US2079430A - Oil burner device - Google Patents

Oil burner device Download PDF

Info

Publication number
US2079430A
US2079430A US734916A US73491634A US2079430A US 2079430 A US2079430 A US 2079430A US 734916 A US734916 A US 734916A US 73491634 A US73491634 A US 73491634A US 2079430 A US2079430 A US 2079430A
Authority
US
United States
Prior art keywords
opening
liquid
space
whirling
spray
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
US734916A
Inventor
Bargeboer Adolf
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 US734916A priority Critical patent/US2079430A/en
Application granted granted Critical
Publication of US2079430A publication Critical patent/US2079430A/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
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/38Nozzles; Cleaning devices therefor
    • F23D11/383Nozzles; Cleaning devices therefor with swirl means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/162Means to impart a whirling motion to fuel upstream or near discharging orifices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/24Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
    • F23D11/26Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space with provision for varying the rate at which the fuel is sprayed
    • F23D11/28Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space with provision for varying the rate at which the fuel is sprayed with flow-back of fuel at the burner, e.g. using by-pass

Definitions

  • This invention relates to a liquid sprayin device in which liquid is forced by pressure through channels which are tangentially arranged to a socalled whirling space.
  • the present invention eliminates these objections by producing in the central part of the whirling space a cavity, so that the liquid emerges as a rapidly rotating film and by break a ing up this film into a very fine mist.
  • the spray-opening has a sharp 5 edge.
  • FIG. 1 is a diagrammatic section of the tip of the atomizer
  • Fig. 2 is a top view of element 2 of Fig. 1;
  • Fig. 3 is a longitudinal section of the atomizer
  • Figs. 4 and 4A are, respectively, a longitudinal section and a top view of elements 31, 22 of Fig. 3.
  • Nozzle I has a spray-opening 5 having a sharp edge and has a. diameter d.
  • the conical part l2 of nozzle l forms, together with the fiat part 4 45 of bushing 2, a whirling space 9.
  • the channels formed by the grooves 3 of the cone-shaped part of element 2 lead tangentially into this space.
  • a bore 1 through bushing 2" has-an opening 5 of diameter D.
  • the bore is opposite opening 50 5, D being larger than d and smaller than /gjof,
  • the liquid forms a hollow curved surface, emerging over the edge of opening 6.
  • the liquid does not emerge as a. jet, but only as a quickly rotating film. Since there are no particles in the center where the centrifugal force is too small, this rotating conical film spreads out intoa very fine mist.
  • Fig. 1 shows schematically this condition.
  • the central space is at I0 (cavity), free of liquid.
  • the hollow space II is formed owing to the rapid spinning of the fluid which escapes through the opening 6 and bores l and 8. This will force a rapidly rotating thin film of liquid through opening 5.
  • the mist emerges in the form. 01" a cone ll. It is very important that the whirling space 9 debouch into the spray-opening 5 over a cone l2, or other converging surface.
  • the channels 3 remain unchanged and that the spaces 8 and I 3 be separated.
  • the tangential channels 3 have a direction with an axial component.
  • Fig. 3 The construction shown in Fig. 3 meets these requirements.
  • the spray-opening 5 is arranged in plate 32, which is held by means of nut 29 centered with respect to part 361), which in turn is held centered in head (36a) by means of nut 26.
  • the unit 29 is held in place on the assembly by means of a screw 29a passing through the head of sleeve 26.
  • Diaphragm 22 40 (see Fig. 4) is clamped between 36a and "D.
  • Diaphragm 22 has six holes which permit communication through two circumferential grooves in 36a and 36b between the supply-opening 20 and channel 24 and supply-chamber l3.
  • the liquid flows from chamber l3 through the tangential grooves 3 on the conical part of the frontal surface of cylinder 31 to the whirling space which is formed by the other part of the frontal surface of cylinder 31 with plate 32.
  • the ⁇ diaphragm 22 is held 'tightj between the shoulder of cylinder 31 and nut 28 'so that space 3 .is hermetically separated from the supply-space II. Owing'to' the flexibilityofdiaphragm .2 ndthe clearance in the central hole of the diapliragmj'li'.
  • said whirling chamber having a relatively small spray opening and a second relatively large opening centrally located therein opposite the spray opening, said second opening being substantially less in diameter than said whirling chamber, a third chamber, a fuel return channel connecting the second opening with the third chamber to the supply chamber.

