US3921915A - Nozzle means producing a high-speed liquid jet - Google Patents
Nozzle means producing a high-speed liquid jet Download PDFInfo
- Publication number
- US3921915A US3921915A US380014A US38001473A US3921915A US 3921915 A US3921915 A US 3921915A US 380014 A US380014 A US 380014A US 38001473 A US38001473 A US 38001473A US 3921915 A US3921915 A US 3921915A
- Authority
- US
- United States
- Prior art keywords
- nozzle
- piston
- cavity
- exit
- nozzle means
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000007788 liquid Substances 0.000 title claims abstract description 29
- 239000012530 fluid Substances 0.000 claims description 17
- 239000002184 metal Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 abstract description 5
- 230000003068 static effect Effects 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 238000009412 basement excavation Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000010438 granite Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000005641 tunneling Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 230000002747 voluntary effect Effects 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B1/00—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
- B05B1/02—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to produce a jet, spray, or other discharge of particular shape or nature, e.g. in single drops, or having an outlet of particular shape
- B05B1/10—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to produce a jet, spray, or other discharge of particular shape or nature, e.g. in single drops, or having an outlet of particular shape in the form of a fine jet, e.g. for use in wind-screen washers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B1/00—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means
- B05B1/34—Nozzles, spray heads or other outlets, with or without auxiliary devices such as valves, heating means designed to influence the nature of flow of the liquid or other fluent material, e.g. to produce swirl
Definitions
- ABSTRACT A nozzle device producing a high-speed liquid jet, to be used for example in an apparatus to cut, break, deform, clean or otherwise treat materials, is characterized in that its internal cavity to receive a liquid column has a continuously converging contour lying within the limits defined by the following two equations: a. A/A, ⁇ ,1 (X/L) 1e/A0) 1] ⁇ b.
- A/A,, ⁇ 1 (X/L) [(Ae/A0)"" 1
- A is the variable internal cross section of the nozzle cavity
- A is the value of A at the nozzle entrance
- A is the value of A at the nozzle exit
- L is the nozzle length from entrance to exit
- X is the variable coordinate along the axis of the jet nozzle.
- the internal cavity of the nozzle of the present inven- This invention relates to a nozzle means producing a 5 tion is approximately hyperbolic in shape. its relative high-speed liquid jet to be used for example in an apparatus to cut, break, deform, clean or otherwise treat materials.
- a column of liquid is accelerated to moderate velocity, preferably by direct application of gas pressure to one end or, via the action of an intermediate free piston, and is then directed into a converging nozzle of appropriate design.
- the function of the nozzle is to redistribute the initially more or less uniform energy content of the column such that a small mass fraction at the forward or leading end contains, at discharge, essentially all the energy.
- the jet stagnation pressure thus derived can be many times the strength e.g. of even the hardest rock materials and can thus serve as a useful tool for excavation, tunneling, mining and a variety of other industrial applications.
- the prior art contour of the internal cavity of a nozzle schematically illustrated as the upper curve 4 in FIG. 1, has a radius that exponentially decreases with distance from the nozzle entrance. With this nozzle, the relative rate of area change (l/A) (SA/8X) is invariant over the entire contour.
- A is the value of A at the nozzle entrance;
- A. is-the value of A at the nozzle exit;
- FIG. 1 A free piston l strikes an initially motionless column of liquid 2 with initial velocity U,,.
- the liquid column 2 has length I and cross-sectional area
- the internal nozzle cavity of the present invention has a surface contour 5 beginning at point 6 and leads to an exit point 7.
- Contour 4 represents the prior art nozzle contour. Assuming the impedance of the piston l is many times that. of the fluid 2, as is the case for example when steel strikes water, the initial velocity of the liquid 2 atthe piston interface will be approximately U,,.
- a shock wave will be driven into the liquid with minimum velocity C the sound speed in the undisturbed fluid, and the pressure behind this shock will be at least P p C, U where p,, is the density of the undisturbed fluid.
- the shock wave When the shock wave has traversed the liquid column 2 it will reflect from the front surface 3 thereof as a rarefaction. As a result of this action, the front surface will be accelerated to a velocity of approximately 2U,,. The rarefaction will travel back towards the piston 1, increasing the velocity of the fluid behind. However, there is also a rarefaction emanating from the piston end since the ambient pressure on the back side of the piston is much lower than the shock induced value P,,.
- A is the value of A at the nozzle entrance 6; A. is the value of A at the nozzleexit 7; L is the nozzle length from entrance to exit;
- the nozzle radius will be a hyperbolic function of the running coordinate (X/L).
