US3799195A - Device for controlling a mixture of two gases - Google Patents

Device for controlling a mixture of two gases Download PDF

Info

Publication number
US3799195A
US3799195A US00227492A US22749272A US3799195A US 3799195 A US3799195 A US 3799195A US 00227492 A US00227492 A US 00227492A US 22749272 A US22749272 A US 22749272A US 3799195 A US3799195 A US 3799195A
Authority
US
United States
Prior art keywords
nozzle
ring
sleeve
nozzles
axis
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
US00227492A
Inventor
F Hermans
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.)
Le Four Industriel Belge SA
Original Assignee
Le Four Industriel Belge SA
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 Le Four Industriel Belge SA filed Critical Le Four Industriel Belge SA
Application granted granted Critical
Publication of US3799195A publication Critical patent/US3799195A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/62Mixing devices; Mixing tubes
    • F23D14/64Mixing devices; Mixing tubes with injectors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F23/00Mixing according to the phases to be mixed, e.g. dispersing or emulsifying
    • B01F23/10Mixing gases with gases
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F25/00Flow mixers; Mixers for falling materials, e.g. solid particles
    • B01F25/30Injector mixers
    • B01F25/31Injector mixers in conduits or tubes through which the main component flows
    • B01F25/312Injector mixers in conduits or tubes through which the main component flows with Venturi elements; Details thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F25/00Flow mixers; Mixers for falling materials, e.g. solid particles
    • B01F25/30Injector mixers
    • B01F25/31Injector mixers in conduits or tubes through which the main component flows
    • B01F25/312Injector mixers in conduits or tubes through which the main component flows with Venturi elements; Details thereof
    • B01F25/3124Injector mixers in conduits or tubes through which the main component flows with Venturi elements; Details thereof characterised by the place of introduction of the main flow
    • B01F25/31242Injector mixers in conduits or tubes through which the main component flows with Venturi elements; Details thereof characterised by the place of introduction of the main flow the main flow being injected in the central area of the venturi, creating an aspiration in the circumferential part of the conduit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/60Devices for simultaneous control of gas and combustion air
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01FMIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F25/00Flow mixers; Mixers for falling materials, e.g. solid particles
    • B01F25/30Injector mixers
    • B01F25/31Injector mixers in conduits or tubes through which the main component flows
    • B01F25/312Injector mixers in conduits or tubes through which the main component flows with Venturi elements; Details thereof
    • B01F25/3125Injector mixers in conduits or tubes through which the main component flows with Venturi elements; Details thereof characteristics of the Venturi parts
    • B01F25/31252Nozzles
    • B01F25/312521Adjustable Venturi nozzle
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/2496Self-proportioning or correlating systems
    • Y10T137/2499Mixture condition maintaining or sensing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8158With indicator, register, recorder, alarm or inspection means
    • Y10T137/8225Position or extent of motion indicator
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/87571Multiple inlet with single outlet
    • Y10T137/87587Combining by aspiration
    • Y10T137/87611Flow control by varying position of a fluid inlet relative to entrainment chamber

