US3256003A - Portable oil heater - Google Patents

Portable oil heater Download PDF

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Publication number
US3256003A
US3256003A US317088A US31708863A US3256003A US 3256003 A US3256003 A US 3256003A US 317088 A US317088 A US 317088A US 31708863 A US31708863 A US 31708863A US 3256003 A US3256003 A US 3256003A
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United States
Prior art keywords
air
nozzle
passage
fuel
recess
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
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US317088A
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English (en)
Inventor
Eugene C Briggs
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.)
Koehring Co
MASTER CONSOLIDATED Inc
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MASTER CONSOLIDATED Inc
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 MASTER CONSOLIDATED Inc filed Critical MASTER CONSOLIDATED Inc
Priority to US317088A priority Critical patent/US3256003A/en
Priority to BE652409D priority patent/BE652409A/xx
Priority to DE19641451413 priority patent/DE1451413A1/de
Priority to DE19641776216 priority patent/DE1776216A1/de
Priority to CH1312964A priority patent/CH442659A/de
Priority to NL6411908A priority patent/NL6411908A/xx
Priority to GB42302/64A priority patent/GB1026969A/en
Priority to AT884664A priority patent/AT278224B/de
Application granted granted Critical
Publication of US3256003A publication Critical patent/US3256003A/en
Assigned to KOEHRING COMPANY, A CORP. OF DE reassignment KOEHRING COMPANY, A CORP. OF DE ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: KOEHRING COMPANY A WI CORP.
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00—Subject-matter not provided for in other groups of this subclass
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24H—FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
    • F24H3/00—Air heaters
    • F24H3/02—Air heaters with forced circulation
    • F24H3/04—Air heaters with forced circulation the air being in direct contact with the heating medium, e.g. electric heating element
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24H—FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
    • F24H3/00—Air heaters
    • F24H3/02—Air heaters with forced circulation
    • F24H3/04—Air heaters with forced circulation the air being in direct contact with the heating medium, e.g. electric heating element
    • F24H3/0488—Air heaters with forced circulation the air being in direct contact with the heating medium, e.g. electric heating element using fluid fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24H—FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
    • F24H9/00—Details
    • F24H9/18—Arrangement or mounting of grates or heating means
    • F24H9/1854—Arrangement or mounting of grates or heating means for air heaters
    • F24H9/1877—Arrangement or mounting of combustion heating means, e.g. grates or burners
    • F24H9/1881—Arrangement or mounting of combustion heating means, e.g. grates or burners using fluid fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2700/00—Special arrangements for combustion apparatus using fluent fuel
    • F23C2700/02—Combustion apparatus using liquid fuel
    • F23C2700/023—Combustion apparatus using liquid fuel without pre-vaporising means
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B30/00—Energy efficient heating, ventilation or air conditioning [HVAC]

