US1733413A - Atomizer - Google Patents

Atomizer Download PDF

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Publication number
US1733413A
US1733413A US133613A US13361326A US1733413A US 1733413 A US1733413 A US 1733413A US 133613 A US133613 A US 133613A US 13361326 A US13361326 A US 13361326A US 1733413 A US1733413 A US 1733413A
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United States
Prior art keywords
tube
air
housing
cone
section
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Expired - Lifetime
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US133613A
Inventor
Kay Oscar
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.)
BERTHA RYAN
EVA R PHIPPS
HOLLY C PHIPPS
Original Assignee
BERTHA RYAN
EVA R PHIPPS
HOLLY C PHIPPS
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Application filed by BERTHA RYAN, EVA R PHIPPS, HOLLY C PHIPPS filed Critical BERTHA RYAN
Priority to US133613A priority Critical patent/US1733413A/en
Application granted granted Critical
Publication of US1733413A publication Critical patent/US1733413A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • 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
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour

Description

O. KAY
ATOIII ZER Qrwcntoc 05eme Kay Oct. 29, 1929.
Filed Sept. 4, 1926 Patented Oct. 29, 1929 UNITED STATES PATENT OFFICE OSCAR KAY, OF LOS ANGELES, CALFORNIA, ASSIGNOR OF ONE-TENTH TO BERTI-.IA RYAN, ONE-TVENTIETI-I TO HOLLY C. PHIPPS AND ONE-TWENTIETH TO EVA R.
PHIPPS, ALL GF LGS ANGELES,
CALIFORNIA ATOMIZER Application filed September 4, 1926.
ing of liquid fuels such as crude oil or other hydrocarbons, and by which a'thorough atomizing of t-he fuel and intimate mixing thereof with air will be eected, and the mixture ejected from the atomizer at a high velo locity, to the end that a highly combustible mixture will be obtained, which when burned will produce a practically complete combustion.
Other objects and advantages will become '15 apparent as the description proceeds.
In the accompanying drawings,
Figure 1 is a vertical longitudinal section through the atomizer;
Figure 2 is a section on line 2 2 of Fig- 2o ure 1.
In order to effect disintegration of the oil through an atomizing process, use is made of an atomizer including a housing 11 closed at one end by a cap 12, and provided at one side preferably adjacent to said cap with an inlet opening 102L in order that air under suitable pressure may be introduced to said housing. Located within the housing is a nozzle 13 comprising a rotary section 14 and a staec tionary section15. The stationary section 15 is formed with a cylindrical enlargement 16 and a reduced branch 17, in which latter is formed a bore 13. The branch 17 is threaded into the head 12 axially thereof, and same finds connection with an cil supply pipe 19.
bers 24-24 are spaced apart by a sleeve 26 and, as illustrated, said members are mounted on the hollow tube 27 of the revolving section of said nozzle 13. The forward end of the tube 27 is shouldered at 28 and the rear end if threaded to receive a clamp nut 29, whereby Serial N0. 133,613.
the members 24-24 are held fast to the tube Screwed or otherwise suitably secured to the revolving sect-ion 14 of the nozzle is an impact member 30 comprising integral, respectively graduated, frusto- conical cones 31 and 32, the largest diameter of the cone 32 being slightly less than the internal diameter of the forward end of the aforementioned housing 11 so that an annular space 33 is formed therebetween.
lVithin the cylinder 16 axially of the tube 27 is a jet pipe 33LL closed at its forward end at 34 and provided liust rearward of said forward end with a radial orifice 35 which opens toward the extreme inner or reduced end of the cone 31. The rear end of the jet pipe opens to the bore 18 which leads to the source of fuel supply.
Extending through the tube 27 in spaced relation to the walls thereof is an air tube 36 whose forward end extends beyond the closed end 34 of the tube 27, and whose rear end extends into the housing 11 where it opens thereto. Mounted on the revolving section 14 of the nozzle 13 is an impeller 37 having radial blades 38.
The forward or enlarged end of the cone 31 is arranged in overlapped relation to the walls of the cone 32 at the small end of the latter.
00M decomposition I have described the characterizing instrumentalities of means or mechanism for effecting decomposition of petroleum with the consequent breaking up of the molecules and the production'of both lighter and heavier hydrocarbons, called cracking7 and the manner of functioning of the partslis set forth as follows: A
