US3066875A - Adjustable liquid ejector nozzle - Google Patents

Adjustable liquid ejector nozzle Download PDF

Info

Publication number
US3066875A
US3066875A US761243A US76124358A US3066875A US 3066875 A US3066875 A US 3066875A US 761243 A US761243 A US 761243A US 76124358 A US76124358 A US 76124358A US 3066875 A US3066875 A US 3066875A
Authority
US
United States
Prior art keywords
nozzle
liquid
ejector
passage
air
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
Application number
US761243A
Inventor
Obidniak Louis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US761243A priority Critical patent/US3066875A/en
Application granted granted Critical
Publication of US3066875A publication Critical patent/US3066875A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q11/00Accessories fitted to machine tools for keeping tools or parts of the machine in good working condition or for cooling work; Safety devices specially combined with or arranged in, or specially adapted for use in connection with, machine tools
    • B23Q11/10Arrangements for cooling or lubricating tools or work
    • B23Q11/1084Arrangements for cooling or lubricating tools or work specially adapted for being fitted to different kinds of machines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02Spray pistols; Apparatus for discharge
    • B05B7/12Spray pistols; Apparatus for discharge designed to control volume of flow, e.g. with adjustable passages

Definitions

  • the present invention relates to improvements in the construction of liquid ejector nozzles, and more particularly to improvements in nozzles of this type adapted to dispense a liquid spray by suction induced flow as opposed to direct pressure spraying of a pressurized liquid.
  • the pressurized gas is .directed in a high velocity ow past the open end of a liquid delivery tube so as to create the aspirating effect drawing the liquid from the tube, and by the mixing of the liquid with the air creating an atomizing effect as it is ejected from the nozzle.
  • the air delivery or primary liow tube is disposed axially of the liquid delivery or secondary flow tube with a portion of the outer tube in advance of the inner primary ow tube serving as a mixing chamber.
  • the high velocity stream of pressurized air since it is disposed along the axis of the nozzle, is in the axial centre of the mixing zone and tends to form a cone extending through the nozzle to which the liquid drawn from the surrounding liquid tube engages only by surface Contact.
  • Adjustment of the degree of atomization is generally achieved by varying the size of the mixing chamber so as to theoretically vary the quantity of liquid withdrawn while maintaining the primary or pressurized air ow constant, This is not too satisfactory and while it can be improved by the addition of a further control, for example a separate valve, on the primary ilow this of course complicates adjustment and adds to the cost of manufacture.
  • the present invention recognizes these disadvantages and aims to provide an improved ejector nozzle construction wherein the liquid to be dispensed is forced to pass directly into the high velocity primary air iiow and accordingly is completely mixed with the air.
  • the present nozzle construction includes means whereby by a single adjustment the discharge of liquid-air mixture can be controlled from the finest mist to the heaviest spray and further permits reversal of a portion of the primary air ilow through the liquid delivery tube for cleaning purposes.
  • an ejector nozzle assembly including an ejector body having at least. a forward portion of cylindrical formation and a liquid passage extending through the body with a terminal portion of the ejector body surrounding the liquid passage being of a reduced diameter relative to the remainder of the body and formed to constitute a conical liquid ejector tip.
  • a hollow outer nozzle is adjustably mounted on the ejector body and includes a tapering conicallyshaped forward portion which iits over and surrounds the liquid ejector tip in spaced relationship to provide an air chamber between the exterior of the tip and the interior of the nozzle. At least one recess is provided through the ejector body into the nozzle air chamber and an axial recess is provided in the forward end of the outer nozzle portion which is disposed in axial alignment with the ejector body liquid passage.