Definitions

  • ABSTRACT nozzle and entering freely in the ring, so as to permit the said nozzle to move inside the device by making the ring rotate around its axis with reference to said sleeve.
  • the present invention relates to a device for controlling a mixture of two gases, such as a comburent gas and a combustible gas, comprising a first nozzle with a converging portion, such nozzle communicating with a first adduction pipe for one of the said components of the mixture and in the rear of which is a second nozzle coaxial with the first one, the second nozzle having a diverging portion, at least the entry of the latter being of larger internal circular cross-section than the external circular cross-section of the first nozzle, a chamber wherein opens a second adduction pipe for the other component of the said mixture, enclosing the outlet end of the first nozzle and communicating with the entry of the second nozzle, means being provided to vary along the common axis of the two nozzles, the relative position of the latter.
  • two gases such as a comburent gas and a combustible gas
  • the aim of the invention is to provide an improved device of the said type enabling to achieve a strictly constant ratio, upstream of the equipment to be supplied, such as heating apparatus, between the two components of the mixture and this for flows of this gas mixture varying between fairly large limits.
  • the means provided to vary, along the common axis of the twonozzles, the relative position of the latter comprise at least one ring, provided with an internal screw thread, mounted in movable manner on a stationary sleeve enclosing one of the nozzles, the nozzle located inside the sleeve being fitted in such a manner as to be able to slide inside the latter along the axis thereof; at least one slot, parallel to the said axis, passing right through the portion of the wall of the said sleeve covered by the said ring; a driving member for such nozzle co-operating with such slot and being secured to the inner wall of the nozzle and engaging freely the inner face of the ring covering the slot, so as to permit the said nozzle to move inside the device by making the ring rotate around its axis with reference to the sleeve.
  • the sleeve comprises atleast two slots diametrically opposite one another, parallel to the axis of the nozzle fitted inside the sleeve, the said driving m'ember for such nozzle co-operating with each one of the said slots.
  • the first nozzle is assembled in the said sleeve, the second nozzle being stationary with reference to the latter.
  • a flange is provided at the outlet of at least one of the nozzles, so as to permit establishing close to such outlet, a stationary gas film.
  • F 1G. 1 shows diagrammatically a longitudinal crosssection partially broken away, of a particular embodiment of the invention.
  • FIG. 2 shows on a large scale a detail of the device shown in FIG. 1.
  • FIG. 3 is an elevational view, partially broken away, of a detail of a modified form of the device shown in FIG. 1.
  • the device according to the invention comprises a first nozzle 1, with a converging portion 2 and communicating with an adduction pipe 3 for a first gas, and a second nozzle 4 coaxial with the first one and mounted downstream of the latter.
  • the second nozzle 4 has a diverging portion, at least the entry 6 of the latter being of larger internal circular cross-section than the external circular cross-section of the outlet 7 of the first nozzle 1, so as to permit engaging such outlet 7 in the entry 6 while maintaining in between them an annular space 8 for the passage of a gas originating from a chamber 9 enclosing the outlet end of the first nozzle 1 and communicating with the entry 6 of the second nozzle 4.
  • a second adduction pipe 10 for a second gas opens into the said chamber 9.
  • a ring 11 with an internal helical thread 17 is freely threaded on a stationary sleeve 12 enclosing the nozzle 1, the latter being fitted in such a manner as to be able to translate inside the sleeve along the common axis 13.
  • a driving member, provided by a stem 16 cooperates with each one of these slots 14 and 15. This member is secured by one of its ends to the outside wall of the nozzle and engages freely with its other end an annular slot 35 provided in the inner face of the ring 11 and concentric with the latter, these two stems 16 being also diametrically opposite one another.
  • the ring 11 is knurled on its outside face and provided with a graduation 18 showing the ratio of the two gases in terms of the position of this ring of the sleeve 12.
  • a secondary ring 19 is provided on the sleeve 12, partially beneath ring 11 and which carries on its outside face, parallel to its axis, a graduated scale 36.
  • Ring 11 may be rotated around its axis in both directions.
  • the graduation of the scale 36 in such that for one revolution of the ring 11, the latter moves in the axial direction by one unit of the graduation, so that the rim of the ring 11 located on the side of the ring 19 shall coincide with the line mark according to the graduation 36.
  • the two graduated rings 11 and 19 thus determine a vernier permitting measurement, in a very accurate manner, of the axial movement of the nozzle 1 and, consequently, also the ratio of the two gases.
  • the ring 19 may, just like the ring 11, rotate around its axis so as to enable a movement of the graduated scale 36 simultaneously with the graduations 18 and thus ensure the accessibility of the reading of the scale, independently of the location of the device.
  • the ring 19 is able to slide, with reference to ring 11, on the sleeve 12 in the longitudinal direction of the latter.
  • This longitudinal motion must be such that, in the case of using a combustible gas and a comburent gas, a composition of gas mixture is obtained which is the neutral combustion or the theoretical basis composition when the line 0 of the graduation 18 of the ring 11 is positioned facing the axial line of scale 36.
  • the line of the graduation 18 will thus be established facing the line 0" of the scale 36 on the ring 19 in such a manner as to obtain on one side of the line 0 of the ring 11 the graduations corresponding to the reducing ratios and on the other side of such line 0 the graduations corresponding to the oxidising ratios.
  • annular gasket 20 Between the nozzle 1 and the sleeve 12 is provided an annular gasket 20 on either side of the slots 14 and 15.
  • the outlet 7 of the nozzle 1 is provided with an outer circular flange 22, shown on a larger scale in FIG. 2, which establishes a stationary gas film 39 on the outer wall of such nozzle 1, located in the space 8 during the flow of the gas originating from the pipe 10 to the second nozzle 4.
  • the wall 23 of such flange 22, provided to establish the said stationary gas film on the outer wall of the nozzle, forms with such wall an angle equal to 90 at the most.
  • the sleeve 12 is provided, at the end thereof directed towards the chamber 9, with an outer screw thread 24, by means of which it is screwed on a hollow body 25 determining such chamber 9.
  • the nozzle 4 which is stationary, is screwed in the said hollow body on the side facing that one in which is screwed the sleeve 12.
  • the converging portion 2 of the nozzle 1 is extended by a cylindrical portion 30 as far as the outlet of the said nozzle, this cylindrical portion being coaxial with the nozzle 4 so as to achieve a laminar flow of the gas at the outlet of the nozzle 1.
  • a pressure regulator 31 connected to a pipe 32 branched off the outlet 33 of the nozzle 4 at the entry of a mixing chamber 34 and controlling a valve 40 mounted in the pipe 10, assures the maintenance in the chamber 9 of a pressure substantially equal to that present at the outlet 33 of the nozzle 4, in the mixing chamber 34.
  • the device according to the invention it is possible to obtain a constant ratio of two gases in a mixture of the latter while maintaining a perfect laminar flow of the superposed coaxial layers of these two gases in the device, in particular at the time when the latter are in contact with one another so that no transmission of energy, within the framework of Bernoullis law, takes place in the device, the mixture of the two gases only taking place in the mixing chamber 34 in which are mounted, for example, two inverted pitch helical screws which have not been shown on the drawings.
  • the coefficient of friction on the walls of the annular space 8 supplying the gas originating from the pipe around the jet of the other gas escaping from the nozzle 1, is maintained as constant as possible independently of the rate of the gas passing therein when the flow varres.
  • the stationary film 39 hereinbefore described which is then established, substantially reduces the coefficient of the said friction within the annular space 8 on the outer wall of the nozzle 1 because the coefficient of friction between a stationary layer of a fluid and a mobile layer of the same fluid is far less than that for the same fluid on a solid wall.
  • a similar flange can, of course, be provided on the inner wall of the entry 6 of the nozzle 4.
  • a substantially plane cross-sectional diagram of the rates will then be obtained the form of which, in practice, does not vary within the usual limits of flow of the device, thus ensuring the ratio of the two gases remaining constant.
  • the device according to the invention permits to carry out with a very great accuracy an axial movement of one of the nozzles, under the circumstances the nozzle 1, with reference to the other nozzle in order to adjust the ratio of the two gases.
  • This accuracy permits the maintenance, for a relative position of the two nozzles, of a well defined ratio constant in time for such poition.
  • a particularly advantageous embodiment of the device is that in which the drive of the movable nozzle takes place in points symmetrical with reference to the axis, for example in locations diametrically facing one another.
  • FIG. 3 shows a modified form of the device hereinbefore described and enables carrying out the movement of the mobile nozzle in a continuous manner.
  • This embodiment is particularly of interest in order to maintain a constant chemical composition of the mixture of two gases, when the temperature of one at least of the gases varies. Indeed, the variation of the temperature of a gas results in a variation of its density and, consequently, the number of moles passing through the nozzle 1 under the influence of the difference in pressure at the entry of nozzle 1 with reference to the outlet thereof.
  • the ring 1 l is moved by means of a pneumatic or hydraulic servo-motor, not shown in FIG. 3, controlled by an analyser of the gas mixture present at the outlet of the nozzle 4, in the mixing chamber 34, this analyser not having been shown either in FIG. 3.
  • the outer cylindrical surface of the ring 11 is grooved along its generatrices.
  • the servo-motor drives a straight tooth pinion 37 meshing with the grooves of the said cylindrical surface, which thus provide teeth.
  • the cylindrical portion 30 of the nozzle 1 engages nozzle 4 as far as the conical frustrum 28 of the latter as shown in dash lines in FIG. 1.
  • the device does not operate as an injector as, on account of the laminar and parallel flow of the two gases, the doses of which are to be controlled, there is no exchange of energy between such gases, i.e. a drawing of one gas by the other.
  • the length of the whole of the device according to the invention does not vary when the distance between the two nozzles is changed so that its mounting in a supply circuit of an apparatus, for example of a burner, does not present any difficulty.
  • the ring 11 may, in a modified form of the object of the present invention, be freely threaded on the sleeve 12, the driving members 14 and 15 then engaging the threads of the inner screw thread 24 provided in the ring 11.
  • the ring 11 therefore does not move along the axis thereof, when it is made to rotate around the latter in order. to adjust the position of the nozzle 1 with reference to the nozzle 4.
  • a first nozzle adapted to communicate with a first adduction pipe at the upstream end thereof and having a converging portion at the downstream end thereof;
  • a housing defining a chamber which is adapted to communicate with a second adduction pipe, said chamber being shaped so as to enclose the downstream end of said first nozzle and so as to communicate with the entry of said second nozzle;
  • said means comprising:
  • a stationary sleeve (a) provided with an external screw thread, (b) enclosing one of said nozzles in a manner permitting said one of said nozzles to translate inside said stationary sleeve along the axis thereof, and having at least one slot therein which is parallel to said axis and which passes right through said sleeve;
  • At least one ring provided with an internal screw thread, by which it is threadedly interconnected with the external screw thread on said stationary sleeve so as to be movable thereon over said slot in said stationary sleeve, said ring being further provided with an annular recess coaxial with said sleeve and located on the inner face of said ring;
  • a driving member for said one of said nozzles which cooperates with said slot, is secured to the outer wall of said one of said nozzles, and engages freely said annular recess in said ring, whereby said one of said nozzles can be caused to move axially inside the device by making said ring rotate around its axis.
  • a device as claimed in claim 1 wherein said sleeve has at least two such slots located diametrically opposite one another in said sleeve and a like number of driving members for said one of said nozzles cooperating with said slots.
  • a first nozzle adapted to communicate with a first adduction pipe at the upstream end thereof and having a converging portion at the downstream end thereof;
  • a second nozzle coaxial with said first nozzle and having a diverging portion at the upstream end thereof at least the entry of which is of larger internal cross-section than the external cross-section of the downstream portion of said first nozzle, whereby said downstream portion of said first nozzle may be inserted in said entry of said second nozzle;
  • a housing defining a chamber which is adapted to communicate with a second adduction pipe, said chamber being shaped so as to enclose the downstream end of said first nozzle and so as to communicate with the entry of said second nozzle;
  • said means comprising:
  • a first ring provided with an internal screw thread, by which it is threadedly interconnected with the external screw thread on said stationary sleeve so as to be movable thereon over said slot in said stationary sleeve, said first ring being further provided with a graduation on the visible face thereof showing the ratio of the two gases to be mixed in terms of the position of said first ring on said sleeve, said graduation extending close to one of the rims of said sleeve over at least a portion of the periphery thereof;
  • a second ring mounted in a movable manner on said stationary sleeve close to said first ring, whereby the location of said second ring may be adjusted with reference to said first ring, said second ring being provided with a mark line extending parallel to the axis of said sleeve on the visible face thereof;
  • the space bea stationary sleeve (a) provided with an external tween two consecutive graduations of such scale screw thread, (b) enclosing one of said nozzles being equal to the pitch of the internal thread of in a manner permitting said one of said nozzles said first ring, whereby the latter moves by one to translate inside said stationary sleeve along the graduation on the second ring when it completes axis thereof, and (c) having at least one slot one revolution around its axis. therein which is parallel to said axis and which 6.
  • a device for controlling a mixture of two gases passes right through said sleeve; said device comprising: at least one ring provided with an internal screw a first nozzle adapted to communicate with a first adthread, by which it is threadedly interconnected duction pipe at the upstream end thereof and havwith the external screw thread on said stationary ing a converging portion at the downstream end sleeve so as to be movable thereon over said slot thereof, said first nozzle being further provided in said stationary sleeve; and with an outer flange around the outlet thereof the a driving member for said one of said nozzles which upstream wall of which forms an angle with the cooperates with said slot, is secured to the outer outside wall of said first nozzle which is less than or wall of said one of said nozzles, and engages equal to 90", whereby it establishes a stationary gas freely the inner face of said first ring, film extending upstream from said flange over at whereby said nozzle can be caused to move axially inleast

Abstract

A device for controlling a mixture of two gases comprises two nozzles mounted in the extension of one another and movable one with reference to the other, a ring, provided with an internal screw thread, being mounted in movable manner on a stationary sleeve enclosing one of the nozzles, the other one being mounted so as to be able to slide inside the said sleeve, at least one slot being provided in the sleeve, one driving member for the second nozzle, cooperating with such slot, being secured to the wall of the said nozzle and entering freely in the ring, so as to permit the said nozzle to move inside the device by making the ring rotate around its axis with reference to said sleeve.