- the internal cavity'of the nozzle has an approximately hyperbolic shape, the continuously converging contour of the internal cavity of the nozzle lying within the limits defined by the following two equations:
- A/A,, 1 (X/L)[(Ae/A0)' 1 where v A is the variable internal cross-section of the nozzle cavity;
- A is the value of A at the nozzle entrance
- a ⁇ . is the value of A at the nozzle exit
- L is the nozzle length from entrance to exit
- X is the variable coordinate along the axis of the jet nozzle.
- FIG. 2 depicts some of the results of analysis of the various nozzle contours, based on incompressible flow theory.
- FIG. 5 illustrates a nozzle configuration which eliminates altogether the piston l of FIG. 1.
- the fluid itself functions as a piston.
- like elements are designated by like reference numerals.
- the characteristics of the embodiment of FIG. 5 in In the above table are tabulated the maximum discharge stagnation pressure Po the maximum static pressure ttained anywhere within the nozzle fi the ratio of employs a metallic piston with a nozzle of exponential contour or shape (A).
- A the maximum static pressure ttained anywhere within the nozzle fi
- A the maximum static pressure ttained anywhere within the nozzle fi
- the ratio of employs a metallic piston with a nozzle of exponential contour or shape
- B hyperbolic con+ tour
- the stagnation pressure loss can be mainly regained, without the detrimental effect of increased static wall pressure, by eliminating the intermediate piston [third configuration (C), FIG. 5].
- I09 kb more than 50 times the cornpressive strength I of conventional granite
- FIG. 3 shows the maximum static pressure distribution in each nozzle as a function of axial position.
- nozzles designed according to the prior art (A) do /P0, and the energy conversion effi ciency, 'n, for each of three possible configurations.
- FIG. 4 shows the ratio of fluid velocity to initial velocity as a function of the axial coordinate at the instant of discharge.
- the prior art design (A) is seen to have a much steeper gradient at the discharge end, the result of the steep pressure gradient within the nozzle shown in FIG. 3.
- the velocity gradients derived with the nozzle configuration of the present invention are much less severe, although the maximum discharge velocity obtained with design (C) differs by only 7% from that of design (A).
- P,,,, for design (C) is reduced to 0.25 of that obtained with design (A).
- the elimination of the piston in design (C) of FIG. 5, aside from the practical advantage gained by simplifying the machine fabrication, serves to increase the efficiency of the energy conversion process by eliminating the impedance mismatch between piston and fluid.
- a nozzle means producing a high-speed liquid jet comprising:
- A is the variable internal cross-section of the nozzle cavity
- A is the value of A at the nozzle entrance
- A is the value of A at the nozzle exit
- L is the nozzle length from entrance to exit
- X is the variable coordinate along the axis of the jet nozzle.
- a nozzle means according to claim 1 comprising means rearward of said continuously converging contour of said cavity for retaining a liquid column therein.
- a nozzle means according to claim 2 comprising a piston located rearward of said liquid column.
- a nozzle means according to claim 2 wherein said means rearward of said continuously converging eontour of said cavity retains therein a liquid column of substantially constant cross-section along the length thereof.
- a nozzle means according to claim 1 wherein said continuously converging contour is approximately hyperbolic in shape.