  • the interior of the nozzle portion surrounding the ejector tip is formed at an angle slightly greater than that of the exterior of the ejector tip so as to provide therebetween a conical air discharge passage converging from the air chamber 'to the outer nozzle discharge passage.
  • the outer nozzle as previously mentioned, is adjustably mounted on the ejector body, preferably by threaded engagement, so that by adjustment of the outer nozzle in the axial direction relative to the ejector body the dimensions of the conical air discharge passage can be varied from a fully open position providing a discharge capacity greater than that of the nozzle outlet passage to a fully closed position sealing off the air discharge passage in advance of the nozzle outlet passage.
  • FIGURE l is a View in side elevation of an ejector nozzle assembly constructed in accordance with the inventicn as it would appear when utilized in combination with a supply container of liquid, for example, a machine tool coolant.
  • FGURE 2 is a top plan view of the ejector nozzle construction shown in FIGURE l.
  • FIGURE 3 is an interior cross-sectional view of the construction shown in FlGURE 2 along the line 3-3.
  • FEGURE 4 is an enlarged detail view, partially in cross-section, to illustrate the connections of the liquid and air delivery conduit, leading from the supply tank shown to the ejector nozzle.
  • FIGURE 5 is a cross-sectional View of the construction shown in FIGURE l along the line 5--5.
  • FIGURE 6 is an enlarged detail View, in section, of the forward portion of the ejector nozzle construction of the invention to show the variance in angle between the interior walls of the outer nozzle and the exterior of the ejector tip more clearly.
  • an ejector nozzle in accordance with the invention consists essentially of a main body lli having a forward threaded extension l2 and a central recess lid adapted to receive a generally cylindrical ejector body 16.
  • the ejector body te is shaped to provide inwardly extending annular recesses 255, 2 and a forward por* tion 22 of reduced diameter and conically tapering formation.
  • the body portions 23, 2.5 of maximum diameter are provided with annular grooves adapted to accommodate seating rings 26 and the tail end ll of the body ld is threaded, as shown most clearly in FlGURE 3, to threadably engage with a corresponding tapped opening l@ provided in the ibase of the recess lid.
  • the ejector body ll@ is bored axially to provide a liquid conducting passage 3% which is reduced in diameter, as indicated at 32, at the body forward portion 22 providing a restricted passage adapted to increase the velocity and measure the quantity of liquid drawn therethrough.
  • the main body titl is bored transversely of the axis of the recess i4- to provide ports 3d, 36 leading into the annular recesses Ztl, 2i for the entrance of pressurized air and inducted liquid respec tively. These are supplied through conduits di), 42 through ttings nl, d3, as will be described in more detail later.
  • A, further trans-axial recess i6 extends through the lower portion of the annular recess 2l. into the liquid passage to complete the communication from the conduit d2 while the ejector body portion 23 is provided with .borings dit parallel to the main passage 3l? and leading from annular recess Zt? to the front face of the body i6 to complete the communication from the conduit ad.
  • the main controlling element of the assembly is a hollow outer nozzle 6@ shaped so as to have a rst cylindrical portion 62 adapted to fit over and threadably engage the mainbody extension l2, and a tapering conical forward portion 6d adapted to tit over the ejector body tip 22 in spaced apart relationship forming therebetween a conically-shaped air passage ed, as shown most clearly in FlGURE 6.
  • the nozzle portion is axially recessed to provide an outlet passage in concentric axial alignment with the ejector body passage 32, Titi.
  • the principle of this rarrangement is as follows. rThe pressurized lluid constituting the primary dow, for example compressed air deliveredthrough the conduit dit, enters the ejector body recess Ztl, passes through the ejector body and enters the conical air passage 66. lt should be noted that the exterior of the ejector tip is formed at converging angles B while the interior walls of the nozzle portion ed are formed at a greater angle C, giving the air passage 66 the form of a tapered hollow cone with gradually converging side walls.
  • This double-tapered or cone within a cone formation of the air passage de creates the best possible discharging conditions for the primary flow and makes the unique control alorded by the present invention possible.