Description

United States Patent [191 Hermans 1 Mar. 26, 1974 DEVICE FOR CONTROLLING A MIXTURE OF TWO GASES Fernand Victor Francois Hermans, Uccle, Belgium [73] Assignee: Le Four Industriel Belge, Uccle,
Belgium 22 Filed: Feb. 17, 1972 21 Appl. No.: 227,492
[75] Inventor:
[30] Foreign Application Priority Data Mar. 17, 1971 Belgium 764407 [52] US. Cl. 137/553, 48/180 P, 137/88, 137/604, 417/184, 417/191, 417/198, 259/4 [51] Int. Cl. Fl6k 19/00 [58] Field of Search 48/180P; 137/88, 90, 553, 137/604;259/4;4l7/183,184,191,198
[56] References Cited UNITED STATES PATENTS 2,178,898 11/1939 Schellin et a1. 417/183 3,643,688 2/1972 Meinert 137/604 1,583,363 5/1926 Ostermann 417/184 2,888,191 5/1959 Neumann et a1. 417/183 X 2,946,293 7/1960 Henshaw 417/183 3,031,127 4/1962 Duhaime et a1. 2,992,084 7/1961 Schropp 3,689,237 9/1972 Stark et a1. 137/604 X Primary ExaminerRobert G. Nilson Attorney, Agent, or Firm--Sughrue, Rothwell, Mion, Zinn & Macpeak [5 7] ABSTRACT nozzle and entering freely in the ring, so as to permit the said nozzle to move inside the device by making the ring rotate around its axis with reference to said sleeve.
7 Claims, 3 Drawing Figures i :ll 1 v I: 1 I l I I I 5 "I i ll DEVICE FOR CONTROLLING A MIXTURE OF TWO GASES The present invention relates to a device for controlling a mixture of two gases, such as a comburent gas and a combustible gas, comprising a first nozzle with a converging portion, such nozzle communicating with a first adduction pipe for one of the said components of the mixture and in the rear of which is a second nozzle coaxial with the first one, the second nozzle having a diverging portion, at least the entry of the latter being of larger internal circular cross-section than the external circular cross-section of the first nozzle, a chamber wherein opens a second adduction pipe for the other component of the said mixture, enclosing the outlet end of the first nozzle and communicating with the entry of the second nozzle, means being provided to vary along the common axis of the two nozzles, the relative position of the latter.
The aim of the invention is to provide an improved device of the said type enabling to achieve a strictly constant ratio, upstream of the equipment to be supplied, such as heating apparatus, between the two components of the mixture and this for flows of this gas mixture varying between fairly large limits.
For this purpose, in the device according to the invention, the means provided to vary, along the common axis of the twonozzles, the relative position of the latter comprise at least one ring, provided with an internal screw thread, mounted in movable manner on a stationary sleeve enclosing one of the nozzles, the nozzle located inside the sleeve being fitted in such a manner as to be able to slide inside the latter along the axis thereof; at least one slot, parallel to the said axis, passing right through the portion of the wall of the said sleeve covered by the said ring; a driving member for such nozzle co-operating with such slot and being secured to the inner wall of the nozzle and engaging freely the inner face of the ring covering the slot, so as to permit the said nozzle to move inside the device by making the ring rotate around its axis with reference to the sleeve.
Advantageously, the sleeve, comprises atleast two slots diametrically opposite one another, parallel to the axis of the nozzle fitted inside the sleeve, the said driving m'ember for such nozzle co-operating with each one of the said slots.
According to a preferred embodiment of the invention, the first nozzle is assembled in the said sleeve, the second nozzle being stationary with reference to the latter.
According to a particular embodiment of the invention, a flange is provided at the outlet of at least one of the nozzles, so as to permit establishing close to such outlet, a stationary gas film.
Particular construction embodiments of the present invention will now be described by way of non limitative examples, with reference to the accompanying drawings in which:
F 1G. 1 shows diagrammatically a longitudinal crosssection partially broken away, of a particular embodiment of the invention.
FIG. 2 shows on a large scale a detail of the device shown in FIG. 1. I
FIG. 3 is an elevational view, partially broken away, of a detail of a modified form of the device shown in FIG. 1.
The device according to the invention, comprises a first nozzle 1, with a converging portion 2 and communicating with an adduction pipe 3 for a first gas, and a second nozzle 4 coaxial with the first one and mounted downstream of the latter.
The second nozzle 4 has a diverging portion, at least the entry 6 of the latter being of larger internal circular cross-section than the external circular cross-section of the outlet 7 of the first nozzle 1, so as to permit engaging such outlet 7 in the entry 6 while maintaining in between them an annular space 8 for the passage of a gas originating from a chamber 9 enclosing the outlet end of the first nozzle 1 and communicating with the entry 6 of the second nozzle 4. A second adduction pipe 10 for a second gas opens into the said chamber 9.
A ring 11 with an internal helical thread 17 is freely threaded on a stationary sleeve 12 enclosing the nozzle 1, the latter being fitted in such a manner as to be able to translate inside the sleeve along the common axis 13.
Two slots 14 and 15, diametrically opposite, parallel to the said axis, pass right through the portion of the wall of the said sleeve covered by the thread 17 of the ring 11. A driving member, provided by a stem 16, cooperates with each one of these slots 14 and 15. This member is secured by one of its ends to the outside wall of the nozzle and engages freely with its other end an annular slot 35 provided in the inner face of the ring 11 and concentric with the latter, these two stems 16 being also diametrically opposite one another.
The movement of such nozzle 1 along its axis 13 is thus achieved by making the ring 11 rotate around its axis 13 with reference to the stationary sleeve 12.
The ring 11 is knurled on its outside face and provided with a graduation 18 showing the ratio of the two gases in terms of the position of this ring of the sleeve 12.
As the position of the nozzle 1, for a given value of the ratio of the two gases, is a function of the density of the latter, a secondary ring 19 is provided on the sleeve 12, partially beneath ring 11 and which carries on its outside face, parallel to its axis, a graduated scale 36. Ring 11 may be rotated around its axis in both directions. The graduation of the scale 36 in such that for one revolution of the ring 11, the latter moves in the axial direction by one unit of the graduation, so that the rim of the ring 11 located on the side of the ring 19 shall coincide with the line mark according to the graduation 36. The two graduated rings 11 and 19 thus determine a vernier permitting measurement, in a very accurate manner, of the axial movement of the nozzle 1 and, consequently, also the ratio of the two gases.
The ring 19 may, just like the ring 11, rotate around its axis so as to enable a movement of the graduated scale 36 simultaneously with the graduations 18 and thus ensure the accessibility of the reading of the scale, independently of the location of the device.
Furthermore, in order to allow for the types of gases used, the ring 19 is able to slide, with reference to ring 11, on the sleeve 12 in the longitudinal direction of the latter. This longitudinal motion must be such that, in the case of using a combustible gas and a comburent gas, a composition of gas mixture is obtained which is the neutral combustion or the theoretical basis composition when the line 0 of the graduation 18 of the ring 11 is positioned facing the axial line of scale 36. By chemical calibration of the stoichiometrical ratio of the combustible gas comburent gas mixture, the line of the graduation 18 will thus be established facing the line 0" of the scale 36 on the ring 19 in such a manner as to obtain on one side of the line 0 of the ring 11 the graduations corresponding to the reducing ratios and on the other side of such line 0 the graduations corresponding to the oxidising ratios.
Between the nozzle 1 and the sleeve 12 is provided an annular gasket 20 on either side of the slots 14 and 15.
These gaskets 20 are arrested in an annular housing 21 provided in the outer wall of the nozzle 1.
The outlet 7 of the nozzle 1 is provided with an outer circular flange 22, shown on a larger scale in FIG. 2, which establishes a stationary gas film 39 on the outer wall of such nozzle 1, located in the space 8 during the flow of the gas originating from the pipe 10 to the second nozzle 4. The wall 23 of such flange 22, provided to establish the said stationary gas film on the outer wall of the nozzle, forms with such wall an angle equal to 90 at the most. The sleeve 12 is provided, at the end thereof directed towards the chamber 9, with an outer screw thread 24, by means of which it is screwed on a hollow body 25 determining such chamber 9.
The nozzle 4 which is stationary, is screwed in the said hollow body on the side facing that one in which is screwed the sleeve 12.
The entry 6 of the nozzle 4 is converging and is formed by two conical frustums 27 and 28 placed end to end. The taper of the first frustum 27 substantially exceeds that of the other frustum 28, which is of rather low taper. The conical frustrum 28 is connected to the said diverging portion by means of a cylindrical portion 29 providing a narrowing in the nozzle 4.
The converging portion 2 of the nozzle 1 is extended by a cylindrical portion 30 as far as the outlet of the said nozzle, this cylindrical portion being coaxial with the nozzle 4 so as to achieve a laminar flow of the gas at the outlet of the nozzle 1. On the other hand, a pressure regulator 31 connected to a pipe 32 branched off the outlet 33 of the nozzle 4 at the entry of a mixing chamber 34 and controlling a valve 40 mounted in the pipe 10, assures the maintenance in the chamber 9 of a pressure substantially equal to that present at the outlet 33 of the nozzle 4, in the mixing chamber 34.
With the device according to the invention it is possible to obtain a constant ratio of two gases in a mixture of the latter while maintaining a perfect laminar flow of the superposed coaxial layers of these two gases in the device, in particular at the time when the latter are in contact with one another so that no transmission of energy, within the framework of Bernoullis law, takes place in the device, the mixture of the two gases only taking place in the mixing chamber 34 in which are mounted, for example, two inverted pitch helical screws which have not been shown on the drawings.
Thus for a mixture of combustible and comburent gas, when the device is mounted on a burner, the ratio of the two gases is not influenced by the back-pressure at the burner outlet.
The coefficient of friction on the walls of the annular space 8 supplying the gas originating from the pipe around the jet of the other gas escaping from the nozzle 1, is maintained as constant as possible independently of the rate of the gas passing therein when the flow varres.
It is, however, well known that as a result of the friction of the gas on the walls, the rate of flow in the thickness of the jet is not uniform but assumes the shape of a parabola which is the more drawn out the more the mean rate of the flow increases. It results, therefrom, consequently, that if precautions are not taken, the flow will not be proportionate to the loss of head in this annular space 8. Thus, for this reason, the outer circular flange 22 has been provided at the outlet 7 of the first nozzle. The stationary film 39 hereinbefore described, which is then established, substantially reduces the coefficient of the said friction within the annular space 8 on the outer wall of the nozzle 1 because the coefficient of friction between a stationary layer of a fluid and a mobile layer of the same fluid is far less than that for the same fluid on a solid wall.
