  
    
      
        
          
            ω
            ⁢
            
              
            
          
          v
        
        =
        
          
            π
            
              2
              ⁢
              l
            
          
          ⁢
          
            (
            
              5
              ,
              7
              ,
              
                9
                ⁢
                
                  
                
                ⁢
                ...
              
            
            ⁢
            
              
            
            )
          
        
      
    
    
      2.8
    
  




The positions of the nodes for a member of length 1 will then be:

    First overtone: x=0
    Second overtone x=0, x=0.7741
    Third overtone x=0, x=0.51, x=0.8681
    Fourth overtone x=0, x=0.3561, x=0.6441, x=0.9051
    Etc.

Figure Two shows the flexible portion oscillating in modes up to the fourth overtone.



For a practical design the forces acting on the flexible member have to be kept within safe limits for the material chosen. The bending moment of the flexible member is given by the equation:




  
    
      
        M
        =
        
          YA
          ⁢
          
            
          
          ⁢
          
            κ
            2
          
          ⁢
          
            
              
                ∂
                2
              
              ⁢
              ξ
            
            
              ∂
              
                x
                2
              
            
          
        
      
    
    
      3.0
    
  




with A being the cross sectional area of the flexible member. Equation 3.0 will be recognized immediately as the standard differential equation for a beam in flexure.

The shear force acting along the member will be given by the equation:





  
    
      
        
          F
          s
        
        =
        
          
            
              ∂
              M
            
            
              ∂
              x
            
          
          =
          
            YA
            ⁢
            
              
            
            ⁢
            
              κ
              2
            
            ⁢
            
              
                
                  ∂
                  3
                
                ⁢
                ξ
              
              
                ∂
                
                  x
                  3
                
              
            
          
        
      
    
    
      3.1
    
  




The preferred embodiment is a probe of circular cross section as described; however alternate shapes could be used as long as certain design constraints are considered. The key parameter is the Yκ2 term appearing in equations 3.0 and 3.1, often referred to as the flexural stiffness. For annealed Ti-6AL-4V titanium optimal values are in the range 2.5×107 to 8.5×107 N/m. Note that the use of the flexural stiffness as a design parameter allows a shape independent specification for flexible member.
The driver and transformer sections are designed to provide sufficient longitudinal amplitude to support the desired transverse mode amplitude (see section on design constraints below). Typically the handle and probe assembly are designed to support a longitudinal amplitude which will be sufficient to induce buckling in the flexible member. The length of the entire probe and handle assembly is chosen to place a longitudinal anti-node at the end of the flexible member. This restricts the length of the handle and tip assembly to integer multiples of one half the longitudinal wavelength. In actual practice it has been found that a slight de-tuning of around 3 to 5 percent aids the conversion to the transverse mode. It should be noted that there is no longitudinal vibration of the tip as this is converted entirely into a transverse vibration through buckling of the thin member at the tip.
The force, or longitudinal push, imparted to the flexible member by the longitudinal section must be sufficient to induce buckling. The maximum longitudinal force exerted at startup must meet the Euler conditions for buckling, which are the solutions to equation 3.0, yielding the formula for the critical force:




  
    
      
        
          
            P
            crit
          
          =
          
            
              
                n
                2
              
              ⁢
              
                π
                2
              
              ⁢
              Y
              ⁢
              
                
              
              ⁢
              
                κ
                2
              
            
            
              l
              2
            
          
        
        ,
        
          (
          
            
              n
              =
              1
            
            ,
            2
            ,
            
              3
              ⁢
              
                
              
              ⁢
              ...
            
          
          )
        
      
    
    
      3.2
    
  




For the longitudinal drive the maximum stress at startup will be:





  
    
      
        s
        =
        
          
            2
            ⁢
            π
            ⁢
            
              
            
            ⁢
            Y
            ⁢
            
              
            
            ⁢
            f
            ⁢
            
              
            
            ⁢
            
              ξ
              m
            
          
          c
        
      
    
    
      3.3
    
  




Where ξm is the maximum longitudinal displacement of the assembly (probe and handle), f is the drive frequency, c is the longitudinal propagation velocity (Eq. 2.4) and Y is Young's modulus for the material.