Definitions

  • a further object of the invention is to provide improvements in heater components.
  • Another object of the invention is to provide a space heater of an extremely compact nature.
  • a further object of the invention is to provide an improved burner unit having particular advantage in application to space heaters.
  • Another object of the invention is to provide a burner unit the construction of which minimizes the need for external piping in application to space heaters.
  • An additional object of the invention is toprovide an improved burner unit for a portable space heater or the like having, integrated therewith, an air compressor and a fan so related to eliminate the extensive hardware normally required for a delivery of air to support combustion.
  • Another object-of the invention is to provide an improved fuel tank for use in portable space heaters and like structure.
  • a further object of the invention is to provide means -for simplifying the interconnection of component portions of a portable space heater.
  • An additional object of the invention is to provide a novel unit which integrates a burner head and a pump.
  • Another object of the invention is to provide improved means for interconnectingsuperposed elements.
  • a further object of the invention is to provide an improved sparking device which enables a W voltage operation of space heaters or like structure.
  • An additional object of the invention is to provide improvements in igniters and ignition systems having a particular advantage in application to space type heaters.
  • Another object of the invention is to provide a more effective means for delivering air to support combustion in a space heater.
  • a further object of the invention is to provide an improved burner head for use in a space heater or the like.
  • Another object of the invention is to provide improvements in sparking devices enabling a maximum spark volume and low voltage operation.
  • Another object of the invention is to provide improvements in combustion chambers and the mount thereof in a portable space heater.
  • An additional object of the invention is to provide heater components and an assembly thereof possessing the advantageous structural features, the inherent meritorious characteristics and the means and mode of operation herein described.
  • FIG. l is a side elevation view of a'portable space heater in accordance with the invention.
  • FIG. 2 is an end View of the device of FIG. l with parts broken away for clarity of disclosure
  • FIG. 3 is a detail View of a burner unit in accordance with the present invention, shown partly in section;
  • FIG. 4 is a view taken on line 4-4 of FIG. 3;
  • FIG. 5 is a frontal view of the burner head incorporated in the burner unit of FIG. 3;
  • FIG. 6 is a fragmentary sectional view illustrating the improved electrode embodied in the present invention.
  • FIG. 7 is a cross-sectional view of the burner head of FIG. 5;
  • FIG. 8 reveals details of the body of the burner head
  • FIG. 9 i-s a top view of the head as shown in FIG. 8;
  • FIG. 10 is a side elevation view of a fuel tank assembly in accordance with the present invention.
  • FIG. 11 is an end view of the tank of FIG. 10;
  • FIG. 12 is a fragmentary view of the fuel tank
  • FIG. 13 is a view of the combustion chamber assembly, as embodied in the device of FIG. 1, and
  • FIG. 14 is a view taken on line 14-14 of FIG. 7, pares being eliminated for clarity of disclosure.
  • a preferred embodiment of the invention as illustrated in the drawings includes a fuel tank 10 fabricatedof two drawn sheet lmetal parts.
  • One forms a generallyv rectangular seamless tray 11, the corners -of which are generally rounded, the other a cap 12.
  • the uppermost wall portion of the tray4 11 has an Outward offset aiording a rim 13 which provides the traywith a horizontal expansion.
  • the cap 12 takes the form of a cover plate which includes, peripherally thereof, a co-extensive, continuous,
  • ange 14 depends immediately about the rim 13 and is secured thereto at spaced intervals by rivnuts 15.
  • the parts 11 and 12 are further bonded and sealed by epoxy resin or an equivalent sealant, the latter being applied between the dependent edge of the flange 14 and the adjacent surface of the rim 13.
  • the invention provides for a very simply effected fuel tank which in the fabrication thereof requires no welding whatsoever.
  • a neck 17 is formed on one end of the cap ⁇ 12 to define a fuel inlet for the tank 10. Spaced longitudinally from the neck 17, towards the center of the cap 12, is a vertically projected boss 18 which-'defines ⁇ a -fuel outlet. Centered on the top of the cap 12, intermediately of the neck 17 and the boss 18, adjacent the later, is a motor mounting bracket 19.
  • the bracket 19 is formed from a single strap of metal. It includes parallel leg portions 20 which so mount to project vertically from the cap 12. As so positioned, the leg portions 20 are bridged to their upper ends by an arcuately concave strap portion 21. To their lower ends, the leg portions 20 each include a right angled foot portion 22 by means Vof which the bracket 19 is secured to the cap 12.
  • the bracket 19 constitutes a motor support, its strap portion 21 supporting the cylindrical housing of a motor 23.
  • Each of the bracket leg portions 20 includes a horizontal slot 24, the slots 24 being in a common plane generally parallel to the upper surface of the cap 12.- Each of the slots 24 receive therethrough a hook extremity 25 of an arcuate strap element 26.
  • the strap elements 26 are so formed to have opposed curvatures whereby to mutually contain the motor housing to the portion 21 of the bracket 19. Their upper relativeiy adjacent extremities 27, which position to the top of the motor 23, are so bent to project .in spaced parallel relation, in a sense vertical to the plane of the cap 12.
  • the portions 27 are conventionally interconnected lby a single screw element 28 to strap the motor 23 in a fixed relation to the bracket 19 and fuel tank 10.
  • the motor 23 is of a conventional nature. It includes a tubular stator housing 30 capped toone end by a plate 31 and to its other end by a plate 32. Its rotor (not shown) embodies a drive shaft 29 the respective ends of which bear in and project through the end plates 31 and 32.
  • the one projected extremity of shaft 29 fixedly mounts a series of blades forming an integrated fan unit 33 adjacent and spaced from the end plate 31. Its other extremity nests in and fixedly mounts a discrtype pump rotor 34.
  • the rotor 34 is so positioned to have one face immediately adjacent the outer face of end plate 32.
  • the rotor 34 is rotatably housed withinan eccentrically disposed ring 35 capped at one face by the end plate 32 and at its outer face by cover plate 36. Together, the ring 35 and the plate 36 comprise a -pump body means. The depth of ring 35 is such to place the plate 36 in immediately adjacent relation to the outermost face of the rotor. l y