A similar flange can, of course, be provided on the inner wall of the entry 6 of the nozzle 4. In the annular space 8 between the nozzles 1 and 4 a substantially plane cross-sectional diagram of the rates will then be obtained the form of which, in practice, does not vary within the usual limits of flow of the device, thus ensuring the ratio of the two gases remaining constant.
On the other hand, another condition met by the device according to the invention and which is also essential in order to reach the aim, hereinbefore defined, is that it permits to carry out with a very great accuracy an axial movement of one of the nozzles, under the circumstances the nozzle 1, with reference to the other nozzle in order to adjust the ratio of the two gases. This accuracy permits the maintenance, for a relative position of the two nozzles, of a well defined ratio constant in time for such poition.
In certain known types of devices of this kind, the nozzle 1 is slightly inclined during its movement so that its axis no longer coincides with that of the other nozzle 4. The annular space 8, therefore, will no longer be in that case centered for such devices and the asymmetry then established will hinder the flow of the gas and influence the said ratio when the flow varies.
It is for this reason that a particularly advantageous embodiment of the device is that in which the drive of the movable nozzle takes place in points symmetrical with reference to the axis, for example in locations diametrically facing one another.
FIG. 3 shows a modified form of the device hereinbefore described and enables carrying out the movement of the mobile nozzle in a continuous manner. This embodiment is particularly of interest in order to maintain a constant chemical composition of the mixture of two gases, when the temperature of one at least of the gases varies. Indeed, the variation of the temperature of a gas results in a variation of its density and, consequently, the number of moles passing through the nozzle 1 under the influence of the difference in pressure at the entry of nozzle 1 with reference to the outlet thereof.
For this purpose, according to the invention, the ring 1 l is moved by means of a pneumatic or hydraulic servo-motor, not shown in FIG. 3, controlled by an analyser of the gas mixture present at the outlet of the nozzle 4, in the mixing chamber 34, this analyser not having been shown either in FIG. 3.
The outer cylindrical surface of the ring 11 is grooved along its generatrices. The servo-motor drives a straight tooth pinion 37 meshing with the grooves of the said cylindrical surface, which thus provide teeth.
In normal operational position, the cylindrical portion 30 of the nozzle 1 engages nozzle 4 as far as the conical frustrum 28 of the latter as shown in dash lines in FIG. 1. Thus the device does not operate as an injector as, on account of the laminar and parallel flow of the two gases, the doses of which are to be controlled, there is no exchange of energy between such gases, i.e. a drawing of one gas by the other.
It should also be noted that the length of the whole of the device according to the invention, does not vary when the distance between the two nozzles is changed so that its mounting in a supply circuit of an apparatus, for example of a burner, does not present any difficulty.
It is well understood that the invention is not limited to the described embodiment and that many changes may be introduced therein without departing from the scope of the present patent application.
Thus either the nozzle 1 or the nozzle 4 and even, as the case may be, both of them may be mobile; that the device may be used also for controlling a mixture of any two gases such as hydrogen and air, or of air and a combustible gas.
On the other hand, the ring 11 may, in a modified form of the object of the present invention, be freely threaded on the sleeve 12, the driving members 14 and 15 then engaging the threads of the inner screw thread 24 provided in the ring 11. In this modified form, the ring 11 therefore does not move along the axis thereof, when it is made to rotate around the latter in order. to adjust the position of the nozzle 1 with reference to the nozzle 4.
I claim:
1. A device for controlling a mixture of two gases, said device comprising:
a first nozzle adapted to communicate with a first adduction pipe at the upstream end thereof and having a converging portion at the downstream end thereof;
a second nozzle coaxial with said first nozzle and having a diverging portion at the upstream end thereof at least the entry of which is of larger internal cross-section than the external cross-section of the downstream portion of said first nozzle, whereby said downstream portion of said first nozzle may be inserted in said entry of said second nozzle;
a housing defining a chamber which is adapted to communicate with a second adduction pipe, said chamber being shaped so as to enclose the downstream end of said first nozzle and so as to communicate with the entry of said second nozzle; and
means for varying the relative position of said first and second nozzles along their common axis, said means comprising:
a stationary sleeve (a) provided with an external screw thread, (b) enclosing one of said nozzles in a manner permitting said one of said nozzles to translate inside said stationary sleeve along the axis thereof, and having at least one slot therein which is parallel to said axis and which passes right through said sleeve;
at least one ring provided with an internal screw thread, by which it is threadedly interconnected with the external screw thread on said stationary sleeve so as to be movable thereon over said slot in said stationary sleeve, said ring being further provided with an annular recess coaxial with said sleeve and located on the inner face of said ring; and
a driving member for said one of said nozzles which cooperates with said slot, is secured to the outer wall of said one of said nozzles, and engages freely said annular recess in said ring, whereby said one of said nozzles can be caused to move axially inside the device by making said ring rotate around its axis.
2. A device as claimed in claim 1 wherein said sleeve has at least two such slots located diametrically opposite one another in said sleeve and a like number of driving members for said one of said nozzles cooperating with said slots.
3. A device as claimed in claim 1 wherein said sleeve has a plurality of such slots symmetrically located in said sleeve and a like number of driving members for said one of said nozzles cooperating with said slots.
4. A device for controlling a mixture of two gases, said device comprising:
a first nozzle adapted to communicate with a first adduction pipe at the upstream end thereof and having a converging portion at the downstream end thereof;
a second nozzle coaxial with said first nozzle and having a diverging portion at the upstream end thereof at least the entry of which is of larger internal cross-section than the external cross-section of the downstream portion of said first nozzle, whereby said downstream portion of said first nozzle may be inserted in said entry of said second nozzle;
a housing defining a chamber which is adapted to communicate with a second adduction pipe, said chamber being shaped so as to enclose the downstream end of said first nozzle and so as to communicate with the entry of said second nozzle; and
means for varying the relative position of said first and second nozzles along their common axis, said means comprising:
a stationary sleeve (a) provided with an external screw thread, (b) enclosing one of said nozzles in a manner permitting said one of said nozzles to translate inside said stationary sleeve along the axis thereof, and (0) having at least one slot therein which is parallel to said axis and which passes right through said sleeve;
a first ring provided with an internal screw thread, by which it is threadedly interconnected with the external screw thread on said stationary sleeve so as to be movable thereon over said slot in said stationary sleeve, said first ring being further provided with a graduation on the visible face thereof showing the ratio of the two gases to be mixed in terms of the position of said first ring on said sleeve, said graduation extending close to one of the rims of said sleeve over at least a portion of the periphery thereof;
a second ring mounted in a movable manner on said stationary sleeve close to said first ring, whereby the location of said second ring may be adjusted with reference to said first ring, said second ring being provided with a mark line extending parallel to the axis of said sleeve on the visible face thereof; and
a driving member for said one of said nozzles which 7 8 the with said slot, is secured to the outer wall of said cross-section than the external cross-section of the one of said nozzles and engages freely the inner downstream portion of said first nozzle, whereby face of said first ring, said downstream portion of said first nozzle may be whereby said one of said nozzles can be caused to move inserted in said entry of said second nozzle; axially inside the device by making said ring rotate a housing defining a chamber which is adapted to around its axis. communicate with a second adduction pipe, said 5. A device as claimed in claim 4 wherein chamber being shaped so as to enclose the downthe outer diameter of at least the portion of said secstream end of said nozzle to a degree at least suffiond ring adjacent to said first ring is less that the cient to include said stationary gas film and so as inner diameter of at least the portion of said first 10 to communicate with the entry of said second nozring adjacent to said second ring, thereby permitzle; and ting at least a portion of said first ring to pass over means for varying the relative position of said first at least a portion of said second ring, and and second nozzles along their common axis, said said mark line on said second ring has in its turn gradmeans comprising:
uations providing a graduated scale, the space bea stationary sleeve (a) provided with an external tween two consecutive graduations of such scale screw thread, (b) enclosing one of said nozzles being equal to the pitch of the internal thread of in a manner permitting said one of said nozzles said first ring, whereby the latter moves by one to translate inside said stationary sleeve along the graduation on the second ring when it completes axis thereof, and (c) having at least one slot one revolution around its axis. therein which is parallel to said axis and which 6. A device for controlling a mixture of two gases, passes right through said sleeve; said device comprising: at least one ring provided with an internal screw a first nozzle adapted to communicate with a first adthread, by which it is threadedly interconnected duction pipe at the upstream end thereof and havwith the external screw thread on said stationary ing a converging portion at the downstream end sleeve so as to be movable thereon over said slot thereof, said first nozzle being further provided in said stationary sleeve; and with an outer flange around the outlet thereof the a driving member for said one of said nozzles which upstream wall of which forms an angle with the cooperates with said slot, is secured to the outer outside wall of said first nozzle which is less than or wall of said one of said nozzles, and engages equal to 90", whereby it establishes a stationary gas freely the inner face of said first ring, film extending upstream from said flange over at whereby said nozzle can be caused to move axially inleast a portion of the outside wall of said first nozside the device by making said ring rotate around its zle when the device is in use; axis. a second nozzle coaxial with said first nozzle and hav- 7. A device as claimed in claim 6 wherein said uping a diverging portion at the upstream end thereof stream wall of said flange is planar.
at least the entry of which is of larger internal