  • the primary flow of air passes through the passage Vto the control section D and from the section D, having acquired high velocity, out of the nozzle outlet passage to atmosphere. Accordingly, as previously explained, the form of the primary flow is a hollow cone with its apex A aligned witn the axial centre line of the Vnozzle outlet passage 63.
  • the dimensions of the air passage at the sec-tion D can be increased or decreased.
  • the axial movement of the nozzle c@ does not in any way affect the relationship of the angles B and C of the nozzle and Vejector so that discharging conditions will remain unchanged. Accordingly, by displacement of the nozzle dit, with a primary iiow of constant pressure, varying quantities of primary flow will be achieved and varying degrees of suction can be created and by such variation the mass of ejected liquid will automatically change in relative proportion.
  • FIG- URE l A practical example of one preferred embodiment of the ejector nozzle of the invention is shown in FIG- URE l. ln this arrangement the conduits dd, 4Z extend through a flexible metal hose 7d to a connection with a liquid coolant supply tank 72. and air supply line 46a, through supporting block 36.
  • the flexible metal hose 70 protects the conduits dit, 42 against physical damage and at the same time provides a flexible support for the ejector nozzle.
  • the ejector nozzle assembly is connected to the end of the hose 7d by a split casing 76 having end flanges engaging the assembly body lll and an end sleeve '78 provided on the hose 79.
  • the por-tions of the casing 76 are held together by a screw 79, as shown in FIGURE 5.
  • the other en d of the hose 7i) is ⁇ similarly attached to a supporting block d@ mounted on a C-type clamp 8l suitable for attachment to a machine frame, for example.
  • the block 3d is bored to provide a liquid conducting passage 9d and an air conducting passage 92 and the terminal ends of the conduits dil, 42 are connected to these passages by suitable fittings, as previously described.
  • An extension conduit i241 is connected into the liquid conducting passage 92 and extends within the coolant tank 72, as indicated in FlGURE l.
  • An air supply conduit Lide is also connected into the passage @il from a suitable source of compressed air.
  • the action of the primary air tlow delivered through the conduit ed creates an aspirating effect on the conduit 42 drawing liquid up through the conduit dita from the supply tank 72 and discharging it in atomized spray of any desired liquid content.
  • This is a furt er advantageous feature in the present construction /hich is particularly useful when the assembly is utilized for the spraying orf machine tool coolant as shown, or similar liquids.
  • the total cross-section of the air delivery borings 49 in the ejector body portion 23 is greater than the cross-section of the nozzle outlet discharge passage 655.
  • rIltis reverse flushing serves two purposes: (a) the flushing of the ejector body and conduit d2, cleans the coolant tube and prevents possible clogging; and (b) the blowing in of air under pressure through the coolant stirs it up and tends to homogenize the suspension. All of the described effects are achieved easily and simply by the rotation of the nozzle 6u relative to the main body lll without the necessity of providing supplementary valves or controls.
  • An aspirator nozzle comprising an elongated body having an externally threaded extension at one end and an axial blind recess opening into said one end, said body including a pair of inlet ports spaced along said axial recess for respective connection to a source of liquid and pressurized fluid, an ejector body extending axially within said axial recess and terminally secured at one end at the end of said blind recess opposite said threaded extension, said ejector body including longitudinally spaced annular grooves each respectively communicating with one of said inlet ports, said ejector body including an axial liquidreceiving passage communicating with one of said annular grooves for receiving liquid therefrom, said axial liquidreceiving passage terminating in a reduced cross-section at the terminal end thereof, said ejector body including longitudinally spaced seal means circumposed about said body and isolating said annular grooves within'said axial recess, said ejector body terminating in a frusto-conical tip portion,