  • the rotor 34 is a vaned rotor, the periphery of which includes radially oriented slots 40 spaced 90 apart. Each of the slots 40 nests a relatively slidable vane 41. As may ⁇ be readily seen from FIG. 4 of the drawings, on energizing the motor 23 the shaft 29 will drive the rotor 34 and thereby induce the slidable vanes 41 to successively move outwardly of the rotor periphery to bridge the space between the rotor and the inner surface of the ring 35. The purpose of this structure will soon become obvious. v
  • an L-shaped bracket 42 Fixed to the cap 12 at one side of the motor 23 is an L-shaped bracket 42 (FIGS. 2 and l0).
  • the upper end of the bracket 42 mounts a housing 43 defining an air chamber 44.
  • Theside of the housing 43 which is outermost with reference to the ring 35 is open and bridged by an air filter 45.
  • the ring 35 has a radial aperture 46 accommodating one end of a tube 47.
  • the other end of the tube 47 is fixed to project interiorly of the air chamber 44. Accordingly, on drive of the shaft 29 the vaned rotor will induce static air to be drawn from the vicinity of the air filter 45 interiorly of the housing 43 and through the tube 47 to the compression chamber 48 defined between the periphery of the rotor and the inner wall of the ring 35.
  • the vanes move past the uppermost portion of the ring 35, they will begin to project exteriorly of the rotor, to the extent permitted by its spacing from the inner surface of the ring.
  • each vane As each vane starts to project, it immediately passes the air intake aperture 46 and induces an inflow of air to chamber 48. This air is picked up by the following vane. and carried in advance thereof to move therewith through the initially expanding and then contracting compression chamber 48. As a vane 41 moves past the lowermost portion of ring 35, it moves inwardly of the rotor 34 due to decreasing space between the rotor and the inner surface of the ring. In flow thereof, the air in advance of the retracting vane is then compressed until it reaches a point of access to a discharge opening 49 in the cover plate 36 (FIG. 3).
  • the body 50 Fixed to the plate 36 so as to form an axial extension of the motor 23 and the ring 35 is the body 50 of a burner head 51.
  • the body 50 has a cylindrical form
  • the filter 57 preferably of felt, has an annular form. It includes radially projected, longitudinally oriented ribs 58, the projected extremities of which abut the recess wall 53 to form therewith vertically oriented air passages 59.
  • the recess 54 is capped by an annular plate 60, the open center of which aligns with the open center of filter 57. Suspended ⁇ from the plate 60 to depend interiorly of the filter 57 is a cylindrical housing 62 of a relief valve 63.
  • the housing 62 has a central recess 64 successively stepped inwardly thereof to a conical shoulder 65 about a central opening 66 in its dependent base. Seated on the shoulder 65 is a ball valve element 67.
  • a centrally apertured plug 68 is engaged to the valve housing 62 in the upper end of its recess 64.
  • the inner end of the plug 68 is counter-sunk to nest one end of a coil spring 69 the other end ⁇ of which abuts the ball valve'element 67.
  • the spring 69 applies a bias to normally cause the valve element 67 to tightly seal the relief opening 66 in the bottom of the valve housing 62.
  • the body 50 provides the vburner head 51 with a front operating face 70 having a central recess 71.
  • the base of the recess 71 includes, at its center, a short conical projection 72, the outer end of which terminates short of the operating face 70.
  • the body 50 also includes a central passage or recess 73 having an axial orientation.
  • the passage 73 opens at its outer end through the center of the projection 72 while the inner end thereof terminates within the body 50 at an intersection with a downwardly directed fuel passage 74.
  • the passage 73 has successive reductions in its crosssectional dimension from its outermost end at the projection 72 to its innermost end which intersects and communicates with the passage 74. This reduction provides the passage 73 with successively spaced shoulders 75, 76 and 77, the latter two of which are generally conical in form, relatively closely spaced and adjacent the passage 74.
  • the body 50 also includes a vertical fiow passage 73 providing a direct communica-tion between the recess 54 and the passage 73 in advance of the shoulders 76 and 77.
  • a siphon nozzle 79 Threadedly engaged to the body 50 in the outer end of the recess 73 is a siphon nozzle 79 the head of which abuts the outer extremity of the projection 72.
  • the discharge end of ⁇ the nozzle 79 positions slightly forward of the operating face 70.
  • the nozzle 79 includes a thin tubular shank portion 80 which extends inwardly of the passage 73 to communicate at its innermost extremity with the flow passage 74.
  • its shank portion 80 is reduced in cross-section dimension to provide it with an external shoulder 81. Note that the cross-sectional dimension of the nozzle shank 80,'in any event, is substantially less than that of the passage 73 through which it extends whereby to form about the nozzle shank an air chamber 73 forming part of the passage 73.
  • the shoulder 81 positions coaxial with and in opposed ⁇ spaced relation to the shoulder 76 in the recess 73.
  • a tubular washer 82 mounts about the innermost portion of thenozzle shank 8f) to have its tapered end abut the shoulder 77. The latter is positioned at the inner end of the recess 73 and 'diverted outwardly therefrom to achieve a V-shape.
  • a at washer 83 is positioned about the inner portion of the nozzle shank to have one face thereof in abutment with the shoulder 81 while its other face provides an abutment for one end of a coil spring 84.
  • the other end of the spring 84 which positions generally concentric to the nozzle shank, abuts the outermost end of the washer 82 in the vicinity of the shoulder 76.
  • the washer 82 is of plastically deformable material.
  • the bias of the spring 84 thereon is made suliicient to plastically distort the washer and cause it to expand in a transverse sense and form a seal of the passage 73 about the nozzle shank and preclude the passage of air from the recess 73 to the ow passage 74.
  • the fuel passage 74 functions as a channel for inliow of fuel to the -innermost extremity of the nozzle shank.
  • the nozzle shank defines an interior flow passage P (FIG. 5) which exits from the nozzle head.
  • the head of the nozzle 79 is conventionally formed to include air flow passages inlet ends of which are defined by grooves 85 in the exterior portion of the nozzle shank 80 (FIG. 7). These grooves 85, as will be fur-ther described, provide for a pressurized inflow of air to the interior flow passage of the nozzle 79 in a manner to draw fuel from the tank 10, through the passage 74 and to atomize and entrain such fuel for discharge therewith from the head of the nozzle 79. The discharge occurs at a point directly forward of and in immediately adjacent relation to the operating face 70 of the burner head 51.
