The invention concerns acoustic cavitation, but more specifically, the invention concerns a method of and an apparatus for suppressing cavitation on a surface of an element in a mechanical system, such as working surfaces in hydraulic equipment.
Cavitation concentrates energy; its occurrence may deleteriously erode surfaces of mechanical elements, even elements made of tungsten or steel. Problematic cavitation is encountered in land, sea, and air vehicles or equipment, whose designs are typically made to avoid cavitation events. At least one hundred years have passed since initial studies of propeller erosion, and since then, much knowledge has been gained in the industry about bubble dynamics and the energetics of cavitation. But even today suppressing cavitation has not successfully been achieved; it still remains an engineering priority. Developing cavitation-proof structural designs and materials often leads to extremely conservative designs, invariably underrealizing the full performance potential of many systems. Cavitation also limits the amount of power that may be mechanically coupled to fluids in hydraulic systems. Fluid includes liquids or other matter in which cavitation may be invoked.
A known method to reduce cavitation includes statically over-pressuring a region over a surface where cavitation pre-emption is sought. As known in the art, subjecting an imperfectly wetted crevice-like region located on surfaces or liquid-borne particles to reduce pressure or tensile environments may nucleate cavitation. Imposing a sufficiently high static pressure on the liquid drives a crevice's liquid meniscus to its root. Eventually, the liquid may adequately wet the crevice-like feature and thus preempt cavitation. It is extremely difficult, however, to create cavitation in fully wetted regions associated with liquids because homogeneous nucleation thresholds generally exceed several hundred atmospheres of peak negative pressure. If, however, overpressuring does not fully wet all cavitation nuclei, should cavitation occur, the violence of cavitation implosion in the statically overpressured environment would be more energetic thereby causing greater surface damage, thus defeating the purpose of cavitation-proof design in the first place.
The above-mentioned hyperbaric confinement technique of cavitation suppression requires containment of the region if it is to be made cavitation-proof. Such physical containment constitutes a primary limitation to cavitation suppression on exterior surfaces of a mechanical element or structure, like a sonar dome or propeller of a sea vessel.
Thus, it is highly desirable to provide a method of and system for cavitation suppression operable in either contained or open environments, and specifically, to provide a method and a system that does not require any hyperbaric confinement.
The confinement limitation may be circumvented by subjecting the targeted region to become a “cavitation proof surface” (CPS) with high frequency ultrasonic waves. Inventor A. Ruffa of U.S. Pat. Nos. 5,996,630; 5,884,650; and 5,717,657 has suggested using a high frequency acoustic energy field, of say one MHz, to flow over the intended CPS. As is known in the art and as Ruffa indicates that such insonification will prevent cavitation occurrences because cavitation thresholds are high and the time duration available for bubble processes is small at high frequencies. However, it has found that one can indeed bring about cavitation quite readily at high frequencies upon invoking an effect known as “acoustic coaxing” to facilitate cavitation nucleation. Implementing Ruffa's suggestion does not appear operable to suppress cavitation, but in fact is believed to enhance cavitation.
According to a first aspect of the present invention, a method of suppressing cavitation in or about a region of a surface that is subjected to cavitation-producing energy comprises providing a transducer and exciting the transducer to produce a biased acoustic field comprising a series of pressure pulses in the region that exceed peak negative tensile force of cavitation-producing energy.
According to another aspect of the invention, there is provided an apparatus that suppresses cavitation in or about a region of an element subjected to cavitation events comprising a transducer and a source of power that excites the transducer to produce a biased acoustic field in and/or about the region to be protected.
Other aspects of the invention will become apparent upon review of the following description taken in connection with the accompanying drawings. The invention, though, is pointed out with particularity by the appended claims.
According to an aspect of the present invention, cavitation prevention is achieved by suppressing the rarefaction or tensile phase of insonifying waves, i.e., by ensuring that the acoustic waves only contain compressive peaks in rapid succession. Ordinarily, AC power amplifiers that drive the transducer amplify the driving voltage symmetrically about a ground reference level even when the inputs contain a DC bias. However, by introducing an appropriate biasing circuit between the output of the power amplifiers and the input of the acoustic wave producer, e.g., a transducer, it may be possible to produce an acoustic field that yields only positive pressure pulses or positive wave halves.