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Nozzles (AREA)

Description

Dec. 4, 1962 L. OBIDNIAK 3,066,875 ADJUSTABLE LIQUID EJEcToR NozzLE United States Patent free Patented Dec.. .li, i352 3,t6,75 ADJUSTABLE LlQUiD EEMCTR NQEZLE Louis Gbidniatr., 7435 de ilpee Ave., Montreal, Quebec, Canada Filed Sept. l5, 195., der. No. dlfl l Claim. (tCi. Z39-4TH The present invention relates to improvements in the construction of liquid ejector nozzles, and more particularly to improvements in nozzles of this type adapted to dispense a liquid spray by suction induced flow as opposed to direct pressure spraying of a pressurized liquid.
While the use of a stream of pressurized gas, cornpressed air for example, as a means of creating an aspirating eifect in an ejector nozzle is well ltnown in general, an eifective simple way or" controlling the flow ot gas and/or liquid has not been provided in the prior art ejector nozzle constructions known to the applicant.
Usually, the pressurized gas is .directed in a high velocity ow past the open end of a liquid delivery tube so as to create the aspirating effect drawing the liquid from the tube, and by the mixing of the liquid with the air creating an atomizing effect as it is ejected from the nozzle. In the most common form of such nozzle arrangements the air delivery or primary liow tube is disposed axially of the liquid delivery or secondary flow tube with a portion of the outer tube in advance of the inner primary ow tube serving as a mixing chamber. In this type of nozzle, the high velocity stream of pressurized air, since it is disposed along the axis of the nozzle, is in the axial centre of the mixing zone and tends to form a cone extending through the nozzle to which the liquid drawn from the surrounding liquid tube engages only by surface Contact. Accordingly, the ow of liquid cannot possibly attain the speed of the pressurized gas stream and therefore complete and eflicient mixing is not achieved, Adjustment of the degree of atomization is generally achieved by varying the size of the mixing chamber so as to theoretically vary the quantity of liquid withdrawn while maintaining the primary or pressurized air ow constant, This is not too satisfactory and while it can be improved by the addition of a further control, for example a separate valve, on the primary ilow this of course complicates adjustment and adds to the cost of manufacture.
The present invention recognizes these disadvantages and aims to provide an improved ejector nozzle construction wherein the liquid to be dispensed is forced to pass directly into the high velocity primary air iiow and accordingly is completely mixed with the air. The present nozzle construction includes means whereby by a single adjustment the discharge of liquid-air mixture can be controlled from the finest mist to the heaviest spray and further permits reversal of a portion of the primary air ilow through the liquid delivery tube for cleaning purposes.
Accordingly, the invention is embodied in an ejector nozzle assembly including an ejector body having at least. a forward portion of cylindrical formation and a liquid passage extending through the body with a terminal portion of the ejector body surrounding the liquid passage being of a reduced diameter relative to the remainder of the body and formed to constitute a conical liquid ejector tip. A hollow outer nozzle is adjustably mounted on the ejector body and includes a tapering conicallyshaped forward portion which iits over and surrounds the liquid ejector tip in spaced relationship to provide an air chamber between the exterior of the tip and the interior of the nozzle. At least one recess is provided through the ejector body into the nozzle air chamber and an axial recess is provided in the forward end of the outer nozzle portion which is disposed in axial alignment with the ejector body liquid passage.
In accordance with the present invention the interior of the nozzle portion surrounding the ejector tip is formed at an angle slightly greater than that of the exterior of the ejector tip so as to provide therebetween a conical air discharge passage converging from the air chamber 'to the outer nozzle discharge passage. The outer nozzle, as previously mentioned, is adjustably mounted on the ejector body, preferably by threaded engagement, so that by adjustment of the outer nozzle in the axial direction relative to the ejector body the dimensions of the conical air discharge passage can be varied from a fully open position providing a discharge capacity greater than that of the nozzle outlet passage to a fully closed position sealing off the air discharge passage in advance of the nozzle outlet passage.
