[go: up one dir, main page]

US2559792A - Rotary atomizing liquid fuel burner - Google Patents

Rotary atomizing liquid fuel burner Download PDF

Info

Publication number
US2559792A
US2559792A US43843A US4384348A US2559792A US 2559792 A US2559792 A US 2559792A US 43843 A US43843 A US 43843A US 4384348 A US4384348 A US 4384348A US 2559792 A US2559792 A US 2559792A
Authority
US
United States
Prior art keywords
liquid fuel
fuel
rotary atomizing
fuel burner
atomizing liquid
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
US43843A
Inventor
Pietri Francois
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
Application granted granted Critical
Publication of US2559792A publication Critical patent/US2559792A/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
    • F23D11/04Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying action being obtained by centrifugal action

Definitions

  • the directing blades, fans and the like auxiliaries may thus be done away with which removes any causes of stoppage, inspection and upkeep.
  • the atomization and blowing of air for combustion is obtained through the rotation of the diffuser itself and consequently the intensity of heating may be reduced without any reduction in efficiency, the amount of air required for combustion and its turbulence being adjusted in proportion to the amount of fuel ejected.
  • the adjustment of this arrangement may be obtained either automatically or by hand.
  • Fig. 1 is a longitudinal cross sectional view of the burner.
  • Fig. 2 is a diagrammatic front view of the same apparatus.
  • the fuel oil burner according to my invention includes an elongated casing I provided at its rear end with air intake apertures 2 and 3 together with means for feeding fuel including a channel 4 the flow through which is adjustable by operation of the needle valve 5. At the other end is an outlet for fuel and air.
  • the longitudinal fuel oil feeding pipe 5 fed by the channel 4 is held stationary by means of a sleeve l secured by a safety nut 8.
  • the outer end of said pipe 5 carries a stationary radially opening distributing fuel outlet nozzle 9 beyond which is secured an inner diffuser member Hi held in position by the fastening screw I I.
  • This diffuser member 10 may be locked or left free to move.
  • the front end of the stationary pipe 6 fed by the channel 4 serves as a shaft carrying rotatably the supporting sleeve [2 for the outer rotary diffuser member l3 having a widened portion surrounding the inner difiuser member [0 and en- 1 Claim. (01. 15847) closing same throughout its operative diffusing surface to form an annular passage into which the outlet nozzle 9 opens.
  • This supporting sleeve I2 is held in position by a thrust ring M at one end and by the distributing nozzle 9 forming a flange at the other end of the sleeve rigid with the rotary diffuser member.
  • the rotation of the outer diffuser member is obtained through any suitable means such as a gear wheel or a pulley as shown at IS.
  • the rotary diffuser member l3 carries on its outer surface helicoidally-arranged blades or fins IS, the pitch of which is suitably chosen for producing an air sucking and propelling action. Said blades cooperate with other stationary helicoidally-arranged blades i'i arranged symmetrically and secured on the inner periphery of the outer end of the casing l in corresponding positions axially of the casing, to the rotating blades and spaced with a radial clearance therefrom. Consequently the liquid fuel fed by the stationary pipe 6 is distributed by the distributing nozzle 9 over the inner wall of the rotary diffuser l3 that forms in association with the stationary or free diffuser l0 an ejection duct promoting turbulence and opening annularly at [8.
  • the fuel oil assumes a rapid rotation so that with the action of centrifugal force it receives a molecular eddying motion and is immediately thrown outwardly by centrifugal force and stirred inside the mass of air sucked in and projected by the air propelling and guiding blades I5.
  • the latter stir the ejected fuel oil and produce thus an inflammable mixture producing a highly homogeneous flame and allowing a great adaptability of combustion. It is also possible to obtain an adjustment of the intensity and length of the flame through the speed of rotation whereby the ejection of the liquid will always be proportional to the turbulence imparted to the air.
  • the diffuser member l3 may be adjusted by means of a brake acting either on the rotary surfaces and controlled through the inside of the pipe 6 or directly on the supporting sleeve l2.
  • a lubricator I9 is provided for the lubrication of the movable members.
  • a fuel oil burner comprising an elongated casing having inlet apertures at one end thereof and an outlet at the other end thereof, a stationary fuel oil feeding pipe longitudinally arranged in said casing, a stationary radially-opening fuel outlet nozzle in the outlet end of said pipe, a cylindrical inner diffuser member also arranged at the outlet end of the pipe and beyond the said nozzle, a rotatable cylindrical outer diffuser member, carried on said pipe as a bearing, having a widened portion surrounding the said inner diffuser member and forming therewith an annular passage into which the fuel outlet nozzle opens, helicoidally-arranged rotating blades arranged along the length of and carried by the widened portion of the rotatable outer diffuser member, other stationary helicoidallyarranged blades secured on the inside of the outlet end of the casing in corresponding positions axially of the casing to the rotating blades and spaced with a radial clearance therefrom, whereby the rotating blades cause an axial air current through the casing towards the outlet end thereof, said