Landscapes
- Nozzles (AREA)
- Cleaning By Liquid Or Steam (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE7209464A SE381704B (sv) | 1972-07-19 | 1972-07-19 | Sett och anordning for generering av vetskestralpulser av hog hastighet for eroderande bearbetning |
Publications (2)
Publication Number | Publication Date |
---|---|
USB380014I5 USB380014I5 (xx) | 1975-01-28 |
US3921915A true US3921915A (en) | 1975-11-25 |
Family
ID=20276739
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US380014A Expired - Lifetime US3921915A (en) | 1972-07-19 | 1973-07-17 | Nozzle means producing a high-speed liquid jet |
Country Status (7)
Country | Link |
---|---|
US (1) | US3921915A (xx) |
JP (1) | JPS4985611A (xx) |
CA (1) | CA1027152A (xx) |
CH (1) | CH561571A5 (xx) |
DE (1) | DE2335434A1 (xx) |
SE (1) | SE381704B (xx) |
ZA (1) | ZA734928B (xx) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3343555A1 (de) * | 1982-12-06 | 1984-06-07 | Dravo Corp., 15222 Pittsburgh, Pa. | Verfahren und vorrichtung zur beschleunigung von fluessigkeitsmengen |
US4622714A (en) * | 1985-04-19 | 1986-11-18 | Sherman Industries, Inc. | Fluid stripping apparatus |
US4762277A (en) * | 1982-12-06 | 1988-08-09 | Briggs Technology Inc. | Apparatus for accelerating slugs of liquid |
US4863101A (en) * | 1982-12-06 | 1989-09-05 | Acb Technology Corporation | Accelerating slugs of liquid |
US5782414A (en) * | 1995-06-26 | 1998-07-21 | Nathenson; Richard D. | Contoured supersonic nozzle |
EP0862950A1 (en) * | 1997-03-07 | 1998-09-09 | Spraying Systems Co. | High-pressure cleaning spray nozzle |
US20050241804A1 (en) * | 2004-04-29 | 2005-11-03 | Foxconn Technology Co.,Ltd | Liquid cooling device |
US20050258562A1 (en) * | 2004-05-21 | 2005-11-24 | 3M Innovative Properties Company | Lubricated flow fiber extrusion |
US20100276506A1 (en) * | 2009-05-04 | 2010-11-04 | Pattom Matthew J | Nozzles for a fluid jet decoking tool |
US20160265557A1 (en) * | 2015-03-09 | 2016-09-15 | Dayco Ip Holdings, Llc | Devices for producing vacuum using the venturi effect |
US20160298656A1 (en) * | 2015-04-13 | 2016-10-13 | Dayco Ip Holdings, Llc | Devices for producing vacuum using the venturi effect |
US10422351B2 (en) | 2015-07-17 | 2019-09-24 | Dayco Ip Holdings, Llc | Devices for producing vacuum using the venturi effect having a plurality of subpassageways and motive exits in the motive section |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3088854A (en) * | 1960-11-08 | 1963-05-07 | Air Reduction | Methods and apparatus for cutting |
US3343794A (en) * | 1965-07-12 | 1967-09-26 | Vyacheslavovich Bogdan | Jet nozzle for obtaining high pulse dynamic pressure heads |
US3520477A (en) * | 1968-02-23 | 1970-07-14 | Exotech | Pneumatically powered water cannon |
US3647137A (en) * | 1970-10-20 | 1972-03-07 | Environment One Corp | Hydraulic chamber incorporating a jet nozzle |
-
1972
- 1972-07-19 SE SE7209464A patent/SE381704B/xx unknown
-
1973
- 1973-07-09 CH CH999573A patent/CH561571A5/xx not_active IP Right Cessation
- 1973-07-12 DE DE19732335434 patent/DE2335434A1/de active Pending
- 1973-07-17 US US380014A patent/US3921915A/en not_active Expired - Lifetime
- 1973-07-18 CA CA176,809A patent/CA1027152A/en not_active Expired
- 1973-07-19 JP JP48080557A patent/JPS4985611A/ja active Pending
- 1973-07-19 ZA ZA734928A patent/ZA734928B/xx unknown
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3088854A (en) * | 1960-11-08 | 1963-05-07 | Air Reduction | Methods and apparatus for cutting |
US3343794A (en) * | 1965-07-12 | 1967-09-26 | Vyacheslavovich Bogdan | Jet nozzle for obtaining high pulse dynamic pressure heads |
US3520477A (en) * | 1968-02-23 | 1970-07-14 | Exotech | Pneumatically powered water cannon |
US3647137A (en) * | 1970-10-20 | 1972-03-07 | Environment One Corp | Hydraulic chamber incorporating a jet nozzle |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4762277A (en) * | 1982-12-06 | 1988-08-09 | Briggs Technology Inc. | Apparatus for accelerating slugs of liquid |
US4863101A (en) * | 1982-12-06 | 1989-09-05 | Acb Technology Corporation | Accelerating slugs of liquid |
DE3343555A1 (de) * | 1982-12-06 | 1984-06-07 | Dravo Corp., 15222 Pittsburgh, Pa. | Verfahren und vorrichtung zur beschleunigung von fluessigkeitsmengen |
US4622714A (en) * | 1985-04-19 | 1986-11-18 | Sherman Industries, Inc. | Fluid stripping apparatus |