Having tnus generally described the nature of the invention, particular reference will be made to the accompanying drawing, showing by way of illustration a preferred embodiment, and in which:
FIGURE l is a View in side elevation of an ejector nozzle assembly constructed in accordance with the inventicn as it would appear when utilized in combination with a supply container of liquid, for example, a machine tool coolant.
FGURE 2 is a top plan view of the ejector nozzle construction shown in FIGURE l.
FIGURE 3 is an interior cross-sectional view of the construction shown in FlGURE 2 along the line 3-3.
FEGURE 4 is an enlarged detail view, partially in cross-section, to illustrate the connections of the liquid and air delivery conduit, leading from the supply tank shown to the ejector nozzle.
FIGURE 5 is a cross-sectional View of the construction shown in FIGURE l along the line 5--5.
FIGURE 6 is an enlarged detail View, in section, of the forward portion of the ejector nozzle construction of the invention to show the variance in angle between the interior walls of the outer nozzle and the exterior of the ejector tip more clearly.
With particular reference to FIGURES 2, 3, 5 and 6 of the drawings, a preferred construction of an ejector nozzle in accordance with the invention consists essentially of a main body lli having a forward threaded extension l2 and a central recess lid adapted to receive a generally cylindrical ejector body 16.
The ejector body te is shaped to provide inwardly extending annular recesses 255, 2 and a forward por* tion 22 of reduced diameter and conically tapering formation. The body portions 23, 2.5 of maximum diameter are provided with annular grooves adapted to accommodate seating rings 26 and the tail end ll of the body ld is threaded, as shown most clearly in FlGURE 3, to threadably engage with a corresponding tapped opening l@ provided in the ibase of the recess lid. rthe ejector body ll@ is bored axially to provide a liquid conducting passage 3% which is reduced in diameter, as indicated at 32, at the body forward portion 22 providing a restricted passage adapted to increase the velocity and measure the quantity of liquid drawn therethrough. the `construction shown .the main body titl is bored transversely of the axis of the recess i4- to provide ports 3d, 36 leading into the annular recesses Ztl, 2i for the entrance of pressurized air and inducted liquid respec tively. These are supplied through conduits di), 42 through ttings nl, d3, as will be described in more detail later. A, further trans-axial recess i6 extends through the lower portion of the annular recess 2l. into the liquid passage to complete the communication from the conduit d2 while the ejector body portion 23 is provided with .borings dit parallel to the main passage 3l? and leading from annular recess Zt? to the front face of the body i6 to complete the communication from the conduit ad.
The main controlling element of the assembly is a hollow outer nozzle 6@ shaped so as to have a rst cylindrical portion 62 adapted to fit over and threadably engage the mainbody extension l2, and a tapering conical forward portion 6d adapted to tit over the ejector body tip 22 in spaced apart relationship forming therebetween a conically-shaped air passage ed, as shown most clearly in FlGURE 6. The nozzle portion is axially recessed to provide an outlet passage in concentric axial alignment with the ejector body passage 32, Titi.