' Crude petroleum under pressure is admitted to the nozzle 13. Air under suitable pressure is admitted to the housing 11 by way of the intake opening 10a. The petroleum is fed through the jet tube 27 where it finds escape by way of the orifice 35. From said orifice, the petroleum is forced against the impact surface of the small end of the cone 31. During the operation of continuously feeding the petroleum through the nozzle, the f function of the respective cones 31 and 32 is to set up rotation of the petroleum within said cones or to impart thereto a whirling motion. This causes a bombardment of the petroleum against the entire inner wall1 sur.- faces of said conesto the end that the molecules are thoroughly broken up. The overlapped relationof the respective cones serves toY further augment. the decomposing action. as the fluid leaves the small' cone and enters the large one. As the parts function in the manner aforementioned, air under press-urefrom the tube 36 and the opening l0a is drawn into the small end of'th'e cone 3l; whene it emerges axially thereof from in front of the closed end: 342 of thejet'pipe; Il find'th'at the air mixing with the elements wit-hin the" conesll and)J additionally lendsto'the'effect of t'hecon'es toward rapidi decomposition of.Y the elements.
Incident to'the'fact'thatfair. under pressureV is constantly entering the housing 1L itt manifestly followsfth'at' this airactsto' drive the impeller 37 to effect rotation.e of he nozzle portion 14 anditscones 3l and 32. Blast iniduced at the space between'the lange end of the cone 32.- and the forward endaof the housing. l'l assists the decomposing-action;-v
Due'to the fact'that the'initiahdischarge.of the petroleum isin af radial directioni at* the innerendofY the coneY 3L, thev impact action; herein referred to is-progressively augmented sothat when the elementsreach'the'large dis charge end of the cone 32 a completecrack V ing` of. theI oilz' hasrbeeneffected and.y by the action of; the air from` openingsV 10a-supplementediby thefprevailingfgeffect of air issuing from -the pipe/36., the 'decomposedpetroleum is expelled spray-like from.l saidf cone."
Although I: have herein shown and' dejscribed4 only on e'f'orm of: atomilZen-embodying my invention, it is to be understoodthatvarouschanges and:modii'ca-tionsmayl be -made thereinxfwithout departing from ther spirit' of the `vinvent-ion andA the spirit and! scope of the appended claim.
I claim as my invention z Anf atomizercomprising; an: elongated' cylindricalihous-ing open atone-end andclosedi at itss'other, the'housinghaviiigran air-inlet adjacent its closed endg alnozz'le in the-housing' comprisingI a tubular stationaryvr sectionY having; a` reduced' portion secured axially toI the closed endfof the housings-and 'anenlarged:v cylindrical portion, a plug threaded into the cyl indiical-port'ion, the nozzle including arotatable section' comprising; abar-rel: rotatably mounted axially in the cylindrical portion'of: the stationary Section5 anV impact: member comprising a plurality of frusto-conical elements of graduated diameters secured to thef forward end ofthe barrel, Vthe larger endof the' largest elementi being slightlyy smaller than the internal diameter of thehousing so-y as 1to 'provide an annular;airpassage betvveen the two, an impeller secured to the rotatable section between the forward end of the stationary section and the smallest frusto-conical element and operating to rotate the rotatable'section in responseto air Vunder pressure admitted-tothe housing through its inlet, a fuel tube axially of and in spaced relation to the barrel, the forward end of the tube being. closed and extendinginto the rearmost frusto-conical element, aradial' port in the tube adjacent its forward' end, the rear end of the tube being secured in said plug and communicating with the interior of the reduced portion ofthe stationary section so that fuel under pressure admitted to the latter willzbe dischangedathrough said port, radially againstI the` smallest element,` and:y an open-` ended air tube axially off and'in' spaced relation to the fuel tube, the rear end of the airlt'ube being angularly disposed and projecting lthrough the'wall of the. reducedportion ofi the stationary section, for communication: with the interior ofl the housing, the forward? end of the air tube projecting through the closed end of the fuel tube into the?fi'nsto-conical elements so that air from thehousing will bedeliveredaxially into the elements.
' OSCAR.- KAY.
US133613A 1926-09-04 1926-09-04 Atomizer Expired - Lifetime US1733413A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457067A (en) * 1938-04-26 1948-12-21 Perretti Attilio Atomizing oil burner
US2474020A (en) * 1946-06-25 1949-06-21 Shell Dev Liquid fuel burner with rotatable atomizing cup
US2535316A (en) * 1940-07-29 1950-12-26 Cryptoteknik Ab Rotary vaporizing type burner with carbon removal means
US2597916A (en) * 1946-07-29 1952-05-27 William Earl Anderson Material feeder and hydrator
DE1060193B (en) * 1954-09-10 1959-06-25 Henschel & Sohn Gmbh Rotating burner for combustion chambers of gas turbines

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457067A (en) * 1938-04-26 1948-12-21 Perretti Attilio Atomizing oil burner
US2535316A (en) * 1940-07-29 1950-12-26 Cryptoteknik Ab Rotary vaporizing type burner with carbon removal means
US2474020A (en) * 1946-06-25 1949-06-21 Shell Dev Liquid fuel burner with rotatable atomizing cup
US2597916A (en) * 1946-07-29 1952-05-27 William Earl Anderson Material feeder and hydrator
DE1060193B (en) * 1954-09-10 1959-06-25 Henschel & Sohn Gmbh Rotating burner for combustion chambers of gas turbines

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