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)

Description

July 10, 1951 F. PIETRI ROTARY ATOMIZING LIQUID FUEL BURNER Filed Aug. 12, 1948 Q l ll 9 Q 2 0 mm Q O\ N 1| 0 Q Q [1| I I I I INVENTOR. mAlvgols P/URI.
A T TORNE YS Patented July 10, 1951 UNITED STATES PATENT OFFICE ROTARY ATOMIZING LIQUID FUEL BURNER Francois Pietri jAubagne, France Application August 12, 1948, Serial No. 43,843
In France August 13, 1947 My invention has for its object improvements in the means used for ejecting liquid fuel chiefly fuel oil and admixing same with air in order to produce a turbulence bestowing a maximum efficiency for the mixture of the two constituents. This result is obtained by means of structural embodiments that include chiefly the incorporation in a rotary diffuser of fins or blades rigid therewith and arranged at a predetermined angle along a helical or the like pitch; said arrangement produces through its mere rotation not only the ejection of the liquid fuel but also a turbulence without the assistance of any fan, which turbulence furthers the mixture and gives the flame a highly efficient adaptability.
The directing blades, fans and the like auxiliaries may thus be done away with which removes any causes of stoppage, inspection and upkeep. The atomization and blowing of air for combustion is obtained through the rotation of the diffuser itself and consequently the intensity of heating may be reduced without any reduction in efficiency, the amount of air required for combustion and its turbulence being adjusted in proportion to the amount of fuel ejected. The adjustment of this arrangement may be obtained either automatically or by hand.
In the accompanying drawings showing diagrammatically by way of example one of the forms of construction of my invention:
Fig. 1 is a longitudinal cross sectional view of the burner.
Fig. 2 is a diagrammatic front view of the same apparatus.
The fuel oil burner according to my invention includes an elongated casing I provided at its rear end with air intake apertures 2 and 3 together with means for feeding fuel including a channel 4 the flow through which is adjustable by operation of the needle valve 5. At the other end is an outlet for fuel and air.
The longitudinal fuel oil feeding pipe 5 fed by the channel 4 is held stationary by means of a sleeve l secured by a safety nut 8. The outer end of said pipe 5 carries a stationary radially opening distributing fuel outlet nozzle 9 beyond which is secured an inner diffuser member Hi held in position by the fastening screw I I. This diffuser member 10 may be locked or left free to move.
The front end of the stationary pipe 6 fed by the channel 4 serves as a shaft carrying rotatably the supporting sleeve [2 for the outer rotary diffuser member l3 having a widened portion surrounding the inner difiuser member [0 and en- 1 Claim. (01. 15847) closing same throughout its operative diffusing surface to form an annular passage into which the outlet nozzle 9 opens. This supporting sleeve I2 is held in position by a thrust ring M at one end and by the distributing nozzle 9 forming a flange at the other end of the sleeve rigid with the rotary diffuser member. The rotation of the outer diffuser member is obtained through any suitable means such as a gear wheel or a pulley as shown at IS.