Claims (7)

1. A device for controlling a mixture of two gases, said device comprising: a first nozzle adapted to communicate with a first adduction pipe at the upstream end thereof and having a converging portion at the downstream end thereof; a second nozzle coaxial with said first nozzle and having a diverging portion at the upstream end thereof at least the entry of which is of larger internal cross-section than the external cross-section of the downstream portion of said first nozzle, whereby said downstream portion of said first nozzle may be inserted in said entry of said second nozzle; a housing defining a chamber which is adapted to communicate with a second adduction pipe, said chamber being shaped so as to enclose the downstream end of said first nozzle and so as to communicate with the entry of said second nozzle; and means for varying the relative position of said first and second nozzles along their common axis, said means comprising: a stationary sleeve (a) provided with an external screw thread, (b) enclosing one of said nozzles in a manner permitting said one of said nozzles to translate inside said stationary sleeve along the axis thereof, and (c) having at least one slot therein which is parallel to said axis and which passes right through said sleeve; at least one ring provided with an internal screw thread, by which it is threadedly interconnected with the external screw thread on said stationary sleeve so as to be movable thereon over said slot in said stationary sleeve, said ring being further provided with an annular recess coaxial with said sleeve and located on the inner face of said ring; and a driving member for said one of said nozzles which cooperates with said slot, is secured to the outer wall of said one of said nozzles, and engages freely said annular recess in said ring, whereby said one of said nozzles can be caused to move axially inside the device by making said ring rotate around its axis.
2. A device as claimed in claim 1 wherein said sleeve has at least two such slots located diametrically opposite one another in said sleeve and a like number of driving members for said one of said nozzles cooperating with said slots.
3. A device as claimed in claim 1 wherein said sleeve has a plurality of such slots symmetrically located in said sleeve and a like number of driving members for said one of said nozzles cooperating with said slots.
4. A device for controlling a mixture of two gases, said device comprising: a first nozzle adapted to communicate with a first adduction pipe at the upstream end thereof and having a converging portion at the downstream end thereof; a second nozzle coaxial with said first nozzle and having a diverging portion at the upstream end thereof at least the entry of which is of larger internal cross-section than the external cross-section of the downstream portion of said first nozzle, whereby said downstream portion of said first nozzle may be inserted in said entry of said second nozzle; a housing defining a chamber which is adapted to communicate with a second adduction pipe, said chamber being shaped so as to Enclose the downstream end of said first nozzle and so as to communicate with the entry of said second nozzle; and means for varying the relative position of said first and second nozzles along their common axis, said means comprising: a stationary sleeve (a) provided with an external screw thread, (b) enclosing one of said nozzles in a manner permitting said one of said nozzles to translate inside said stationary sleeve along the axis thereof, and (c) having at least one slot therein which is parallel to said axis and which passes right through said sleeve; a first ring provided with an internal screw thread, by which it is threadedly interconnected with the external screw thread on said stationary sleeve so as to be movable thereon over said slot in said stationary sleeve, said first ring being further provided with a graduation on the visible face thereof showing the ratio of the two gases to be mixed in terms of the position of said first ring on said sleeve, said graduation extending close to one of the rims of said sleeve over at least a portion of the periphery thereof; a second ring mounted in a movable manner on said stationary sleeve close to said first ring, whereby the location of said second ring may be adjusted with reference to said first ring, said second ring being provided with a mark line extending parallel to the axis of said sleeve on the visible face thereof; and a driving member for said one of said nozzles which the with said slot, is secured to the outer wall of said one of said nozzles and engages freely the inner face of said first ring, whereby said one of said nozzles can be caused to move axially inside the device by making said ring rotate around its axis.
5. A device as claimed in claim 4 wherein the outer diameter of at least the portion of said second ring adjacent to said first ring is less that the inner diameter of at least the portion of said first ring adjacent to said second ring, thereby permitting at least a portion of said first ring to pass over at least a portion of said second ring, and said mark line on said second ring has in its turn graduations providing a graduated scale, the space between two consecutive graduations of such scale being equal to the pitch of the internal thread of said first ring, whereby the latter moves by one graduation on the second ring when it completes one revolution around its axis.
6. A device for controlling a mixture of two gases, said device comprising: a first nozzle adapted to communicate with a first adduction pipe at the upstream end thereof and having a converging portion at the downstream end thereof, said first nozzle being further provided with an outer flange around the outlet thereof the upstream wall of which forms an angle with the outside wall of said first nozzle which is less than or equal to 90*, whereby it establishes a stationary gas film extending upstream from said flange over at least a portion of the outside wall of said first nozzle when the device is in use; a second nozzle coaxial with said first nozzle and having a diverging portion at the upstream end thereof at least the entry of which is of larger internal cross-section than the external cross-section of the downstream portion of said first nozzle, whereby said downstream portion of said first nozzle may be inserted in said entry of said second nozzle; a housing defining a chamber which is adapted to communicate with a second adduction pipe, said chamber being shaped so as to enclose the downstream end of said nozzle to a degree at least sufficient to include said stationary gas film and so as to communicate with the entry of said second nozzle; and means for varying the relative position of said first and second nozzles along their common axis, said means comprising: a stationary sleeve (a) provided with an external screw thread, (b) enclosing one of said nozzles in a manner permitting said one of said nozzles to translate inside saiD stationary sleeve along the axis thereof, and (c) having at least one slot therein which is parallel to said axis and which passes right through said sleeve; at least one ring provided with an internal screw thread, by which it is threadedly interconnected with the external screw thread on said stationary sleeve so as to be movable thereon over said slot in said stationary sleeve; and a driving member for said one of said nozzles which cooperates with said slot, is secured to the outer wall of said one of said nozzles, and engages freely the inner face of said first ring, whereby said nozzle can be caused to move axially inside the device by making said ring rotate around its axis.
7. A device as claimed in claim 6 wherein said upstream wall of said flange is planar.
US00227492A 1971-03-17 1972-02-17 Device for controlling a mixture of two gases Expired - Lifetime US3799195A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE764407A BE764407A (en) 1971-03-17 1971-03-17 DEVICE FOR THE DOSING OF A MIXTURE OF TWO GASES.