An optimal design will try to place as many anti-nodes as possible along the length of the flexible member. In the exemplary embodiment described and illustrated before, with a 3.748 inch long flexible member with a diameter of 0.020 inches, 6 nodes are produced at a frequency of 20 kHz.
The proceeding equations show that the stresses on the material increase with frequency. When coupled with the need to produce sufficient amplitude to remove tissue upper bounds for frequency can be established. To produce cavitation in fluid the transverse amplitude should be at least 75 microns. This will limit the frequency to about 80 kHz for 6Al-4V titanium (this disregards material losses which must be experimentally determined). The lower limit for the frequency is usually chosen to be outside of the range of human hearing, or greater than 20 kHz.
The transverse mode probe is much more effective at tissue removal than are the longitudinal designs of the prior art. One reason for this is because the action of the energy is along most of the length of the exposed flexible member and is not confined to the surface area of the tip of the member. The probes described in the prior art which are only driven in the longitudinal direction only work at the tip. Even with a solid tip, its active area in contact with tissue is much less than the transverse mode tip. Also, the tissue destruction of the transverse mode probes extends up to 1 mm circumferentially beyond the probe. The following calculations indicate the efficacy of the transverse mode compared to a standard longitudinal probe.
A rigid, solid, 4 mm probe works only at the tip. As it moves forward and back, it cavitates the fluid in front of it. The volume of tissue effected is:















Frequency
f
20,000 hz



Stroke
Δx
350 microns (.35 mm)


Radius
r
2 mm


Cross sectional area
Ax
πr2
12.6 mm2


Volume of tissue removed
V
Ax*Δx
4.40 mm3


per stroke


Volume of tissue removed
Vt
V*f/60/1,000
1.47 cc/min


per time









For a 2 cm long by 0.5 mm diameter probe working in the transverse mode:
















Frequency
f
20,000 hz



Radius
r
0.25 mm


Effective radius
re
1.25 mm


Effective length
L
20 mm


Cross sectional area
Ax
π re2
4.91 mm2


Volume of tissue removed per stroke
V
Ax* L
98.1 mm3


Volume of tissue removed per time
Vt
V*f/60/1,000
32.7 cc/min









This means that in these circumstances, the transverse mode tip removes tissue at a rate 22.2 times faster than the solid tip working in the longitudinal mode. Also, the transverse mode flexible member is typically 1⁄8th the size of the longitudinal probe. Comparing two, 0.5 mm probes, one working in the longitudinal mode and one in the transverse mode, the transverse mode tip removes tissue 1,428 times faster than the longitudinal probe.
The transverse mode probe is capable of maintaining its vibration when bent if the sum of the stresses imposed by the transverse vibration and the bending stresses do not exceed the elastic limit of the material. This offers significant advantages over longitudinal mode designs that are typically rigid over their entire length.

## Claims

1. An ultrasonic device comprising:
a flexible probe coupled to a horn, the flexible probe having a proximal end, a distal end and a longitudinal axis therebetween, the flexible probe comprising first and second transformer sections configured to amplify an amplitude of longitudinal vibration when longitudinal vibration is applied to the transformer sections by the horn, the first transformer section having a first diameter and the second transformer section having a second diameter, the first diameter differing from the second diameter, wherein a portion of the flexible probe extending distally from the transformer sections has a degree of stiffness which allows the portion of the flexible probe extending distally from the transformer sections to support a transverse ultrasonic vibration when longitudinal vibration is applied by the transformer sections to the portion of the flexible probe extending distally from the transformer sections, and a length and a cross section of the portion of the flexible probe extending distally from the transformer sections are sized to support the transverse ultrasonic vibration with a plurality of transverse nodes and transverse anti-nodes along the length of the portion of the flexible probe extending distally from the transformer sections.

2. The device of claim 1 wherein the cross section of the flexible probe has a small profile.

3. The device of claim 1 wherein the cross section of the flexible probe is approximately circular.

4. The device of claim 1 wherein the transverse anti-nodes are points of a maximum transverse displacement along at least a portion of the longitudinal axis of the flexible probe.