The rotary diffuser member l3 carries on its outer surface helicoidally-arranged blades or fins IS, the pitch of which is suitably chosen for producing an air sucking and propelling action. Said blades cooperate with other stationary helicoidally-arranged blades i'i arranged symmetrically and secured on the inner periphery of the outer end of the casing l in corresponding positions axially of the casing, to the rotating blades and spaced with a radial clearance therefrom. Consequently the liquid fuel fed by the stationary pipe 6 is distributed by the distributing nozzle 9 over the inner wall of the rotary diffuser l3 that forms in association with the stationary or free diffuser l0 an ejection duct promoting turbulence and opening annularly at [8. The fuel oil assumes a rapid rotation so that with the action of centrifugal force it receives a molecular eddying motion and is immediately thrown outwardly by centrifugal force and stirred inside the mass of air sucked in and projected by the air propelling and guiding blades I5. The latter stir the ejected fuel oil and produce thus an inflammable mixture producing a highly homogeneous flame and allowing a great adaptability of combustion. It is also possible to obtain an adjustment of the intensity and length of the flame through the speed of rotation whereby the ejection of the liquid will always be proportional to the turbulence imparted to the air. The diffuser member l3 may be adjusted by means of a brake acting either on the rotary surfaces and controlled through the inside of the pipe 6 or directly on the supporting sleeve l2. A lubricator I9 is provided for the lubrication of the movable members.
What I claim is:
A fuel oil burner comprising an elongated casing having inlet apertures at one end thereof and an outlet at the other end thereof, a stationary fuel oil feeding pipe longitudinally arranged in said casing, a stationary radially-opening fuel outlet nozzle in the outlet end of said pipe, a cylindrical inner diffuser member also arranged at the outlet end of the pipe and beyond the said nozzle, a rotatable cylindrical outer diffuser member, carried on said pipe as a bearing, having a widened portion surrounding the said inner diffuser member and forming therewith an annular passage into which the fuel outlet nozzle opens, helicoidally-arranged rotating blades arranged along the length of and carried by the widened portion of the rotatable outer diffuser member, other stationary helicoidallyarranged blades secured on the inside of the outlet end of the casing in corresponding positions axially of the casing to the rotating blades and spaced with a radial clearance therefrom, whereby the rotating blades cause an axial air current through the casing towards the outlet end thereof, said air current having a rotary motion imparted to it and being made turbulent I by the coaction one with the other of the stationary and rotating blades, the fuel emerging from the fuel outlet nozzle having a rotary motion imparted to it by the rotation of the outer diffuser member, whereby as the fuel emerges from the annular passage it is thrown outwardly by centrifugal force into the air current the turbulence of which causes thorough mixing of the fuel with the air current.
FRANCOIS PIETRI.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,327,571 Ray Jan. 6, 1920 1,595,931 Fesler Aug. 10, 1926 1,820,758 Miller Aug. 25, 1931 1,979,757 Melot Nov. 6, 1934 2,108,872 Swallow Feb. 22, 1938 2,214,027 McClammy, Jr. Sept. 10, 1940 2,214,568 Thomas Sept. 10, 1940 FOREIGN PATENTS Number Country Date 2,964 Australia July 8, 1927 of 1926 OTHER REFERENCES Great Britain, No. 498,501, printed 1939 (unaccepted patent specification).
US43843A 1947-08-13 1948-08-12 Rotary atomizing liquid fuel burner Expired - Lifetime US2559792A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR2559792X 1947-08-13

Publications (1)

Publication Number Publication Date
US2559792A true US2559792A (en) 1951-07-10

Family

ID=9686507

Family Applications (1)

Application Number Title Priority Date Filing Date
US43843A Expired - Lifetime US2559792A (en) 1947-08-13 1948-08-12 Rotary atomizing liquid fuel burner

Country Status (1)