  • the flow passage 74 opens from the bottom of the body 50 through a vertically dependent tubular projection 88 accommodating one end of a threadedly engaged tubular adaptor 89.
  • the outermost end of the adaptor 89 is suitably engaged in the discharge end of a fuel hose or pipe 91.
  • the pipe 91 depends from the burner head 51 to extend through the outlet 18 in the cap 12 and terminate interiorly of the tray 11, adjacent its bottom.
  • a cylindrical filter element 92 Lodged in the uppermost end of the fuel pipe 91, relatively adjacent the adaptor 89, is a cylindrical filter element 92.
  • the upper end of the element 92 is centrally and axially recessed in a conventional manner.
  • the body 50 is also formed, adjacent its outer periphery, wi-th a through passage 93 (FIGS. 6 and 8) extending from front to rear thereof and angularly inclined, in a radial sense, to open at its forward end to the recess 71, adjacent the conical projection 72.
  • a through passage 93 (FIGS. 6 and 8) extending from front to rear thereof and angularly inclined, in a radial sense, to open at its forward end to the recess 71, adjacent the conical projection 72.
  • the igniter 95 includes an insulating body 94 containing projected electrode 96.- The outer tip of this electrode positions adjacent the forward extremity of the nozzle head.
  • Mounted externally of the body 94 is a metallic sleeve 97 conductively engaged to the body 50, the latter being of metallic content.
  • a wire-like ground element 98 Fixed at one end, in conductive relation to the sleeve 97 and extending forwardly therefrom, is a wire-like ground element 98.
  • the ground element projects adjacent and generally parallel to the electrode 96 until it reaches a point adjacent its projected extremity. At this point the projected extremity of the wire 98 is first angularly diverted towards the electrode to form 'a small gap therebetween and then
  • This structure produces a simple igniter means providing a relatively small spark gap yand enabling a fan-shaped spark. It allows the use of low voltage (5,000 v.) ignition in lieu of conventional high voltage (10,000 v.) and the achievement of a large volume spark in a manner to be further described.
  • the recess 71 is bounded by wall structure which in the main has a generally cylindrical form. Projected from the inner surface of this wall structure are arcuately formed fingers 101. The .lingers 101 curve in a common direction so as to achieve, peripherally of the recess 7 1, a series of pockets 99 which are encompassed by arcuate wall sections 100.
  • the wall structure which peripherally defines the recess 71 also includes circumferentially spaced, relatively angled, slots 102. Slots 102 are so oriented to provide for a peripheral inliow of air to. the pockets 99 in a sense tangential Ito the arcuate wall sections 100 formed by the fingers 101. As may be readily seen, the slots 102 not only provide for alperipheral inflow of air to the recess 71 to swirl about the discharge end of nozzle 79 ⁇ but also they are so positioned to lie in the operating face 70 of the body 50.
  • the assembly 10'5 includes concentric assembly 105. sleeves 107 and 111, the inner of which is shorter and longitudinally centered in reference to the outer sleeve 111. Nested in the one end of the inner sleeve 107 is a dish-shaped plate 106 having a central aperture 108. The apert-ure 108 is deiined by a conically flared plate portion 109 which extends in a sense inwardly of the sleeve 107. Formed integral Awith the outer peripheral portion of the plate 106 are circumferentially spaced, radially projected fingers the extremities of which are bent to provide lianges 110. The lianges4 110 are so formed to commonly abut thel inner surface of lthe sleeve 111 and are fixed thereto in circumferentially spaced relation thereabout.
  • a dish-shaped plate 112 Nested in the opposite end of the inner sleeve 107 is a dish-shaped plate 112 having a central aperture 113 which positions co-axial to the aperture 108 in the plate 106.
  • the plate 112 is peripherallyl formed likerthe plate 106. Thus at spaced points it abuts the inner wall of the sleeve 111 and is fixed thereto.
  • a deliector plate 114 Spaced to the outermost side of the plate112 is a deliector plate 114 presenting a conically dished surface to its side immediately adjacent the aperture 13 in the plate 112.
  • the plate 114 peripherally corresponds to and is fixed to the plate -112 in a manner believed obvious.
  • the conically dished portion of the plate 114 projects centrally and forwardly of the adjacent end of the outer sleeve 111 which is capped by a convergent nose cone 115.
  • the nose cone 115 is cento accommodate a stud 103 (FIG. 3) or 103 on the burner head 51.
  • the combustion chamber is assembled to peripherally contine and form an axial extension of the burner unit previously described by engagement of its plate por- Itions 117 to form bayonet connections with studs 103 and 103' on the burner head 51 in a manner believed obvious.
  • the single screw stud 103 may be conventionally utilized to fix the position of .the combustion chamber in relation to the burner unit.
  • the projected extremity of the assembly 105 extends co-extensively with the cap 12 and is secured to the cap 12 through the medium of a supporting bracket 120, as may be seen in FIG. 1 of the drawings.
  • the sleeve 107 together with the end plates 106 and 112 form a combustion chamber 121.
  • the plate 106 nests the operating face 70 of the burner head 51 in the interior of its flared portion 109. Further, the concentric sleeves 107 and 111 provide therebetween a tubular air passage 118 for use in a conventional manner.
  • the invention embodiment as above described mounts 7 to its cap 12 suitable connector means through the medium of which power may be fed to energize the motor 23. Simultaneous with the energizing of the motor 23 the drive shaft 29 turns the blades forming the fan unit 33 and the connected rotor 34.
  • the blades 33 produce a pressured flow of air which is external to and proceeds forwardly of the burner unit to move about the burner head and through the tubular passage 118 defined about the combustion chamber 121 to exit as heated'air through the central aperture 116 in the nose cone 115.
  • the vaned rotor 34 continuously rotates within its housing as defined by the ring 35, the motor end plate 32 and the cover plate 36.
  • each vane 41 therein moves past the upper and relatively abutting surface of the ring 35 and shortly thereafter starts to project and passes the opening 46 in the ring 35.
  • the opening 46 it induces an insuction or inflowof static air drawn ythrough the air filter 45 to enter the chamber 44 and pass through the tube 47 to the compression chamber 48 in the path of a following vane 41.
  • the vanes 41 drive the air in advance thereof to an initially expanding portion of the compression chamber 48 and then through a relatively contracting portion thereof until this air is brought in communication with the exit aperture 49 in the cover plate 36.