Publications (1)

Publication Number Publication Date
US3799195A true US3799195A (en) 1974-03-26

Family

ID=3857859

Family Applications (1)

Application Number Title Priority Date Filing Date
US00227492A Expired - Lifetime US3799195A (en) 1971-03-17 1972-02-17 Device for controlling a mixture of two gases

Country Status (8)

Country Link
US (1) US3799195A (en)
BE (1) BE764407A (en)
DE (1) DE2209812A1 (en)
DK (1) DK132720C (en)
FR (1) FR2130101B1 (en)
GB (1) GB1371698A (en)
PL (1) PL88978B1 (en)
SU (1) SU469270A3 (en)

Cited By (54)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2431674A1 (en) * 1974-07-02 1976-01-22 Lindgens Kg Mixing valve for two component gas mixture - e.g. for glass or ceramics production has hollow control piston sliding in mixing housing
US4000001A (en) * 1975-06-23 1976-12-28 The Great Western Sugar Company Hydrodynamic precipitation method and apparatus
US4029299A (en) * 1975-09-22 1977-06-14 Hechler Iv Valentine Multi-stage solution proportioner dispenser
US4123800A (en) * 1977-05-18 1978-10-31 Mazzei Angelo L Mixer-injector
US4210166A (en) * 1977-09-14 1980-07-01 Munie Julius C Mixing apparatus
US4422833A (en) * 1981-05-11 1983-12-27 Free Flow, Inc. Pneumatic transfer system and a fluid flow control device therefor
US4615352A (en) * 1984-05-17 1986-10-07 Carboxyque Francaise Process and apparatus for supplying a mixture of CO2 and SO2 or a like mixture under pressure
EP0207501A2 (en) * 1985-07-05 1987-01-07 K.E.W. Industri A/S An automatic aspirator-transfer valve, and a jet washing apparatus comprising such a valve
US4765373A (en) * 1987-07-07 1988-08-23 Coppus Engineering Corporation Gas flow amplifier
US5107891A (en) * 1989-09-05 1992-04-28 Sanki Kogyo Yugen Kaisha Safety device for gas welding
US5205648A (en) * 1990-09-06 1993-04-27 Transsonic Uberschall-Anlagen Gmbh Method and device for acting upon fluids by means of a shock wave
US5544961A (en) * 1992-02-11 1996-08-13 April Dynamics Industries Ltd. Two-phase supersonic flow system
US5779355A (en) * 1997-02-27 1998-07-14 Roger H. Woods Limited Mixing apparatus venturi coupled multiple shear mixing apparatus for repairing a liquid-solid slurry
US5842497A (en) * 1996-05-20 1998-12-01 Hydro-Thermal Corporation Adjustable shear direct contact steam injection heater
US5863128A (en) * 1997-12-04 1999-01-26 Mazzei; Angelo L. Mixer-injectors with twisting and straightening vanes
US5951922A (en) * 1998-02-10 1999-09-14 Mazzei; Angelo L. Aeration system for substantial bodies of water
US6016840A (en) * 1996-11-19 2000-01-25 Popov; Serguei A. Liquid/gas vacuum ejector device
WO2000074832A1 (en) * 1999-06-07 2000-12-14 Centro Sviluppo Materiali S.P.A. Device for introducing a gaseous substance in a fluid and use thereof
US6203186B1 (en) * 1999-09-13 2001-03-20 Luis R. Cruz Spherical eductor atomizer
US6299343B1 (en) * 1997-12-02 2001-10-09 Tivon Co. Method of heating and/or homogenizing of liquid products in a steam-liquid injector
US20030007874A1 (en) * 2001-07-06 2003-01-09 Junichi Ikeda Ejector and negative-pressure supply apparatus using the same
US20030024485A1 (en) * 2001-06-08 2003-02-06 Freidell James E. Animal bathing system
US6523991B1 (en) * 1998-07-08 2003-02-25 Jaber Maklad Method and device for increasing the pressure or enthalpy of a fluid flowing at supersonic speed
US20030137897A1 (en) * 2000-10-30 2003-07-24 Whiteley Bruce Alan Fluid mixer with rotatable eductor tube and metering orifices
US6623154B1 (en) * 2000-04-12 2003-09-23 Premier Wastewater International, Inc. Differential injector
US20040141410A1 (en) * 2002-02-01 2004-07-22 Fenton Marcus B M Fluid mover
EP1499447A1 (en) * 2002-04-30 2005-01-26 Avrom R. Handleman Eductor mixer system
US20050053887A1 (en) * 2002-06-26 2005-03-10 Per Westergaard Burner fuel mixer head for concurrently burning two gaseous fuels
US20050077057A1 (en) * 2003-10-10 2005-04-14 Hale Products, Inc. Fire truck booster pump
US20050133615A1 (en) * 2003-12-18 2005-06-23 Bowles Fluidics Corporation Fluid injector and mixer apparatus
US20070025862A1 (en) * 2005-07-28 2007-02-01 Graham Corporation Compressible gas ejector with unexpanded motive gas-load gas interface
US20070210186A1 (en) * 2004-02-26 2007-09-13 Fenton Marcus B M Method and Apparatus for Generating a Mist
US20080219087A1 (en) * 2005-05-20 2008-09-11 Tronox Llc Fluid Mixing Apparatus and Method
US20080230632A1 (en) * 2004-02-24 2008-09-25 Marcus Brian Mayhall Fenton Method and Apparatus for Generating a Mist
US20080310970A1 (en) * 2004-07-29 2008-12-18 Pursuit Dynamics Plc Jet Pump
US20090240088A1 (en) * 2007-05-02 2009-09-24 Marcus Brian Mayhall Fenton Biomass treatment process and system
US7618182B1 (en) * 2007-04-19 2009-11-17 Vortex Systems (International) LI Dust-free low pressure mixing system with jet ring adapter
US20090314500A1 (en) * 2006-09-15 2009-12-24 Marcus Brian Mayhall Fenton Mist generating apparatus and method
US20100129888A1 (en) * 2004-07-29 2010-05-27 Jens Havn Thorup Liquefaction of starch-based biomass
US7784999B1 (en) * 2009-07-01 2010-08-31 Vortex Systems (International) Ci Eductor apparatus with lobes for optimizing flow patterns
US20120085124A1 (en) * 2010-10-08 2012-04-12 Tomohiro Maruyama Jet pump and air conditioner
CN102444626A (en) * 2010-10-08 2012-05-09 康奈可关精株式会社 Jet pump and air conditioner
CN101737777B (en) * 2008-11-12 2012-10-17 中国市政工程华北设计研究院 Burner used for fuel gas distribution and exchangeability test
US20130142007A1 (en) * 2011-11-16 2013-06-06 Basf Se Injector for a Granular Solid
CN104028153A (en) * 2014-05-22 2014-09-10 西安交通大学 Rotating Venturi mixer with uniform plate
EP2863125A1 (en) * 2013-10-16 2015-04-22 Robert Bosch Gmbh Heating device with a burner assisted by a blower
EP2863120A1 (en) * 2013-10-16 2015-04-22 Robert Bosch Gmbh Heating device with a burner assisted by a blower
US20180043319A1 (en) * 2016-08-11 2018-02-15 Evan Schneider Venturi device
WO2018217711A1 (en) * 2017-05-22 2018-11-29 Vayu Global Health Innovations, LLC An adjustable ambient air-oxygen blender
US10507480B2 (en) 2004-02-26 2019-12-17 Tyco Fire Products Lp Method and apparatus for generating a mist
US10596530B2 (en) * 2017-07-19 2020-03-24 Chapin Manufacturing, Inc. Variable venturi device with adjustable valve stem
US20210046434A1 (en) * 2016-03-23 2021-02-18 Alfa Laval Corporate Ab Apparatus for dispersing particles in a liquid
US11673104B2 (en) * 2018-12-07 2023-06-13 Produced Water Absorbents Inc. Multi-fluid injection mixer and related methods
CN117101997A (en) * 2023-09-06 2023-11-24 苏州子高科技有限公司 Drying device for coating equipment