Description

I May 4, 1937. A. BARGEBOER 2,079,430
on. BURNER DEVICE Filed July 15, 1954 F/q:4 Adali- Bav eboer INVENTOI'E.
Patented May 4, 1937 UNITED .STATES,
PATENT OFFICE 3 Claims.
This invention relates to a liquid sprayin device in which liquid is forced by pressure through channels which are tangentially arranged to a socalled whirling space. The
5 liquid flowing tangentially into this whirling space will rapidly rotate. v
Since in a rotating =-frictionless fluid the product of velocity and radius of every particle has a constant value (r v=constant), the speed of lo rotation is increased by the spiral flow towards the centre of the whirling space, whereby the liquid will emerge in the form of a rapidly rotating liquid-jet from a central spray opening in the whirling space.
18 Centrifugal force breaks up the jet into mist consisting mostly of fine particles. The central part of the mist-cone will, however, be rich in coarser particles because the centrifugal force in the center of such a jet is insufilcient to produce 20 fine particles.
The present invention eliminates these objections by producing in the central part of the whirling space a cavity, so that the liquid emerges as a rapidly rotating film and by break a ing up this film into a very fine mist.
This is accomplished by arranging in the surface opposite the spray-opening an opening opposite the spray-opening, the diameter of which is less than of the diameter of the whirling 30 space and larger than the spray-opening, and
which is connected with a return-lead for returning a part of the liquid suppiled to the whirling space.
Furthermore, the spray-opening has a sharp 5 edge.
In the drawing Fig. 1 is a diagrammatic section of the tip of the atomizer;
Fig. 2 is a top view of element 2 of Fig. 1;
Fig. 3 is a longitudinal section of the atomizer;
4 Figs. 4 and 4A are, respectively, a longitudinal section and a top view of elements 31, 22 of Fig. 3.
Nozzle I has a spray-opening 5 having a sharp edge and has a. diameter d. The conical part l2 of nozzle l forms, together with the fiat part 4 45 of bushing 2, a whirling space 9. The channels formed by the grooves 3 of the cone-shaped part of element 2 lead tangentially into this space.
A bore 1 through bushing 2"has-an opening 5 of diameter D. The bore is opposite opening 50 5, D being larger than d and smaller than /gjof,
the diameter of 4.
The operation is as follows: the liquidflowing through the tangentially arranged channels 3 at high velocity and tangentially to the whirling" I space 9, maintains the liquid which is spirally supplied to this whirling space in a very rapid rotation. When it reaches the circumference of opening 6, part of the liquid flows always rotating through bore 1 to space 8 and flows back to a space of lower pressure i. e. through a pressure 5 regulating valve to the liquid-reservoir. v
Owing to this rotating movement and rather I sharp direction-change, the liquid forms a hollow curved surface, emerging over the edge of opening 6. There is no liquid in the center of the 10 whirling space so that when it reaches the smaller spray-opening, the liquid does not emerge as a. jet, but only as a quickly rotating film. Since there are no particles in the center where the centrifugal force is too small, this rotating conical film spreads out intoa very fine mist.
Fig. 1 shows schematically this condition. The central space is at I0 (cavity), free of liquid.
The hollow space II is formed owing to the rapid spinning of the fluid which escapes through the opening 6 and bores l and 8. This will force a rapidly rotating thin film of liquid through opening 5. The mist emerges in the form. 01" a cone ll. It is very important that the whirling space 9 debouch into the spray-opening 5 over a cone l2, or other converging surface.
Furthermore, it isof great importance that the channels 3 remain unchanged and that the spaces 8 and I 3 be separated. In many cases it 3 is preferred that the tangential channels 3 have a direction with an axial component.
The construction shown in Fig. 3 meets these requirements. Here the spray-opening 5 is arranged in plate 32, which is held by means of nut 29 centered with respect to part 361), which in turn is held centered in head (36a) by means of nut 26. The unit 29 is held in place on the assembly by means of a screw 29a passing through the head of sleeve 26. Diaphragm 22 40 (see Fig. 4) is clamped between 36a and "D. Diaphragm 22 has six holes which permit communication through two circumferential grooves in 36a and 36b between the supply-opening 20 and channel 24 and supply-chamber l3. The liquid flows from chamber l3 through the tangential grooves 3 on the conical part of the frontal surface of cylinder 31 to the whirling space which is formed by the other part of the frontal surface of cylinder 31 with plate 32. The {diaphragm 22 is held 'tightj between the shoulder of cylinder 31 and nut 28 'so that space 3 .is hermetically separated from the supply-space II. Owing'to' the flexibilityofdiaphragm .2 ndthe clearance in the central hole of the diapliragmj'li'.
around the screw holding, cylinder 31, the cen- 'tering of the cylinder 31 'on'plate 32 is not disturbed. The liquid supplied under pressure at 20, flows through 24, I3, grooves 3, to the whirling space. The part which'is' not atomized returns through bore 1, chamber 39, channel l8 and connection I'l.
By this arrangement it is possible to regulate the atomized quantity of liquid is a very simple fashion. If the pressure of the liquid returning through i is varied, then the diameter of the cavity within the spinning fluid in the whirling space will also change, and consequently the thickness of the film to be atomized emerging from the opening 5 increases with the increase in the thickness of this film. The atomized quantity of liquid will increase at increasing pressure in I and will diminish at decreasing pressure in I. On the other hand, the speed of rotation will increase at increasing pressure in the annular passage i3 in response to the adjustment of the pressure regulator, and consequentlythe' diameter of III will increase, whereby the atomized quantity of liquid diminishes. As the liquid whirls faster in 9 the hollow space I!) grows wider and the liquid film issuing from opening 5 grows thinner, whereby the quantity of atomized fluid iS diminished,
1 channels leading from the pressure chamber to the whirling chamber, said whirling chamber having a relatively small spray opening and a second relatively large opening centrally located therein opposite the spray opening, said second opening being substantially less in diameter than said whirling chamber, a third chamber, a fuel return channel connecting the second opening with the third chamber to the supply chamber.
2. A device according to claim 1 and in which the diameterof the second opening is less than three-fourths of the diameter of the whirling chamber. V
3. A device according to claim 1 and in which the tangential channels have an axial component. l
ADQLF BARGEBOER.
US734916A 1934-07-13 1934-07-13 Oil burner device Expired - Lifetime US2079430A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US734916A US2079430A (en) 1934-07-13 1934-07-13 Oil burner device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US734916A US2079430A (en) 1934-07-13 1934-07-13 Oil burner device

