Cavitation nozzle assembly

• US 4,342,425 A
• Filed: 08/15/1980
• Issued: 08/03/1982
• Est. Priority Date: 04/10/1980
• Status: Expired due to Term

• Current Assignee: Her Majesty The Queen In Right of Canada As Represented By The Minister of National Defence
• Original Assignee: Her Majesty The Queen In Right of Canada As Represented By The Minister of National Defence
• Inventors: Vickers, Geoffrey W.
• Primary Examiner(s): Marbert, James B.
• Application Number:
  US06/178,603
• Time in Patent Office: 718 Days
• Field of Search: 239/423, 239/424, 239/499, 239/584, 239/596, 239/601, 239/288.5, 134/1, 175/67, 175/340, 175/422, 175/393, 299/14, 299/17, 299/37
• US Class Current: 239/424
• CPC Class Codes: B05B 1/34 designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl designed to control volume of flow B05B1/30
• CPC Class Codes: B05B 1/3402 to avoid or to reduce turbulencies, e.g. comprising fluid flow straightening means
• CPC Class Codes: B05B 13/00 Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00 B05B5/08 takes precedence ; means for supplying or discharging liquid or other fluent material for this purpose, see the relevant preceding groups; processes for applying liquids or other fluent materials to surfaces in general B05D
• CPC Class Codes: B05B 17/04 operating with special methods
• CPC Class Codes: B24C 5/02 Blast guns, e.g. for generating high velocity abrasive fluid jets for cutting materials perforating by fluid jet B26F1/26
• CPC Class Codes: E02F 3/9206 Digging devices using blowing effect only, like jets or propellers E02F5/107 takes precedence; passive suction heads with jets E02F3/925; active suction heads with jets E02F3/9262; drilling by jets E21B7/18; slitting by jets E21C25/60

Abstract

A cavitation nozzle assembly is described for discharging a high velocity jet of liquid with cavitation bubbles therein. The nozzle assembly includes a supply chamber having an upstream portion divergent in a downstream direction, a downstream portion convergent in the downstream direction, and a central section of generally constant cross-sectional area. The convergent portion is conical in form and encloses an angle of about 65°-90°, more preferably 75° to 85° and optimally about 80°. The convergent portion converges to a discharge orifice having a circular cross-section with a diameter in the range from about 1.2 mm to about 4.0 mm. In a more preferred form, liquid distribution means are provided adjacent to the discharge orifice, configured to produce a shroud of said liquid at low pressure surrounding the high velocity jet. In another preferred embodiment, the central section of the supply chamber has a diameter from about 12 mm to about 50 mm. Still more preferably, the convergent portion and discharge orifice are provided in a disc-like nozzle element, preferably releasably secured to define a downstream end of the supply chamber. In yet another preferred embodiment the nozzle element has a plurality of said discharge orifices. In a further preferred embodiment positioning means are provided to abut a surface being treated, and causing the high velocity jet to impinge the surface at an angle from about 30° to about 60°.

Claims

1. A cavitation nozzle assembly adapted to be connected to a source supplying liquid under superatmospheric pressure and for discharging a high velocity jet of said liquid with cavitation bubbles therein, said nozzle comprising inter alia;

a supply chamber connectible to said source for receiving said liquid therefrom, said chamber including an upstream portion divergent in a downstream direction, a downstream portion convergent in the downstream direction, and a central section of generally constant cross-sectional area interconnecting the divergent and convergent portions, said convergent portion being conical in form and converging to an apex so as to define an enclosed angle of about 65°

to 90°

; and

a discharge orifice at the apex of the convergent portion, and being circular in cross-section with a diameter in the range from about 1.2 mm to about 4.0 mm, said supply liquid undergoing expansion upon passage through said orifice such that cavitation bubbles form in the high velocity jet discharged therefrom.

2. The nozzle assembly defined in claim 1, wherein said convergent portion converges to a discharge orifice having a diameter in the range from about 1.6 mm to about 3.0 mm with a length to diameter ratio of about 1.8.