5. The device of claim 1 wherein, during use, the transverse anti-nodes cause a cavitation in a fluid containing medium in communication with the flexible probe in a direction approximately perpendicular to the longitudinal axis of the flexible probe.

6. The device of claim 1 wherein the transformer sections are located between the proximal end of the flexible probe and the distal end of the flexible probe.

7. The device of claim 1, further comprising a driver coupled to the horn, the driver configured to produce longitudinal vibration.

8. The device of claim 1, wherein the longitudinal vibration applied to the transformer sections has a frequency in the range of about 20 kHz to about 80 kHz.

9. The device of claim 1, wherein the portion of the flexible probe extending distally from the transformer sections has a length such that eight transverse nodes are produced along the length of the portion of the flexible probe extending distally from the transformer sections when the longitudinal vibration is applied by the transformer sections to the portion of the flexible probe extending distally from the transformer sections.

10. The device of claim 1, wherein the portion of the flexible probe extending distally from the transformer sections comprises titanium.

11. The device of claim 1, wherein the transformer sections are sized to produce a gain of about 4-5 over the horn.

12. The device of claim 1, wherein the portion of the flexible probe extending distally from the transformer sections has a diameter of less than about 1 millimeter.

13. The device of claim 1, wherein the portion of the flexible probe extending distally from the transformer sections has a diameter of about 0.020 inches.

14. The device of claim 1, wherein the flexural stiffness of the portion of the flexible probe extending distally from the transformer sections is in the range of about 2.5×107 N/m to about 8.5×107 N/m.

15. The device of claim 1, wherein the first transformer section comprises a threaded portion and the horn comprises a threaded portion, the threaded portion of the first transformer section configured to mate with the threaded portion of the horn.

16. The device of claim 1, further comprising a sheath, the flexible probe being disposed within the sheath.

17. An ultrasonic medical device comprising:
an ultrasonic probe coupled to an ultrasonic horn, the ultrasonic probe having a proximal end, a distal end and a longitudinal axis therebetween, the ultrasonic probe comprising first and second transformer sections located between the proximal end of the ultrasonic probe and the distal end of the ultrasonic probe, the transformer sections configured to amplify an amplitude of longitudinal vibration when longitudinal vibration is applied to the transformer sections by the ultrasonic horn, the first transformer section having a first diameter and the second transformer section having a second diameter, the first diameter differing from the second diameter, a portion of the ultrasonic probe extending distally from the transformer sections being configured to vibrate in a direction transverse to the longitudinal axis of the ultrasonic probe when longitudinal vibration is applied by the transformer sections to the portion of the flexible probe extending distally from the transformer sections.

18. The device of claim 17 wherein the cross section of the ultrasonic probe has a small profile.

19. The device of claim 17 wherein the cross section of the ultrasonic probe is approximately circular.

20. The device of claim 17 wherein, during use, a transverse ultrasonic vibration along at least a portion of the longitudinal axis of the ultrasonic probe produces a plurality of transverse nodes and transverse anti-nodes along at least a portion of the longitudinal axis of the ultrasonic probe.

21. The device of claim 20 wherein the transverse anti-nodes are points of maximum transverse displacement along at least a portion of the longitudinal axis of the ultrasonic probe.

22. The device of claim 20 wherein, during use, the transverse anti-nodes cause a cavitation in a fluid containing medium in communication with the ultrasonic probe in a direction approximately perpendicular to the longitudinal axis of the ultrasonic probe.

23. The device of claim 20 wherein, during use, more than one of the plurality of transverse antinodes is in communication with a biological material.

24. The device of claim 17, further comprising an ultrasonic driver coupled to the horn, the ultrasonic driver configured to produce longitudinal ultrasonic vibration.

25. The device of claim 17, wherein the longitudinal vibration applied to the transformer sections has a frequency in the range of about 20 kHz to about 80 kHz.

26. The device of claim 17, wherein the portion of the ultrasonic probe extending distally from the transformer sections has a length such that eight transverse nodes are produced along length of the portion of the ultrasonic probe extending distally from the transformer sections when the longitudinal vibration is applied by the transformer sections to the portion of the ultrasonic probe extending distally from the transformer sections.