Publications (1)

Publication Number Publication Date
US2079430A true US2079430A (en) 1937-05-04

Family

ID=24953575

Family Applications (1)

Application Number Title Priority Date Filing Date
US734916A Expired - Lifetime US2079430A (en) 1934-07-13 1934-07-13 Oil burner device

Country Status (1)

Country Link
US (1) US2079430A (en)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2549092A (en) * 1943-10-19 1951-04-17 Sulzer Ag Burner for liquid fuels
US2561939A (en) * 1948-12-30 1951-07-24 A V Roe Canada Ltd Dual spray nozzle for fuel burners
US2566532A (en) * 1947-08-20 1951-09-04 Delavan Mfg Company Combustion spray nozzle
US2567818A (en) * 1949-05-17 1951-09-11 Jet Heet Inc Liquid fuel nozzle
US2578272A (en) * 1947-12-13 1951-12-11 Power Jets Res & Dev Ltd Liquid fuel burner
US2579215A (en) * 1947-10-27 1951-12-18 Shell Dev Wide range liquid fuel burner and method for increasing adjustability r ge of whirl-type atomizing burners
US2579829A (en) * 1949-01-10 1951-12-25 Shell Dev Liquid fuel burner with oil precirculation
US2608247A (en) * 1947-01-20 1952-08-26 Dowty Equipment Ltd Fuel supply system for spill type burners
US2613998A (en) * 1948-09-15 1952-10-14 Thompson Prod Inc Variable area fuel nozzle
US2614888A (en) * 1948-10-15 1952-10-21 American Locomotive Co Fuel injector
US2702590A (en) * 1949-09-08 1955-02-22 Eloise B Stillman Liquid fuel circulating system for mechanically atomizing liquid fuel burner and method of controlling the output of said burner
US2715546A (en) * 1949-09-10 1955-08-16 Babcock & Wilcox Co Atomizer
US2757961A (en) * 1950-09-07 1956-08-07 Chrysler Corp Regulated fuel system
US2920831A (en) * 1957-02-28 1960-01-12 Jr Wadsworth J Johnsyn Fuel atomizing nozzle
US3050960A (en) * 1959-09-14 1962-08-28 Jersey Creme Holdings Pty Ltd Soft ice-cream machines
US3819116A (en) * 1972-07-26 1974-06-25 Plessey Handel Investment Ag Swirl passage fuel injection devices