With reference to FIGURE 6, the principle of this rarrangement is as follows. rThe pressurized lluid constituting the primary dow, for example compressed air deliveredthrough the conduit dit, enters the ejector body recess Ztl, passes through the ejector body and enters the conical air passage 66. lt should be noted that the exterior of the ejector tip is formed at converging angles B while the interior walls of the nozzle portion ed are formed at a greater angle C, giving the air passage 66 the form of a tapered hollow cone with gradually converging side walls. This double-tapered or cone within a cone formation of the air passage de creates the best possible discharging conditions for the primary flow and makes the unique control alorded by the present invention possible. To continue, the primary flow of air passes through the passage Vto the control section D and from the section D, having acquired high velocity, out of the nozzle outlet passage to atmosphere. Accordingly, as previously explained, the form of the primary flow is a hollow cone with its apex A aligned witn the axial centre line of the Vnozzle outlet passage 63. 'l'his form of discharge creates the desired maximum aspirating action and completely surrounds the conical ejector tip 22 causing liquid to be sucked up through the conduit i2 into the liquid passages and from the passage 32 into and through the point A of the primary flow. lt will be appreciated that every drop of the liquid in the secondary flow is pulled into the primary ilow and intimately mixed in the outlet passage @d prior to discharge. By this arrangement the two flows change their speed in the outlet passage ed and acquire some intermediate speed which is a function of the two masses. 'Since no part of the secondary or induced flow can escape the mixing in the outlet passage without being affected by the primary discharging flow, an ideal condi- 'tion is achieved in which the primary and secondary flows 'are physically forced to exchange their speeds.
As the nozzle titl can be adjusted axially relative to the ejector tip 22 and parallel to the centre line of the nozzle assembly, the dimensions of the air passage at the sec-tion D can be increased or decreased. The axial movement of the nozzle c@ does not in any way affect the relationship of the angles B and C of the nozzle and Vejector so that discharging conditions will remain unchanged. Accordingly, by displacement of the nozzle dit, with a primary iiow of constant pressure, varying quantities of primary flow will be achieved and varying degrees of suction can be created and by such variation the mass of ejected liquid will automatically change in relative proportion.
For example, by retraction of the nozzle 6d to a point Where the end of the ejector tip 22 is in actual contact with the tapering inner walls of the outer nozzle it will act as a valve and completely shut off the primary flow. In the absence of primary dow, of course, no suc-tion is created and there is no discharge of secondary flow or liquid. Extension of the nozzle ou from this position will gradually increase the dimensions of the conical air passage 66 at section D permitting liow of primary air and consequent aspiration and discharge of liquid.
A practical example of one preferred embodiment of the ejector nozzle of the invention is shown in FIG- URE l. ln this arrangement the conduits dd, 4Z extend through a flexible metal hose 7d to a connection with a liquid coolant supply tank 72. and air supply line 46a, through supporting block 36. The flexible metal hose 70 protects the conduits dit, 42 against physical damage and at the same time provides a flexible support for the ejector nozzle.
As is shown most clearly in FIGURES 3 and 5, the ejector nozzle assembly is connected to the end of the hose 7d by a split casing 76 having end flanges engaging the assembly body lll and an end sleeve '78 provided on the hose 79. The por-tions of the casing 76 are held together by a screw 79, as shown in FIGURE 5. The other en d of the hose 7i) is `similarly attached to a supporting block d@ mounted on a C-type clamp 8l suitable for attachment to a machine frame, for example. The block 3d is bored to provide a liquid conducting passage 9d and an air conducting passage 92 and the terminal ends of the conduits dil, 42 are connected to these passages by suitable fittings, as previously described. An extension conduit i241 is connected into the liquid conducting passage 92 and extends within the coolant tank 72, as indicated in FlGURE l. An air supply conduit Lide is also connected into the passage @il from a suitable source of compressed air.