27. The device of claim 17, wherein the portion of the ultrasonic probe extending distally from the transformer sections comprises titanium.

28. The device of claim 17, wherein the transformer sections are sized to produce a gain of about 4-5 over the horn.

29. The device of claim 17, wherein the portion of the ultrasonic probe extending distally from the transformer sections has a diameter of less than about 1 millimeter.

30. The device of claim 17, wherein the portion of the ultrasonic probe extending distally from the transformer sections has a diameter of about 0.020 inches.

31. The device of claim 17, wherein the flexural stiffness of the portion of the ultrasonic probe extending distally from the transformer sections is in the range of about 2.5×107 N/m to about 8.5×107 N/m.

32. The device of claim 17, wherein the first transformer section comprises a threaded portion and the horn comprises a threaded portion, the threaded portion of the first transformer section configured to mate with the threaded portion of the horn.

33. The device of claim 17, further comprising a sheath, the ultrasonic probe being disposed within the sheath.

34. An ultrasonic medical device comprising:
a flexible probe coupled to a horn, the flexible probe having a proximal end, a distal end and a longitudinal axis therebetween;
a largest diameter of the flexible probe at a proximal end of the flexible probe;
a smallest diameter of the flexible probe at a distal end of the flexible probe; and
first and second transformer sections located between the proximal end of the flexible probe and the distal end of the flexible probe, the transformer sections configured to amplify an amplitude of longitudinal vibration when longitudinal vibration is applied to the transformer section by the horn, the first transformer section having a first diameter and the second transformer section having a second diameter, the first diameter differing from the second diameter,
wherein, when longitudinal vibration is applied by the transformer sections to a portion the flexible probe extending distally from the transformer sections, a transverse ultrasonic vibration is produced along the longitudinal axis of the portion of the flexible probe extending distally from the transformer sections, which produces a plurality of transverse nodes and transverse anti-nodes along the longitudinal axis of the portion of the flexible probe extending distally from the transformer sections.

35. The device of claim 34 wherein the cross section of the flexible probe has a small profile.

36. The device of claim 34 wherein the cross section of the flexible probe is approximately circular.

37. The device of claim 34 wherein the flexible probe is configured to vibrate in a direction transverse to at least a portion of the longitudinal axis of the flexible probe.

38. The device of claim 34 wherein the transverse anti-nodes are points of a maximum transverse displacement along at least a portion of the longitudinal axis of the flexible probe.

39. The device of claim 34 wherein, during use, the transverse anti-nodes cause a cavitation in a fluid containing medium in communication with the flexible probe in a direction approximately perpendicular to the longitudinal axis of the flexible probe.

40. The device of claim 34 wherein, during use, more than one of the plurality of transverse antinodes are in communication with a biological material.

41. The device of claim 34, further comprising a driver coupled to the horn, the driver configured to produce longitudinal vibration.

42. The device of claim 34, wherein the longitudinal vibration applied to the transformer sections has a frequency in the range of about 20 kHz to about 80 kHz.

43. The device of claim 34, wherein the portion of the flexible probe extending distally from the transformer sections has a length such that eight transverse nodes are produced along the length of the portion of the flexible probe extending distally from the transformer sections when the longitudinal vibration is applied by the transformer sections to the portion of the flexible probe extending distally from the transformer sections.

44. The device of claim 34, wherein the portion of the flexible probe extending distally from the transformer sections comprises titanium.

45. The device of claim 34, wherein the transformer sections are sized to produce a gain of about 4-5 over the horn.

46. The device of claim 34, wherein the portion of the flexible probe extending distally from the transformer sections has a diameter of less than about 1 millimeter.

47. The device of claim 34, wherein the portion of the flexible probe extending distally from the transformer sections has a diameter of about 0.020 inches.

48. The device of claim 34, wherein the flexural stiffness of the portion of the flexible probe extending distally from the transformer sections is in the range of about 2.5×107 N/m to about 8.5×107 N/m.

49. The device of claim 34, wherein the first transformer section comprises a threaded portion and the horn comprises a threaded portion, the threaded portion of the first transformer section configured to mate with the threaded portion of the horn.

50. The device of claim 34, further comprising a sheath, the flexible probe being disposed within the sheath.