US5782414A (en) * | 1995-06-26 | 1998-07-21 | Nathenson; Richard D. | Contoured supersonic nozzle |
EP0862950A1 (en) * | 1997-03-07 | 1998-09-09 | Spraying Systems Co. | High-pressure cleaning spray nozzle |
US7143815B2 (en) * | 2004-04-29 | 2006-12-05 | Foxconn Technology Co., Ltd. | Liquid cooling device |
US20050241804A1 (en) * | 2004-04-29 | 2005-11-03 | Foxconn Technology Co.,Ltd | Liquid cooling device |
US7476352B2 (en) | 2004-05-21 | 2009-01-13 | 3M Innovative Properties Company | Lubricated flow fiber extrusion |
US20070154708A1 (en) * | 2004-05-21 | 2007-07-05 | Wilson Bruce B | Melt extruded fibers and methods of making the same |
US20050258562A1 (en) * | 2004-05-21 | 2005-11-24 | 3M Innovative Properties Company | Lubricated flow fiber extrusion |
US8481157B2 (en) | 2004-05-21 | 2013-07-09 | 3M Innovative Properties Company | Melt extruded fibers and methods of making the same |
US20100276506A1 (en) * | 2009-05-04 | 2010-11-04 | Pattom Matthew J | Nozzles for a fluid jet decoking tool |
US10077403B2 (en) * | 2009-05-04 | 2018-09-18 | Flowserve Management Company | Nozzles for a fluid jet decoking tool |
US10370594B2 (en) | 2009-05-04 | 2019-08-06 | Flowserve Management Company | Nozzles for a fluid jet decoking tool |
US20160265557A1 (en) * | 2015-03-09 | 2016-09-15 | Dayco Ip Holdings, Llc | Devices for producing vacuum using the venturi effect |
US10443627B2 (en) * | 2015-03-09 | 2019-10-15 | Dayco Ip Holdings, Llc | Vacuum producing device having a suction passageway and a discharge passageway entering through the same wall |
US20160298656A1 (en) * | 2015-04-13 | 2016-10-13 | Dayco Ip Holdings, Llc | Devices for producing vacuum using the venturi effect |
US10316864B2 (en) * | 2015-04-13 | 2019-06-11 | Dayco Ip Holdings, Llc | Devices for producing vacuum using the venturi effect |
US10422351B2 (en) | 2015-07-17 | 2019-09-24 | Dayco Ip Holdings, Llc | Devices for producing vacuum using the venturi effect having a plurality of subpassageways and motive exits in the motive section |
Also Published As
Publication number | Publication date |
---|---|
CA1027152A (en) | 1978-02-28 |
DE2335434A1 (de) | 1974-01-31 |
USB380014I5 (xx) | 1975-01-28 |
SE381704B (sv) | 1975-12-15 |
ZA734928B (en) | 1974-06-26 |
CH561571A5 (xx) | 1975-05-15 |
JPS4985611A (xx) | 1974-08-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3921915A (en) | Nozzle means producing a high-speed liquid jet | |
US3997111A (en) | Liquid jet cutting apparatus and method | |
US3343794A (en) | Jet nozzle for obtaining high pulse dynamic pressure heads | |
Rylov | On the impossibility of regular reflection of a steady-state shock wave from the axis of symmetry | |
EP1011931B1 (en) | A method and drilling apparatus to adjust the shape of a stroke pulse to be transmitted to the drill bit | |
US3561239A (en) | Apparatus for forming metals by means of jet liquid | |
Cooker et al. | Violent motion as near breaking waves meet a vertical wall | |
Laitone | The subsonic flow about a body of revolution | |
Hansson et al. | Comparison of the initial stage of vibratory and flow cavitation erosion | |
Chisnell | A note on Whitham's rule | |
JPS56101004A (en) | Vibration damper for turbine blade | |
Gaur et al. | Comparative Viscous Flow Analysis for Rocket Engine Convergent-Divergent Nozzle for Distinct Geometric Parameters | |
Kozlov et al. | Possibility of Forming Periodic Pulsed Jets Using Cavitation Self-Oscillation Modes | |
Salenko et al. | Improvement of the fracture resistance of calibration tubes of the hydroabrasive equipment | |
Ivanov | Simple hydrodynamic model of atmospheric breakup of hypervelocity projectiles | |
Dawson | Axial rarefaction wave in a radially expanding tube of pressurized gas | |
DE3731234C1 (de) | Hochdruckwasserstrahlgeraet mit pulsierendem Wasserstrahl | |
GB1513736A (en) | Jet assemblies | |
FR2440779A2 (fr) | Concasseur a percussion | |
Atanov et al. | Peculiarities of the Power Hydrocannon Operation | |
EREMIN et al. | Total shock-tube working time in the investigation of the discharge through holes in the end face | |
GB1149353A (en) | Excavation machines particularly for use in mines | |
Atanov | Powder impulsive water jetter | |
ARUTYUNYAN | Interaction of a shock wave with a wedge(Numerical analysis of two dimensional shock wave resulting from mobile wedge moving with supersonic velocity and specific angle of attack into detonation wave) | |
Hawkings | Transonic fan noise |