As previously described, the action of the primary air tlow delivered through the conduit ed creates an aspirating effect on the conduit 42 drawing liquid up through the conduit dita from the supply tank 72 and discharging it in atomized spray of any desired liquid content. This is a furt er advantageous feature in the present construction /hich is particularly useful when the assembly is utilized for the spraying orf machine tool coolant as shown, or similar liquids. The total cross-section of the air delivery borings 49 in the ejector body portion 23 is greater than the cross-section of the nozzle outlet discharge passage 655. As long as the cross-section D of the conical air discharge passage is adjusted so as Vto 'oe smaller than that of the nozzle outlet passage 63 a pressure drop will occur and create the desired aspirating edect. However, if the nozzle 69 is advanced to the point where the section D is greater than that of the nozzle passage 63 there will b e no pressure drop or expansion in the section D and the primary iiow of air will be forced back through the passages 32, 353 of the ejector body 22, through the conduit 42 and into the supply tank 72. rIltis reverse flushing serves two purposes: (a) the flushing of the ejector body and conduit d2, cleans the coolant tube and prevents possible clogging; and (b) the blowing in of air under pressure through the coolant stirs it up and tends to homogenize the suspension. All of the described effects are achieved easily and simply by the rotation of the nozzle 6u relative to the main body lll without the necessity of providing supplementary valves or controls.
l claim:
An aspirator nozzle comprising an elongated body having an externally threaded extension at one end and an axial blind recess opening into said one end, said body including a pair of inlet ports spaced along said axial recess for respective connection to a source of liquid and pressurized fluid, an ejector body extending axially within said axial recess and terminally secured at one end at the end of said blind recess opposite said threaded extension, said ejector body including longitudinally spaced annular grooves each respectively communicating with one of said inlet ports, said ejector body including an axial liquidreceiving passage communicating with one of said annular grooves for receiving liquid therefrom, said axial liquidreceiving passage terminating in a reduced cross-section at the terminal end thereof, said ejector body including longitudinally spaced seal means circumposed about said body and isolating said annular grooves within'said axial recess, said ejector body terminating in a frusto-conical tip portion, having a base disposed at an annular face, said ejector body including longitudinally extending liuid pressure passage means opening into said annular face and communicating with said other annular groove, and a tubular nozzle element threadedly engaged on said threaded extension for free and ready manual longitudinal adjustment thereon, seal means interposed between said nozzle element and said ejector body, said nozzle element including an outlet passage in coaxial, spaced alignment with said reduced cross-section passage portion of said ejector body, said nozzle element including a frustoconical internal chamber circumposed about said frustoconical terminal tip portion of said ejector body, a projection of the frusto-conical chamber terminating at an imaginary apex intermediately of said outlet passage and at a greater angle than a projection of the outer surface of said frusto-conical tip portion, said nozzle element being retractable on said body whereby the terminal end of said ejector body will engage said internal chamber wall and no pressurized uid will flow to cause aspiration of liquid from the axial passage of said ejector body, and said noz- 5 zle element being positionable in spaced relation from said ejector body tip portion a sufficient extent to cause a back pressure in said ejector body axial passage to keep the axial passage free of foreign matter and stir the liquid with which the axial passage normally communicates.
References Cited in the file of this patent UNITED STATES PATENTS 817,819 Walkup Apr. 17, 1906 1,069,437 Lambeth Aug. 5, 1913 1,098,429 Coleman June 2, 1914 1,302,827 Miller May 6, 1919 1,415,383 Nettgens May 9, 1922 1,597,033 Gibbons Aug. 24, 1926 2,259,215 Scheurer Oct. 14, 1941 FOREIGN PATENTS 730,806 Great Britain June 1, 1955
US761243A 1958-09-15 1958-09-15 Adjustable liquid ejector nozzle Expired - Lifetime US3066875A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US761243A US3066875A (en) 1958-09-15 1958-09-15 Adjustable liquid ejector nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US761243A US3066875A (en) 1958-09-15 1958-09-15 Adjustable liquid ejector nozzle