  • the fuel flow directed to and through the nozzle 79 may be' described as following a main flow passage, with the air reaching and flowing through the nozzle by way of grooves 85 following an auxiliary flow passage. These flows intersect, with the combined ow leaving the tip of the nozzle by what may be considered a main discharge passage.
  • the aperture 49 communicates with the ⁇ burner flow passage 52 and thereby provides that compressed air is released from the compression chamber 48 to be Vdischarged in a sense tangential to the inner wall 53 of the recess 54 in the burner head 51.
  • the longitudinal passages 59 defined by the secondary filter 57 in the recess 54 facilitate the tangential inflow of the compressed air which swirls about and through the filter and gradually inwardly thereof to enable the filter to relieve the air of carbon particles as it moves inwardly to its center.
  • the air reaches the center of the recess 54 Within the tubular filter 57 it passes through the base filter 56 to enter the flow passage 78 in communication with the recess 73 in the face of the burner head 51.
  • the air will enter the recess 73 in a pressured flow to move about the shank 80 of the nozzle 79 to enter the grooves 85 in the shank exterior. Passing through the grooves 85 the compressed air swirls through the passages in the nozzle head to move interiorly of the fuel ow passage defined therethrough. As this air, which is under pressure, is swirled interiorly of the main flow passage through the nozzle 79, it will produce an insuction to draw fuel from the tank to move up through the pipe 91 to pass through the filter 92, to move interiorly of the ow passage 74 and liow through the delivery passage as defined by the nozzle shank.
  • the swirling air which enters the nozzle flow passage not only draws the fuel therethrough but atomizes the fuel, entrains it and causes the fuel to discharge therewith in an atomized condition. This discharge occurs immediately adjacent the operating face 7 0.
  • the positioning of the filters 56 and 57 renders them highly accessible for cleaning and replacement.
  • the relief valve 63 is so provided as to insure a proper control of the pressure under which air is delivered to the recess 73.
  • the fan unit 33 will drive air past the yburner head and interiorly of the combustion chamber assembly 105 through the tubular passage 118 to be heated and discharged thereby.
  • the air liows past the burner head a portion thereof is induced to swirl iuwardly through the slots 182 to enter the recess 71 in a sense tangential to the nger surfaces 160.
  • the swirl of the air is increased thereby.
  • This air which enters the recess 71 swirls therein to move outwardly thereof about the nozzle 79.
  • the igniter 95 provides a set of points which are preformed and fixed. rl ⁇ he spark gap as established by the end of its electrode 96 and the divergent extremity of the ground 98 is positioned immediately forward of the discharge end of nozzle 79.
  • the spark which is developed at the inner end of the V established at the projected ends of the electrode 96 and ground 98 is fanned outwardly between the divergent portions thereof under the influence of the air which moves thereby from the recess 71. In this way, using only a relatively low voltage, one may develop a spark of maximum volume. This insures a most effective ignition of the super atomized fuel at its discharge from the nozzle 79 at a point immediately within the entrance to the combustion chamber 121.
  • the association of the improved ignition features with the effective use of air delivered to the burner head 51 provides for essentially complete combustion of the fuel in the chamber 121 with essentially no deleterious residue. There is a minimal afterfume and optimum heating of the air passing through the chamber passage 118 to exit through the opening 116 in the nose cone.
  • the igniter of the invention incorporates a single electrode in contrast to the conventional use of a pair of adjustable electrodes.
  • the embodiment of the invention as above described includes many features offering improvements in spaceheater elements and the composition thereof in a single compact unit.
  • the means and manner whereby air is delivered to and through the nozzle 79 is significant in and of itself.
  • the manner in which this is accomplished enables the elimination of much hardware and inhibits the occurrence of impurities which would normally cause an undesirable residue in burner units and their component structures.
  • the fuel control and ignition as achieved by the present invention is of considerable importance in developing space heaters of an improved character.
  • Another feature of the invention is evidenced in the simple means by which the burner unit and combustion chamber is applied to a lbase structure offering an improved fuel tank.
  • the manner in which the nozzle is incorporated in the burner, as well as the construction of the burner head per se facilitates maintenance procedures and enables a most economical fabrication of burner units.
  • the space heater in accordance with the present invention achieves maximum economy in the fabrication thereof and maximum efficiency in the operation of its various components.
  • the invention embodiment offers a novel package rendered portable by the following means.
  • a basket-type handle 131 Connecting to the bridging portions of frame members 130 and 1 bridging the wrapper 133 in spaced relation thereto is a basket-type handle 131 having an inverted U-shape.
  • the bridging portion of handle 131 includes a grip 132 which serves as a carrying means for the entire space heater structure. Since the handle 131 is secured to the leg frames 130 which are in turn fixed to the fuel tank 10 through the medium of the cap flange 14, by simply grasping the portion 132, and one may easily lift and transport the entire space heater unit incorporating its fuel tank. It may be seenl from FIG. 2 of the drawings that theleg frames 130 are arranged to be slightly divergent as are the dependent leg portions of the basket-.type handle 131. This achieves a symmetry of structure and facilitates a broad base support for the space heater which inhibits inadvertent displacement thereof from a desired location.
  • a burner unit including a nozzle, said nozzle having flow passages which intersect to provide a main discharge passage, means defining a body structure mounting said nozzle to expose its discharge passage, means provided in said body structure for passage of fuel therethrough to at least a portion of said nozzle flow passages, means defining an airliow passage through said body structure and through said nozzle formed to produce a movement of air therethrough to another portion of said nozzle iiow passages whereby on communication of said fuel passage with a' fuel supply and said air fow passage with air under pressure to induce a iiow of fuelto said nozzle and a discharge thereof from said nozzle in an atomized condition, and means defining a cylindrical recess in Said body structure which intersects said airfiow passage, thepor- Itions of said airfiow passage to the upstream and downstream sides of said recess being oriented in a sense generally at right angles to each other and filter elements stacked in said recess to position in the vpath of air moving from said upstream to said