Driving a transducer so that high frequency, high amplitude sequences of positive pressure pulses present over the CPS of a targeted region effectively provides a “containerless” hyperbaric environment and precludes cavitation events. Various methods and apparatuses may be employed to provide such bias. For example, one can provide a diode circuit for rectification or voltage divider circuits with mixers or other suitable circuit devices to drive the acoustic transducer at one bias level—for instance, in either only positive or only negative bias level. The transducer performance is not expected to deteriorate under such biased drive because the driving does not have a tendency to cause depoling. The presence of adequately intense, rapidly fluctuating, “positive pressure” will not engender cavitation nucleation—lacking acoustic pressure pulses in a liquid region—will not engender any cavitation nucleation and hence preclude the occurrence of cavitation.
In one implementation of the invention depicted in
In actual implementation, a cavitation suppression transducer 10 may be located at a region behind the liquid-hosting cavitation, e.g., inside the propeller or sonar dome, or it may be positioned directly within the liquid at a location that subjects acoustic suppression energy directly upon the CPS area to be protected.
Once a cavitation bubble has formed it cannot be locally closed unto itself. In this regard, cavitation in liquids is like fracture in solids. The fracture in the liquid, however, assumes a spherical shape of a bubble primarily because of surface tension, and a lack of resistance on the part of the liquids for shape change. Once a bubble is formed, the only way to render the liquid at that location cavitation free is to remove the bubble by some means, hydrodynamic or kinetic buoyancy, mechanical, thermal or fluid flow.
Cavitation suppression proposed by the present invention involves prevention of bubble nucleation, and for this there should not be any reduced pressure environment, or tensile (negative pressure) pressure environment within the region of control, the CPS area (regardless of the flow conditions).
Referring to
A closer study of the vibrating piston as the source of sound in a liquid tube reveals that as long as the piston moves towards the liquid in the direction of wave propagation of the launched wave, it will generate a compressive phase of the wave. The instant the piston starts to retract, moving away from the liquid in the opposite direction to the launched wave, it begins generating expansion fans that lead to the tensile phase of the wave. To avoid expansion fans, the liquid should not encounter a receding or withdrawing piston. One way to achieve this is to impart a steady axial velocity to the piston as it vibrates, that is, to bodily move the piston into the liquid in the direction of the propagation of a launched wave at a speed so that the resultant piston velocity is never negative. Due to finite translations of most mechanical systems, however, a single piston cannot be continuously and forever moved “into” the liquid at such a steady state velocity.
An arrangement depicted in
To avoid retracting the piston from the liquid, the head of the piston should not retreat relative to the local liquid directly in front of it. One way to achieve this includes arranging for the liquid to flow onto the face of the vibrating piston in a direction 31 at a sufficient velocity, e.g., a mean velocity greater than or equal to the pressure amplitude divided by the acoustic impedance, the product of the density and the speed of sound in the liquid. This is illustrated in
In another embodiment illustrated in
One may use a flat or planar transducer if moderate compressive pulse are desired, or a focused transducers if intense compressive are needed. The above arrangement can be obviated if the liquids were incapable of supporting tension. In gaseous environments, one cannot launch a tensile wave because gases cannot support tension. If a liquid region excluding a CPS region is seeded with gas bubbles, then that two-phase region will not support tension significantly. Therefore if such a region is interposed between the piston-transducer and the CPS region, only the compressive pulses will pass through the latter. The bubbly region effectively acts as a filter or a half-wave rectifier.
The embodiments disclosed herein are exemplary and, as such, are not intended to limit the scope of the invention. Based of these teachings, modifications and adaptations are envisioned that fall within the scope of the invention defined by the appended claims.
This invention claims the benefit of U.S. Provisional Application Ser. No. 60/293,919, filed May 30, 2001, in the name of the inventor hereof. This invention also relates to U.S. application Ser. No. 09/488,574 entitled “Single Transducer ACIM Method and Apparatus” filed Jan. 21, 1999 (now U.S. Pat. No. 6,395,096), in the name of the same inventor hereof, which is incorporated herein by reference.
Number | Name | Date | Kind |
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5594165 | Madanshetty | Jan 1997 | A |
5681396 | Madanshetty | Oct 1997 | A |
5694936 | Fujimoto et al. | Dec 1997 | A |
5717657 | Ruffa | Feb 1998 | A |
5884650 | Ruffa | Mar 1999 | A |
6395096 | Madanshetty | May 2002 | B1 |
Number | Date | Country |
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2000287988 | Oct 2000 | JP |
Number | Date | Country | |
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20020179111 A1 | Dec 2002 | US |
Number | Date | Country | |
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60293919 | May 2001 | US |