Publications (1)

Publication Number Publication Date
US3066875A true US3066875A (en) 1962-12-04

Family

ID=25061621

Family Applications (1)

Application Number Title Priority Date Filing Date
US761243A Expired - Lifetime US3066875A (en) 1958-09-15 1958-09-15 Adjustable liquid ejector nozzle

Country Status (1)

Country Link
US (1) US3066875A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228613A (en) * 1964-07-10 1966-01-11 Munsey S Goldstein Spraying attachment with base
US3331537A (en) * 1965-08-13 1967-07-18 Elmer M Benedict Ring type finger supported defensive spray dispenser
US3398609A (en) * 1966-12-22 1968-08-27 Thomas C Wilson Inc Power tool
US4314671A (en) * 1978-10-10 1982-02-09 Briar Jack E Pressure jet spray apparatus
WO1985003853A1 (en) * 1984-03-02 1985-09-12 New Regina Corporation Machine for cleaning surfaces such as carpets, floors and the like
US4712740A (en) * 1984-03-02 1987-12-15 The Regina Co., Inc. Venturi spray nozzle for a cleaning device

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US817819A (en) * 1905-08-18 1906-04-17 Liberty Walkup Air-brush.
US1069437A (en) * 1912-06-04 1913-08-05 Edgar V Lambeth Lubricator.
US1098429A (en) * 1914-06-02 Frederick A Coleman Oil-burner.
US1302827A (en) * 1919-02-06 1919-05-06 Tate Jones & Company Inc Hydrocarbon-burner.
US1415383A (en) * 1922-02-03 1922-05-09 Eduard Straub Keller Burner for gaseous and liquid fuels
US1597033A (en) * 1925-04-17 1926-08-24 James W Gibbons Spraying apparatus
US2259215A (en) * 1940-02-26 1941-10-14 J W Mortell Company Spray gun
GB730806A (en) * 1952-11-25 1955-06-01 Peter Edward Bromley Martin Improvements in or relating to the application of rubber compositions to structures

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1098429A (en) * 1914-06-02 Frederick A Coleman Oil-burner.
US817819A (en) * 1905-08-18 1906-04-17 Liberty Walkup Air-brush.
US1069437A (en) * 1912-06-04 1913-08-05 Edgar V Lambeth Lubricator.
US1302827A (en) * 1919-02-06 1919-05-06 Tate Jones & Company Inc Hydrocarbon-burner.
US1415383A (en) * 1922-02-03 1922-05-09 Eduard Straub Keller Burner for gaseous and liquid fuels
US1597033A (en) * 1925-04-17 1926-08-24 James W Gibbons Spraying apparatus
US2259215A (en) * 1940-02-26 1941-10-14 J W Mortell Company Spray gun
GB730806A (en) * 1952-11-25 1955-06-01 Peter Edward Bromley Martin Improvements in or relating to the application of rubber compositions to structures

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228613A (en) * 1964-07-10 1966-01-11 Munsey S Goldstein Spraying attachment with base
US3331537A (en) * 1965-08-13 1967-07-18 Elmer M Benedict Ring type finger supported defensive spray dispenser
US3398609A (en) * 1966-12-22 1968-08-27 Thomas C Wilson Inc Power tool
US4314671A (en) * 1978-10-10 1982-02-09 Briar Jack E Pressure jet spray apparatus
WO1985003853A1 (en) * 1984-03-02 1985-09-12 New Regina Corporation Machine for cleaning surfaces such as carpets, floors and the like
US4712740A (en) * 1984-03-02 1987-12-15 The Regina Co., Inc. Venturi spray nozzle for a cleaning device

Similar Documents

Publication Publication Date Title
US3764074A (en) Shower head and liquid agent dispensing attachment
US5054249A (en) Method and apparatus for liquid-abrasive blast cleaning
US5018670A (en) Cutting head for water jet cutting machine
US3735778A (en) Driving of fluids
US2513081A (en) Multichromatic spraying apparatus
US4123005A (en) Acoustical texture applicator
AU648959B2 (en) Spray system
US4951876A (en) Spray tip for a caulking tube
US4948054A (en) Pneumatic drywall texture bazooka
US3066875A (en) Adjustable liquid ejector nozzle
US4314671A (en) Pressure jet spray apparatus
US5390854A (en) Coolant spray system
US1988017A (en) Spraying apparatus
US2405854A (en) Gun for blasting and spraying
US2851213A (en) Compressed-air operated vacuum cleaners
US2801880A (en) Hopper spray gun
US3879140A (en) Painting apparatus
US2188366A (en) Spray apparatus
US3042315A (en) Air and liquid spray gun
EP0137765B1 (en) Spraying gun
US2275691A (en) Apparatus for atomizing liquids
US2295661A (en) Apparatus for spraying liquid
US3759449A (en) Device for producing coolant mist
US2528927A (en) Spraying device for liquids
US2550888A (en) Spray gun