  • a burner unit including a nozzle having a main fiow passage and intersecting flow passages which merge to its 'discharge end characterized-by a body structure having a recess accommodating a portion of said nozzle forming an air chamber thereabout in communication with said 'ing to said air chamber and opening to the main flow passage in said nozzle on engagement thereof to said body struc-ture means engaged about said nozzle and to said body structure to form a seal whichv separates said air chamber from said fuel passage, the wall of said air chamber about said nozzle being successively stepped in a sense inwardly from the discharge end of said engaged nozzle and having its most reduced portion, in absence of said nozzle in said air chamber, open to said fuel passage, the innermost end of said nozzle being arranged to nest in Ithe innermost end of said air chamber and have lthe seal means thereabout in the form of a deformable washer, the innermost end of which abuts the innermost step in the wall which defines said air chamber, and biasing means interposed between a portion of said
  • a burner unit for space heaters and the like consisting of an integrally conected body structure including a burned head to one end thereof, a motor Ito its other end andA asingle housing formed therebetween, a drive shaft extending from said motor, one end of which terminates in said housing, a vaned rotor on said one end of lsaid drive shaft positioned to form a compression chamber thereabout in said housing, means defining an inlet opening in said housing for inflow of air .to said compression chamber under the influence of said rotor or drive thereby by said motor, means defining an outlet from said chamber for delivery of air therefrom under the influence of said rotor, means forming -a circuitous passage in said burned 'head providing a direct extension of said chamber and enabling direct passage therethrough of air delivered from said chamber and a siphon nozzle mounted in said burner head having means defining a fuel passage in connection therewith and including openings which communicate with said circuitous passage to receive air, the latter passing through said nozzle and drawing fuel to mingle therewith and discharge from
  • a burner unit including Ia burner head, a nozzle mounted t-o project therefrom and said nozzle having main and auxiliary flow passages which intersect to provide a main discharge'passage, characterized by means defining an air compression chamber in direct connect-ion with said head, said chamber having a first opening to the air about said burner unit and means defining a second opening therefrom in direct abutment to said head, means defining a ow passage through said head one end of which forms an extension of said second opening and the other end of which terminates in communication with a portion of the aforementioned main and auxiliary flow passages in said nozzle and means in said compression chamber operative to produce an insuction of air through said first opening and a pressured ow thereof from said second open-ing to and through said portion of said main and c ⁇ carrying frame including .an inverted U-shaped element fixed longitudinally of either side of said tank to have the leg portions thereof depend and provide an elevated support of said tank and a basket type handle transverse to and interconnecting the bridging
  • a burner devi-ce comprising, a nozzle unit, a burner ⁇ head including a first recess accommodating said nozzle unit to mount thereto and project therefrom, a second recess in said burner head about the projected portion of said nozzle, said second recess being defined by a generally cylindrical wall structure including arcuate lingers which extend inwardly thereof to form pockets i-n said burner head which open laterally about said nozzle, the walls of said pockets being arcuately formed and providing peripheral openings for inflow of -air thereto and for tangential delivery of such air to the wall structure delining said pockets whereby to induce a swirling of said air about said nozzle and produce an entrainment of the discharge therefrom, said pockets being formed in a circumferential series extending completely around said nozzle.
  • a burner dev-ice for use in a space heater or t-he like including a burner head having an operating face, a porytion of which is recessed, a nozzle fixed in said burner head to have the discharge end thereof project in said recess, the peripheral wall of said recess having openings therein for inow of air and arcuately formed fingers projecting inwardly thereof in the direct-ion of the projected portion of said nozzle which lingers are operable to induce a swirling of the air thereabout to atomize and accelerate t-he discharge from said nozzle, said fingers being formed in a circumferential series extending completely around said nozzle.
  • a space heater including a motor and burner, the latter having the form of a body provided with oppositely disposed front and rear faces and with a Ithrough fuel ow passage ⁇ opening through the said front face of the body, ring means installed between said mot-or and said burner body interconnecting with said motor which provides its inner face and incorporating motor driven air pump means, said ring means having means in connection therewith providing an outer face in intimately contacting relation to the rear face of said burner body and having further an air discharge pass-age opening through the said other face thereof, said burner body having an air ow passage intersecting at its one end said fuel flow passage and opening at its other end through the said rear face of said burner body, said burner body and said pump body means being so oriented relative to one another as to align said air ow passage and said air discharge passage therein.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
US317088A 1963-10-17 1963-10-17 Portable oil heater Expired - Lifetime US3256003A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US317088A US3256003A (en) 1963-10-17 1963-10-17 Portable oil heater
BE652409D BE652409A (de) 1963-10-17 1964-08-28
DE19641776216 DE1776216A1 (de) 1963-10-17 1964-10-03 Tragbares OElraumheizgeraet
DE19641451413 DE1451413A1 (de) 1963-10-17 1964-10-03 Tragbarer Raumheizapparat
CH1312964A CH442659A (de) 1963-10-17 1964-10-09 Raumheizgerät
NL6411908A NL6411908A (de) 1963-10-17 1964-10-14
GB42302/64A GB1026969A (en) 1963-10-17 1964-10-16 Portable oil heater
AT884664A AT278224B (de) 1963-10-17 1964-10-19 Brennereinheit für einen Raumheizer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US317088A US3256003A (en) 1963-10-17 1963-10-17 Portable oil heater