Country Link
US (1) US2559792A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938345A (en) * 1954-07-27 1960-05-31 Bendix Aviat Corp Combustion fuel atomizer
US4045159A (en) * 1974-07-30 1977-08-30 Mitsubishi Denki Kabushiki Kaisha Combustion apparatus
DE3120637A1 (en) * 1981-05-23 1982-12-16 Ruhrgas Ag, 4300 Essen DEVICE FOR QUANTITY AND / OR RATIO CONTROL OF TWO GAS AND / OR LIQUID FLOWS
EP0057342A3 (en) * 1981-01-31 1983-02-09 Joh. Vaillant Gmbh U. Co Oil evaporation burner

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1327571A (en) * 1919-01-15 1920-01-06 William R Ray Oil-burner
US1595931A (en) * 1924-05-19 1926-08-10 Petroleum Heat & Power Company Oil burner
AU296426A (en) * 1926-07-26 1927-07-19 Charles Fox Frederick Improvements in oil fuel burners
US1820758A (en) * 1929-07-23 1931-08-25 Burrell Engineering & Construc Oil burner
US1979757A (en) * 1932-07-19 1934-11-06 Melot Henri Fabrice Liquid fuel burner
US2108872A (en) * 1936-01-13 1938-02-22 Charies E Swallow Oil burner
US2214027A (en) * 1938-06-07 1940-09-10 Foster Wheeler Corp Burner
US2214568A (en) * 1939-02-17 1940-09-10 Fred P Martin Fuel burner

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1327571A (en) * 1919-01-15 1920-01-06 William R Ray Oil-burner
US1595931A (en) * 1924-05-19 1926-08-10 Petroleum Heat & Power Company Oil burner
AU296426A (en) * 1926-07-26 1927-07-19 Charles Fox Frederick Improvements in oil fuel burners
US1820758A (en) * 1929-07-23 1931-08-25 Burrell Engineering & Construc Oil burner
US1979757A (en) * 1932-07-19 1934-11-06 Melot Henri Fabrice Liquid fuel burner
US2108872A (en) * 1936-01-13 1938-02-22 Charies E Swallow Oil burner
US2214027A (en) * 1938-06-07 1940-09-10 Foster Wheeler Corp Burner
US2214568A (en) * 1939-02-17 1940-09-10 Fred P Martin Fuel burner

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938345A (en) * 1954-07-27 1960-05-31 Bendix Aviat Corp Combustion fuel atomizer
US4045159A (en) * 1974-07-30 1977-08-30 Mitsubishi Denki Kabushiki Kaisha Combustion apparatus
EP0057342A3 (en) * 1981-01-31 1983-02-09 Joh. Vaillant Gmbh U. Co Oil evaporation burner
DE3120637A1 (en) * 1981-05-23 1982-12-16 Ruhrgas Ag, 4300 Essen DEVICE FOR QUANTITY AND / OR RATIO CONTROL OF TWO GAS AND / OR LIQUID FLOWS

Similar Documents

Publication Publication Date Title
US4592202A (en) Thrust augmentor
FI98406C (en) Nozzle
US2559792A (en) Rotary atomizing liquid fuel burner
NO136224B (en)
US3033711A (en) Carbo-blast method and unit
US4270698A (en) Aerosol forming device
US2661195A (en) Method and apparatus for atomizing liquids
US2674494A (en) Shear nozzle for spraying and dusting apparatus
US2325442A (en) Pulverized fuel burner
US2560866A (en) Rotating atomizing cup burner
US2990165A (en) Apparatus for generating foam for use in fire fighting
US3220457A (en) Liquid-fuel smash atomizing and burning apparatus
US3221993A (en) Spraying equipment
US4230449A (en) Self contained compact burner
US1680455A (en) Oil burner
US2359049A (en) Oil burner
US2497480A (en) Air directing means for gun type oil burners
US2202822A (en) Oil burner
US2147053A (en) Cement mixer
US2011606A (en) Oil burner
US2632994A (en) Ram jet engine and flame holder therefor
US4509683A (en) Apparatus for dispersing atomized liquid
US2929442A (en) Combustion system
US1787652A (en) Blower
US2530617A (en) Spiral flame gas burner