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2946120A1 (en) * 1979-11-15 1981-05-27 Southwire Co., Carrollton, Ga. Controlling gaseous fuel combustion in metal melting furnace - by equalising temperature and pressure of fuel and air prior to combustion
DE3018752A1 (en) * 1980-05-16 1981-11-26 Ruhrgas Ag, 4300 Essen DEVICE FOR CONTROLLING THE COMBUSTION AIR AMOUNT IN GAS CONSUMPTION DEVICES WITH INJECTOR BURNERS
US4637792A (en) * 1980-12-22 1987-01-20 Arkansas Patents, Inc. Pulsing combustion
DE10228853B4 (en) * 2002-06-27 2007-02-08 Esau & Hueber Gmbh Nozzle arrangement for introducing gas into a liquid
BE1018675A3 (en) 2009-03-03 2011-06-07 Fib Belgium Sa DEVICE FOR DETERMINING A GASEOUS MIXTURE.
WO2016097669A1 (en) * 2014-12-19 2016-06-23 Smiths Medical International Limited Entrainment devices and respiratory therapy devices
GB2550130B (en) * 2016-05-09 2021-01-27 James Muggleton Kevin System including passive blender for use with gas from an unconventional source
CN112880386B (en) * 2021-02-21 2024-04-19 广西广投正润新材料科技有限公司 All-round aluminum alloy casting crystallizer baking equipment

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1583363A (en) * 1924-02-18 1926-05-04 Superheater Co Ltd Injector
US2178898A (en) * 1938-07-01 1939-11-07 Akron Brass Mfg Company Inc Siphon pump construction
US2888191A (en) * 1954-05-03 1959-05-26 Rheem Mfg Co Jet pump
US2946293A (en) * 1955-04-18 1960-07-26 Pyrene Co Ltd Inductors
US2992084A (en) * 1956-08-24 1961-07-11 Four Industriel Belge Apparatus for regulating the composition of a mixture of air and fuel-gas
US3031127A (en) * 1960-12-12 1962-04-24 Air Vac Engineering Company Vacuum creating devices
US3643688A (en) * 1969-01-28 1972-02-22 Noll Maschfab Gmbh Device for the continuous mixing of beverage components in a predetermined quantity ratio
US3689237A (en) * 1970-02-19 1972-09-05 North American Utility Constru Fuel gas pipeline system

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR869312A (en) * 1940-09-30 1942-01-29 Lemoine Ets Gas burner
US2321483A (en) * 1941-01-06 1943-06-08 Nat Machine Works Proportional mixer
FR1180516A (en) * 1956-08-24 1959-06-04 Four Industriel Belge Device for regulating a mixture of air and combustible gas
FR1499966A (en) * 1966-05-05 1967-11-03 Bertin & Cie Improvements to gaseous fluid mixers

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1583363A (en) * 1924-02-18 1926-05-04 Superheater Co Ltd Injector
US2178898A (en) * 1938-07-01 1939-11-07 Akron Brass Mfg Company Inc Siphon pump construction
US2888191A (en) * 1954-05-03 1959-05-26 Rheem Mfg Co Jet pump
US2946293A (en) * 1955-04-18 1960-07-26 Pyrene Co Ltd Inductors
US2992084A (en) * 1956-08-24 1961-07-11 Four Industriel Belge Apparatus for regulating the composition of a mixture of air and fuel-gas
US3031127A (en) * 1960-12-12 1962-04-24 Air Vac Engineering Company Vacuum creating devices
US3643688A (en) * 1969-01-28 1972-02-22 Noll Maschfab Gmbh Device for the continuous mixing of beverage components in a predetermined quantity ratio
US3689237A (en) * 1970-02-19 1972-09-05 North American Utility Constru Fuel gas pipeline system