Publications (1)

Publication Number Publication Date
US3256003A true US3256003A (en) 1966-06-14

Family

ID=23232059

Family Applications (1)

Application Number Title Priority Date Filing Date
US317088A Expired - Lifetime US3256003A (en) 1963-10-17 1963-10-17 Portable oil heater

Country Status (7)

Country Link
US (1) US3256003A (de)
AT (1) AT278224B (de)
BE (1) BE652409A (de)
CH (1) CH442659A (de)
DE (2) DE1776216A1 (de)
GB (1) GB1026969A (de)
NL (1) NL6411908A (de)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3319947A (en) * 1964-12-14 1967-05-16 Century Engineering Corp Portable space heaters
US3393903A (en) * 1966-06-29 1968-07-23 Dura Corp Space heater
FR2132155A1 (de) * 1971-03-29 1972-11-17 Koehring Co
FR2132154A1 (de) * 1971-03-29 1972-11-17 Koehring Co
US3794461A (en) * 1973-04-11 1974-02-26 Lambert Eng Co Motor means for space heater and method of use
US4081238A (en) * 1975-08-08 1978-03-28 Koehring Company Portable heater
US4201544A (en) * 1977-11-10 1980-05-06 Keohring Company High pressure heater
US4203720A (en) * 1978-03-31 1980-05-20 Gilmore & Tatge Mfg. Co. Oil burner
US4313417A (en) * 1979-07-09 1982-02-02 Koehring Company Portable space heater
US5307800A (en) * 1992-07-21 1994-05-03 Desa International, Inc. Afterburner for a fuel-burning heater and method of construction
US5893711A (en) * 1997-12-29 1999-04-13 Vogelzang International Corporation Space heater with plastic fuel tank
US6142141A (en) * 1997-05-05 2000-11-07 The Coleman Company, Inc. Airflow diffuser for use with a forced-air space heater and a forced-air space heater using the same
US9267704B1 (en) 2012-01-26 2016-02-23 Procom Heating, Inc. Portable heater housing
US20210396139A1 (en) * 2020-06-22 2021-12-23 Pinnacle Climate Technologies Rotary Vane Pump

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4162887A (en) * 1977-05-23 1979-07-31 Greenmace Limited Oil burner
US4443187A (en) * 1982-06-04 1984-04-17 Koehring Company Portable heater with integrated control system
CN109028262B (zh) * 2018-07-26 2019-10-01 珠海格力电器股份有限公司 油汀电暖器

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US2655209A (en) * 1950-04-07 1953-10-13 David L Newton Oil burner
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US2759763A (en) * 1952-07-22 1956-08-21 Ransburg Electro Coating Corp Spray coating apparatus and method
US2832403A (en) * 1955-09-20 1958-04-29 Sundstrand Machine Tool Co Air-oil unit
US2879837A (en) * 1958-01-28 1959-03-31 Edgar S Downs Liquid fuel burning heater
US2907529A (en) * 1956-09-17 1959-10-06 Seri A G Liquid fuel burner
US2966347A (en) * 1958-12-22 1960-12-27 Aerovent Fan Co Inc Heater unit
US3071183A (en) * 1959-07-25 1963-01-01 Wilhelm Baier Kg Apparatus for setting space heating systems into operation
US3073583A (en) * 1960-10-28 1963-01-15 John Wood Company Heater
US3101193A (en) * 1961-05-05 1963-08-20 Master Vibrator Co Portable heater
US3129748A (en) * 1961-06-15 1964-04-21 Master Cons Inc Oil burner