3. The nozzle assembly defined in claim 1, wherein said enclosed angle is from 75°

to about 85°

, and liquid distributor means are provided for developing a shroud of said liquid at a pressure lower than that in the supply chamber, said shroud substantially completely surrounding the high velocity jet of said liquid.

4. The nozzle assembly defined in claim 1, 2 or 3 wherein said central section has a diameter in the range of about 15 mm to about 50 mm.

5. The nozzle assembly defined in claim 1, wherein the converging portion of the supply chamber is defined by a disc-like nozzle element.

6. The nozzle assembly defined in claim 5 wherein the nozzle element is releasably secured, and defines a downstream end of the supply chamber.

7. The nozzle assembly defined in claim 3, wherein said distribution means supplying said shroud of liquid is in the form of a distribution collar, said collar being removeably retained in a housing and defining therewith an annular region of liquid at the lower pressure, said annular region being located generally concentrically of the nozzle element, said collar having flow channels therein to enable the formation of said shroud of low pressure liquid surrounding the high velocity jet.

8. The nozzle assembly defined in claim 1 wherein said divergent upstream portion has its longitudinal axis at least substantially parallel to the axis of said convergent downstream portion.

9. The nozzle assembly defined in claim 8 wherein the axes of said divergent upstream portion, said central section and said convergent downstream portion are in coaxial alignment.

10. The nozzle assembly defined in claim 1 wherein the diameter of said discharge orifice is about 1.6 mm, said enclosed angle is about 80°

, and said central section has a diameter in the range of about 15 mm to about 50 mm.

14. The nozzle assembly defined in claim 1, 11 or 12, wherein a plurality of discharge orifices are provided, symmetrically disposed about a vertical apex of the converging portion.

15. The nozzle assembly defined in claim 1, 11 or 12, wherein a plurality of discharge orifices are provided, symmetrically disposed about a virtual apex of the converging portion, each of such orifices being in the range from about 1.5 mm to about 3.0 mm.

11. A cavitation nozzle assembly adapted to be connected to a source supplying liquid under superatmospheric pressure, and operable to discharge a high velocity jet of said liquid with cavitation bubbles therein, said nozzle assembly comprising, inter alia;

an inlet housing adapted to be connected to said source of liquid, and defining an inlet channel, an upstream portion of a chamber, divergent in a downstream direction and connected to the inlet channel, and a central section of the chamber, of generally constant cross-sectional area;

a terminal housing of generally tubular form, having an open upstream end and a downstream end having radially inwardly extending flange means to define an exit for the high velocity jet, said terminal housing being secured to the inlet housing, said terminal housing also including liquid distribution means connectible to a supply of liquid at a pressure lower than that of said source and configured to provide a shroud of liquid surrounding said high velocity jet upon discharge from said nozzle assembly; and

a disc-like nozzle element having a conically formed central portion configured to enclose an angle in the range of about 75°

to 85°

, said central portion converging to define a discharge orifice, with the nozzle element being releasably retained by the inlet and terminal housings and positioned such that the central portion of said nozzle element converges in a downstream direction.

12. The nozzle assembly defined in claim 11, wherein said central section of the chamber is of a diameter in the range of about 15 mm to about 50 mm.

13. The nozzle assembly defined in claim 11 or 12 wherein said discharge orifice has a diameter in the range from about 1.2 mm to about 4.0 mm.

16. The nozzle assembly defined in claim 11, or 12, wherein said liquid distribution means is in the form of a bobbin-like tubular collar having radially outwardly extending flange means at upstream and downstream ends thereof, there being flow channels through a body portion of the collar to enable development of said shroud of low pressure liquid.

17. The nozzle assembly defined in claim 11 or 12, wherein said liquid distribution means in in the form of an annular chamber formed generally concentrically of the nozzle element, there being flow directing means operatively associated with said annular chamber to enable formation of said shroud of liquid at low pressure, surrounding the high velocity jet.