Cited By (87)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2431674A1 (en) * 1974-07-02 1976-01-22 Lindgens Kg Mixing valve for two component gas mixture - e.g. for glass or ceramics production has hollow control piston sliding in mixing housing
US4000001A (en) * 1975-06-23 1976-12-28 The Great Western Sugar Company Hydrodynamic precipitation method and apparatus
FR2315312A1 (en) * 1975-06-23 1977-01-21 Great Western Sugar Co IMPROVEMENTS IN THE PRECIPITATION OF SOLID MATERIALS FROM LIQUIDS
US4029299A (en) * 1975-09-22 1977-06-14 Hechler Iv Valentine Multi-stage solution proportioner dispenser
US4123800A (en) * 1977-05-18 1978-10-31 Mazzei Angelo L Mixer-injector
US4210166A (en) * 1977-09-14 1980-07-01 Munie Julius C Mixing apparatus
US4422833A (en) * 1981-05-11 1983-12-27 Free Flow, Inc. Pneumatic transfer system and a fluid flow control device therefor
US4615352A (en) * 1984-05-17 1986-10-07 Carboxyque Francaise Process and apparatus for supplying a mixture of CO2 and SO2 or a like mixture under pressure
EP0207501A2 (en) * 1985-07-05 1987-01-07 K.E.W. Industri A/S An automatic aspirator-transfer valve, and a jet washing apparatus comprising such a valve
EP0207501A3 (en) * 1985-07-05 1988-02-17 Westergaard, Knud Erik An automatic aspirator-transfer valve, and a jet washing apparatus comprising such a valve
US4765373A (en) * 1987-07-07 1988-08-23 Coppus Engineering Corporation Gas flow amplifier
US5107891A (en) * 1989-09-05 1992-04-28 Sanki Kogyo Yugen Kaisha Safety device for gas welding
US5205648A (en) * 1990-09-06 1993-04-27 Transsonic Uberschall-Anlagen Gmbh Method and device for acting upon fluids by means of a shock wave
US5275486A (en) * 1990-09-06 1994-01-04 Transsonic Uberschall-Anlagen Gmbh Device for acting upon fluids by means of a shock wave
US5544961A (en) * 1992-02-11 1996-08-13 April Dynamics Industries Ltd. Two-phase supersonic flow system
US5842497A (en) * 1996-05-20 1998-12-01 Hydro-Thermal Corporation Adjustable shear direct contact steam injection heater
US6016840A (en) * 1996-11-19 2000-01-25 Popov; Serguei A. Liquid/gas vacuum ejector device
US5779355A (en) * 1997-02-27 1998-07-14 Roger H. Woods Limited Mixing apparatus venturi coupled multiple shear mixing apparatus for repairing a liquid-solid slurry
US6299343B1 (en) * 1997-12-02 2001-10-09 Tivon Co. Method of heating and/or homogenizing of liquid products in a steam-liquid injector
US5863128A (en) * 1997-12-04 1999-01-26 Mazzei; Angelo L. Mixer-injectors with twisting and straightening vanes
US5951922A (en) * 1998-02-10 1999-09-14 Mazzei; Angelo L. Aeration system for substantial bodies of water
US6523991B1 (en) * 1998-07-08 2003-02-25 Jaber Maklad Method and device for increasing the pressure or enthalpy of a fluid flowing at supersonic speed
US6767006B1 (en) * 1999-06-07 2004-07-27 Centro Sviluppo Materiali S.P.A. Device for introducing a gaseous substance in a fluid and use thereof
WO2000074832A1 (en) * 1999-06-07 2000-12-14 Centro Sviluppo Materiali S.P.A. Device for introducing a gaseous substance in a fluid and use thereof
US6203186B1 (en) * 1999-09-13 2001-03-20 Luis R. Cruz Spherical eductor atomizer
US6623154B1 (en) * 2000-04-12 2003-09-23 Premier Wastewater International, Inc. Differential injector
US20040036185A1 (en) * 2000-04-12 2004-02-26 Premier Wastewater International, Inc. Differential injector
US6877890B2 (en) * 2000-10-30 2005-04-12 Bruce Alan Whiteley Fluid mixer with rotatable educator tube and metering orifices
US20030137897A1 (en) * 2000-10-30 2003-07-24 Whiteley Bruce Alan Fluid mixer with rotatable eductor tube and metering orifices
US7032840B2 (en) 2001-06-08 2006-04-25 Hair Patrol Llc Animal bathing system
US20060157586A1 (en) * 2001-06-08 2006-07-20 Freidell James E Animal bathing system
US20030024485A1 (en) * 2001-06-08 2003-02-06 Freidell James E. Animal bathing system
US7614570B2 (en) 2001-06-08 2009-11-10 Hair Patrol Llc Animal bathing system
US6796772B2 (en) * 2001-07-06 2004-09-28 Tokico Ltd. Ejector and negative-pressure supply apparatus using the same
DE10230142B4 (en) * 2001-07-06 2009-09-10 Hitachi, Ltd. Feeding device for negative pressure with an ejector
US20030007874A1 (en) * 2001-07-06 2003-01-09 Junichi Ikeda Ejector and negative-pressure supply apparatus using the same
US20040141410A1 (en) * 2002-02-01 2004-07-22 Fenton Marcus B M Fluid mover
EP1499447A1 (en) * 2002-04-30 2005-01-26 Avrom R. Handleman Eductor mixer system
EP1499447A4 (en) * 2002-04-30 2006-06-07 Handleman Avrom Ringle Eductor mixer system
US20050053887A1 (en) * 2002-06-26 2005-03-10 Per Westergaard Burner fuel mixer head for concurrently burning two gaseous fuels
US7111975B2 (en) * 2002-10-11 2006-09-26 Pursuit Dynamics Plc Apparatus and methods for moving a working fluid by contact with a transport fluid
US20050077057A1 (en) * 2003-10-10 2005-04-14 Hale Products, Inc. Fire truck booster pump
US20050133615A1 (en) * 2003-12-18 2005-06-23 Bowles Fluidics Corporation Fluid injector and mixer apparatus
US7357565B2 (en) 2003-12-18 2008-04-15 Bowles Fluidics Corporation Fluid injector and mixer apparatus
US20080230632A1 (en) * 2004-02-24 2008-09-25 Marcus Brian Mayhall Fenton Method and Apparatus for Generating a Mist
US20070210186A1 (en) * 2004-02-26 2007-09-13 Fenton Marcus B M Method and Apparatus for Generating a Mist
US9010663B2 (en) 2004-02-26 2015-04-21 Tyco Fire & Security Gmbh Method and apparatus for generating a mist
US9004375B2 (en) 2004-02-26 2015-04-14 Tyco Fire & Security Gmbh Method and apparatus for generating a mist
US10507480B2 (en) 2004-02-26 2019-12-17 Tyco Fire Products Lp Method and apparatus for generating a mist
US20080310970A1 (en) * 2004-07-29 2008-12-18 Pursuit Dynamics Plc Jet Pump
US9239063B2 (en) 2004-07-29 2016-01-19 Pursuit Marine Drive Limited Jet pump
US20100129888A1 (en) * 2004-07-29 2010-05-27 Jens Havn Thorup Liquefaction of starch-based biomass
US8419378B2 (en) 2004-07-29 2013-04-16 Pursuit Dynamics Plc Jet pump
US20080219087A1 (en) * 2005-05-20 2008-09-11 Tronox Llc Fluid Mixing Apparatus and Method
US8215825B2 (en) * 2005-05-20 2012-07-10 Tronox Llc Fluid mixing apparatus and method
US20070025862A1 (en) * 2005-07-28 2007-02-01 Graham Corporation Compressible gas ejector with unexpanded motive gas-load gas interface
US20090314500A1 (en) * 2006-09-15 2009-12-24 Marcus Brian Mayhall Fenton Mist generating apparatus and method
US9931648B2 (en) 2006-09-15 2018-04-03 Tyco Fire & Security Gmbh Mist generating apparatus and method
US8789769B2 (en) 2006-09-15 2014-07-29 Tyco Fire & Security Gmbh Mist generating apparatus and method
US7618182B1 (en) * 2007-04-19 2009-11-17 Vortex Systems (International) LI Dust-free low pressure mixing system with jet ring adapter
US8193395B2 (en) 2007-05-02 2012-06-05 Pursuit Dynamics Plc Biomass treatment process and system
US20100233769A1 (en) * 2007-05-02 2010-09-16 John Gervase Mark Heathcote Biomass treatment process
US8513004B2 (en) 2007-05-02 2013-08-20 Pursuit Dynamics Plc Biomass treatment process
US20090240088A1 (en) * 2007-05-02 2009-09-24 Marcus Brian Mayhall Fenton Biomass treatment process and system
CN101737777B (en) * 2008-11-12 2012-10-17 中国市政工程华北设计研究院 Burner used for fuel gas distribution and exchangeability test
US7784999B1 (en) * 2009-07-01 2010-08-31 Vortex Systems (International) Ci Eductor apparatus with lobes for optimizing flow patterns
CN102444626A (en) * 2010-10-08 2012-05-09 康奈可关精株式会社 Jet pump and air conditioner
US20120085124A1 (en) * 2010-10-08 2012-04-12 Tomohiro Maruyama Jet pump and air conditioner
EP2439469A3 (en) * 2010-10-08 2014-01-22 Calsonic Kansei Corporation Jet pump and air conditioner
US20130142007A1 (en) * 2011-11-16 2013-06-06 Basf Se Injector for a Granular Solid
CN104613495A (en) * 2013-10-16 2015-05-13 罗伯特·博世有限公司 Heating device with a burner assisted by a blower
EP2863125A1 (en) * 2013-10-16 2015-04-22 Robert Bosch Gmbh Heating device with a burner assisted by a blower
EP2863120A1 (en) * 2013-10-16 2015-04-22 Robert Bosch Gmbh Heating device with a burner assisted by a blower
CN104613495B (en) * 2013-10-16 2018-11-20 罗伯特·博世有限公司 Heating utensil with the burner supported by air blower
CN104028153A (en) * 2014-05-22 2014-09-10 西安交通大学 Rotating Venturi mixer with uniform plate
CN104028153B (en) * 2014-05-22 2015-11-25 西安交通大学 A kind of rotatable and with the venturi mixer of uniformity plate
US20210046434A1 (en) * 2016-03-23 2021-02-18 Alfa Laval Corporate Ab Apparatus for dispersing particles in a liquid
US10625221B2 (en) * 2016-08-11 2020-04-21 Evan Schneider Venturi device
US20180043319A1 (en) * 2016-08-11 2018-02-15 Evan Schneider Venturi device
WO2018217711A1 (en) * 2017-05-22 2018-11-29 Vayu Global Health Innovations, LLC An adjustable ambient air-oxygen blender
CN110662574A (en) * 2017-05-22 2020-01-07 瓦优全球健康创新有限责任公司 Adjustable ambient air-oxygen mixer
US11524132B2 (en) 2017-05-22 2022-12-13 Vayu Global Health Innovations, LLC Adjustable ambient air-oxygen blender
CN110662574B (en) * 2017-05-22 2023-02-17 瓦优全球健康创新有限责任公司 Adjustable ambient air-oxygen mixer
US10596530B2 (en) * 2017-07-19 2020-03-24 Chapin Manufacturing, Inc. Variable venturi device with adjustable valve stem
US11673104B2 (en) * 2018-12-07 2023-06-13 Produced Water Absorbents Inc. Multi-fluid injection mixer and related methods
CN117101997A (en) * 2023-09-06 2023-11-24 苏州子高科技有限公司 Drying device for coating equipment
CN117101997B (en) * 2023-09-06 2024-02-06 苏州子高科技有限公司 Drying device for coating equipment

Also Published As

Publication number Publication date
GB1371698A (en) 1974-10-23
FR2130101A1 (en) 1972-11-03
BE764407A (en) 1971-08-16
DK132720C (en) 1976-06-28
FR2130101B1 (en) 1974-12-13
SU469270A3 (en) 1975-04-30
DE2209812A1 (en) 1972-09-28
DK132720B (en) 1976-01-26
PL88978B1 (en) 1976-10-30

Similar Documents

Publication Publication Date Title
US3799195A (en) Device for controlling a mixture of two gases
US3524344A (en) Apparatus for testing carburetors
GB1508051A (en) Combustion apparatus
GB1328915A (en) Apparatus for uniformalizing the flow of a fluid
US3255966A (en) Annulus type burner for the production of synthesis gas
US2564306A (en) Apparatus for proportionally blending liquids
US2600733A (en) Gas mixing apparatus
SE8008941L (en) SET FOR PARTIAL OXIDATION OF SOLID CARBON FUEL AND BURNER HERE
DE3471352D1 (en) Plug valve
GB944445A (en) Combustion apparatus for the combustion of gaseous and liquid fuels
US2321483A (en) Proportional mixer
US2912011A (en) Valve structure
ATE9732T1 (en) DEVICE FOR ADJUSTING THE QUANTITY AND/OR THE RATIO OF TWO FLOW OF GAS AND/OR LIQUID.
US3733902A (en) Minimum length high quality differential pressure producing flow meter
GB1484489A (en) Device for mixing fluids
GB1140837A (en) Method and apparatus for mixing streams of gas
GB1174654A (en) Apparatus for Mixing Fluids
GB1332065A (en) Burner construction for a flame spectrophotometer
US3538933A (en) Fluid mixing device
Walker et al. Investigation of the ignition properties of flowing combustible gas mixtures
US3187560A (en) Extensometers
US2645124A (en) Flowmeter for gases
RU1831620C (en) Flowmeter
SU945553A1 (en) Three-wave distribution valve
SU1657951A1 (en) Pneumatic device for inside taper checking