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1122147A (en) * 1914-05-14 1914-12-22 James Wesley Moore Blow-torch.
US1180818A (en) * 1915-03-18 1916-04-25 Bradley & Vrooman Company Spraying apparatus.
US1386462A (en) * 1920-05-28 1921-08-02 Charles E Schanck Tank
US1769647A (en) * 1927-01-15 1930-07-01 William J Press Fluid pump
US1855187A (en) * 1928-12-27 1932-04-26 Timken Silent Automatic Compan Oil burner
US2040523A (en) * 1934-06-25 1936-05-12 Edward A Morrison Fluid fuel burner
US2083039A (en) * 1936-01-13 1937-06-08 Edward M Searls Spraying apparatus
US2311018A (en) * 1941-01-08 1943-02-16 Bahnson Co Atomizer
US2363168A (en) * 1942-10-08 1944-11-21 Eaton Mfg Co Heater
US2549253A (en) * 1945-07-02 1951-04-17 Cecil W Smith Liquid fuel and air mixing and supply means for oil burners
US2512301A (en) * 1946-06-19 1950-06-20 Gen Bronze Corp Bowl type oil burner with spark ignition means
US2703607A (en) * 1949-03-25 1955-03-08 Milo R Simmonds Multiple cell fuel tank arrangement
US2658567A (en) * 1949-10-11 1953-11-10 Eureka Williams Corp Oil burner
US2655209A (en) * 1950-04-07 1953-10-13 David L Newton Oil burner
US2606014A (en) * 1950-10-02 1952-08-05 Arthur C Baumann Space heater
US2759763A (en) * 1952-07-22 1956-08-21 Ransburg Electro Coating Corp Spray coating apparatus and method
US2832403A (en) * 1955-09-20 1958-04-29 Sundstrand Machine Tool Co Air-oil unit
US2907529A (en) * 1956-09-17 1959-10-06 Seri A G Liquid fuel burner
US2879837A (en) * 1958-01-28 1959-03-31 Edgar S Downs Liquid fuel burning heater
US2966347A (en) * 1958-12-22 1960-12-27 Aerovent Fan Co Inc Heater unit
US3071183A (en) * 1959-07-25 1963-01-01 Wilhelm Baier Kg Apparatus for setting space heating systems into operation
US3073583A (en) * 1960-10-28 1963-01-15 John Wood Company Heater
US3101193A (en) * 1961-05-05 1963-08-20 Master Vibrator Co Portable heater
US3129748A (en) * 1961-06-15 1964-04-21 Master Cons Inc Oil burner

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3319947A (en) * 1964-12-14 1967-05-16 Century Engineering Corp Portable space heaters
US3393903A (en) * 1966-06-29 1968-07-23 Dura Corp Space heater
FR2132155A1 (de) * 1971-03-29 1972-11-17 Koehring Co
FR2132154A1 (de) * 1971-03-29 1972-11-17 Koehring Co
US3706446A (en) * 1971-03-29 1972-12-19 Koehring Co Portable heater
US3794461A (en) * 1973-04-11 1974-02-26 Lambert Eng Co Motor means for space heater and method of use
US4081238A (en) * 1975-08-08 1978-03-28 Koehring Company Portable heater
US4201544A (en) * 1977-11-10 1980-05-06 Keohring Company High pressure heater
US4203720A (en) * 1978-03-31 1980-05-20 Gilmore & Tatge Mfg. Co. Oil burner
US4313417A (en) * 1979-07-09 1982-02-02 Koehring Company Portable space heater
US5307800A (en) * 1992-07-21 1994-05-03 Desa International, Inc. Afterburner for a fuel-burning heater and method of construction
US6142141A (en) * 1997-05-05 2000-11-07 The Coleman Company, Inc. Airflow diffuser for use with a forced-air space heater and a forced-air space heater using the same
US5893711A (en) * 1997-12-29 1999-04-13 Vogelzang International Corporation Space heater with plastic fuel tank
US9267704B1 (en) 2012-01-26 2016-02-23 Procom Heating, Inc. Portable heater housing
US20210396139A1 (en) * 2020-06-22 2021-12-23 Pinnacle Climate Technologies Rotary Vane Pump
US11680566B2 (en) * 2020-06-22 2023-06-20 Pinnacle Climate Technologies, Inc. Rotary vane pump

Also Published As

Publication number Publication date
NL6411908A (de) 1965-04-20
GB1026969A (en) 1966-04-20
BE652409A (de) 1964-12-16
DE1776216A1 (de) 1972-08-31
DE1451413A1 (de) 1969-10-23
AT278224B (de) 1970-01-26
CH442659A (de) 1967-08-31

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Owner name: KOEHRING COMPANY 200 EXECUTIVE DRIVE, BROOFIELD, W

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:KOEHRING COMPANY A WI CORP.;REEL/FRAME:003995/0514

Effective date: 19810505