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2549092A (en) * 1943-10-19 1951-04-17 Sulzer Ag Burner for liquid fuels
US2608247A (en) * 1947-01-20 1952-08-26 Dowty Equipment Ltd Fuel supply system for spill type burners
US2566532A (en) * 1947-08-20 1951-09-04 Delavan Mfg Company Combustion spray nozzle
US2579215A (en) * 1947-10-27 1951-12-18 Shell Dev Wide range liquid fuel burner and method for increasing adjustability r ge of whirl-type atomizing burners
US2578272A (en) * 1947-12-13 1951-12-11 Power Jets Res & Dev Ltd Liquid fuel burner
US2613998A (en) * 1948-09-15 1952-10-14 Thompson Prod Inc Variable area fuel nozzle
US2614888A (en) * 1948-10-15 1952-10-21 American Locomotive Co Fuel injector
US2561939A (en) * 1948-12-30 1951-07-24 A V Roe Canada Ltd Dual spray nozzle for fuel burners
US2579829A (en) * 1949-01-10 1951-12-25 Shell Dev Liquid fuel burner with oil precirculation
US2567818A (en) * 1949-05-17 1951-09-11 Jet Heet Inc Liquid fuel nozzle
US2702590A (en) * 1949-09-08 1955-02-22 Eloise B Stillman Liquid fuel circulating system for mechanically atomizing liquid fuel burner and method of controlling the output of said burner
US2715546A (en) * 1949-09-10 1955-08-16 Babcock & Wilcox Co Atomizer
US2757961A (en) * 1950-09-07 1956-08-07 Chrysler Corp Regulated fuel system
US2920831A (en) * 1957-02-28 1960-01-12 Jr Wadsworth J Johnsyn Fuel atomizing nozzle
US3050960A (en) * 1959-09-14 1962-08-28 Jersey Creme Holdings Pty Ltd Soft ice-cream machines
US3819116A (en) * 1972-07-26 1974-06-25 Plessey Handel Investment Ag Swirl passage fuel injection devices

Similar Documents

Publication Publication Date Title
US2079430A (en) Oil burner device
US2592297A (en) Arrangement for atomizing liquids
US2703260A (en) Dual orifice atomizing nozzle
US3084874A (en) Method and apparatus for generating aerosols
US2055864A (en) Atomizing nozzle
US2904263A (en) Liquid spray nozzle
US2878065A (en) Liquid fuel discharge nozzles
US2410215A (en) Spray nozzle
US2984420A (en) Aerosol devices
US2984421A (en) Adjustable aerosol device
US1934837A (en) Liquid fuel burner or atomizer
US2503481A (en) Atomizing nozzle
RU2560239C1 (en) Kochetov's centrifugal vortex burner
US2530206A (en) Spray gun
US2974881A (en) Fuel injection nozzle
US2373707A (en) Atomizer
US3022954A (en) Variable area valve
US1919027A (en) Atomizer
US2801881A (en) Open orifice nozzle and valve
US2668084A (en) Atomizing device
US2237842A (en) Spraying device
US2235708A (en) Spraying device
US2323001A (en) Liquid spraying device for liquid fuel burners
US2243995A (en) Nozzle
US3301490A (en) Multiple outlet water discharge head with internal flow distributing baffle