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US3602621A - Recirculating fuel burner - Google Patents

Recirculating fuel burner Download PDF

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Publication number
US3602621A
US3602621A US874130A US3602621DA US3602621A US 3602621 A US3602621 A US 3602621A US 874130 A US874130 A US 874130A US 3602621D A US3602621D A US 3602621DA US 3602621 A US3602621 A US 3602621A
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Prior art keywords
plate
fuel
housing
chamber
assembly
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US874130A
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Jesse B Mellett
Tilford W Sutterfield
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Stewart Warner Corp
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Stewart Warner Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D3/00Burners using capillary action
    • F23D3/40Burners using capillary action the capillary action taking place in one or more rigid porous bodies
    • 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
    • F23D11/44Preheating devices; Vaporising devices
    • F23D11/441Vaporising devices incorporated with burners

Definitions

  • Newman and Norton Lesser ABSTRACT The use of paired, concentric, axially spaced and nested coaxial cup-shaped members downstream of an apertured plate carrying a porous conical fuel wick to aims 6 Drawmg Figs promote recirculation of the forced combustion air within the U.S.Cl 431/116, combustion chamber. Additionally, a spiral-type igniter is 431/300 used in a position recessed from the combustion chamber and lnt.Cl F231 1/00, to which a short wicking material is extended for initiating F 231 7/00 combustion.
  • HO. 1 is a side elevation, partially in section, of the improved recirculating liquid burner of the present invention
  • FIG. 2 is a sectional elevation of a portionof the apparatus of P16. 3 taken about lines 2-2;
  • FIG. 3 is a rear elevational view of theimproved recirculating apparatus or assembly
  • F l0. 4 is a sectional view illustrating a recessed igniter assembly contributing to the reliability and service of the igniter
  • FIG. 5 is an enlarged fragmentary sectional view illustrating a portion of the igniter assembly.
  • FIG. 6 is a sectional view taken generally along the line 6-6 in FIG. 5.
  • the apparatus of the present invention comprises an improved liquid fuel burner of the recirculating t combustion products type.
  • a blower at the airinlet end of the housing forces combustion air longitudinally therethrough.
  • a transversely extending, aperturedplate, downstream of the blower directs the air along prescribed paths relative to a conical ceramic wick which is carried coaxially of the apertured plate on a downstream side thereof.
  • Paired, concentric, axially spaced cup-shaped members are also'positioned in nested fashion downstream of the porous conical wick with their open ends receiving the combustion air which passes through the plate and across the surface of the porous wick.
  • the cupshap'ed-members reflect heat onto the porous wick surface to promote fuel vaporizationand the recirculated combustion products insureefficient mixing of the vaporized fuel with the air duringcombustion.
  • Anelectrical resistance igniter comparable to an automobile cigar lighter in form is carried by the aperture plate and "in-juxtaposition to the porous wick for igniting the fuel.
  • the multiple turn resistance igniter because of the flat spiral face,
  • FIG. 1 it is noted in FIG. 1 that the recirculating liquidfuelburner ofthe present invention may be appropriately employed in a vehicle to supply forced heated air.
  • the heater assembly 10 includes an outer cylindrical casing or'housing 12 which carries at the upstream or .air inlet end a blower motor 16 including a combustion air blowerf20.
  • Shroud 22 overlies the blower 20 at the upstream end of the combu'stion 'chamber.
  • a somewhat smaller cylindrical casing casing 26 defined principally the combustion chamber 24, the exhaust gases leave the combustion chamber as indicated by the arrows 28through combustion chamber opening 30 into an annular channel 32 defined by a cylindrical casing35 between the combustion chamber casing 26 and a third annular casing 34', of slightly larger diameter.
  • Casing 34 is spaced inwardly from the main cylindrical casing member 12 to define a narrow annular passage 36 through which heated ventilating air indicated by arrows 38 is directed from the heater at the desired temperature exiting at outlet 120.
  • a transversely extending, support plate .40 closes off the combustion chamber fromthe area immediately downstream of the blower of the combustion air blower 20.
  • Ceramic,.coaxial wick 42 is carried centrally of the support .plate 40."Fuel' is supplied through a fuel inlet tube44, and controlled by valve'means '45 to wick'42.
  • the inlet tube or spud 44 is coupled to the support plate, at the axis thereof, by coupling means 46.
  • the spud-44 is provided with cross bored apertures 47 allowing'the liquid fuel to permeate the porous ceramic wick 42.
  • Th'e 'fuel is vaporized on the surface as a result of the heat of combustionPressurized air in passing over the outer surface 48 of the ceramic wick, picks up the vaporized fuel and mixes with the same.
  • the porous wick'42 is bored at 50 an d'is inserted onto the reduced diameter end 52 of the'fuel inlettube or spud 42 against shoulder 54.
  • Wick retaining washers 56 sandwich the axial ends of the wick 42 while threaded.
  • screw 58 couples the wick and the wick retaining washer 56 to spud 42 and fixes a small diameter cup 1 shaped member60' to the downstream end of the porous conithe smallercup-shaped member 60 and partially encirclesthe ceramic wick 42 while completely encirclingthe smaller cupshaped member 60 to facilitate proper recirculation of the pressurized, moving combustion air.
  • the wick 42 is partially nested within both the cup-shaped member 60 and the larger cup-shaped member 62, while the smaller cupshaped' member-60 is completely nested within axially and radially spaced from the larger outer cup-shaped member 62.
  • Thelarge'cup-shaped member 62 is coupled to the transverse apertured plate 40 by means of a plurality of cup support legs 64, each threaded at their upstream ends and carrying suitable nuts 66.
  • the support plate 40 forms an important part of the present invention other than its function to support the ceramic wick 42 and the coaxial nested cup-shaped members 60 and 62.
  • the transverse plate 40 is apertured in a manner best indicated at FIG. 3 to direct both primary and secondary air along desired circumferential but regularly spaced paths relative to these downstream elements.
  • Combustion air under pressure from blower moves through the apertured plate within three sets of circumferentially arranged apertures 68, 70 and 72.
  • the four circumferentially arranged apertures 68 are spaced close to the fuel tube or spud 44 and directly behind the somewhat cup-shaped conical wick 42.
  • the apertures or holes 68 provide minor amounts of combustion air for the area 74 between the porous-wick 42 and the support plate 40.
  • Primary combustion air of much greater magnitude is forcibly directed through the larger number of circumferentially arranged holes 70 which are spaced radially outward of the four holes 68, the holes 70 being positioned such that the air passing therethrough as indicated by arrows 76 moves along the outer surface 48 of the porous wick 42 but inwardly of the peripheral rim 78 of the smaller cup-shaped member 60.
  • the larger portion of this air is caused to reverse itself along the outside of the incoming airstream,
  • a certain portion of the air exits from the rim or peripheral edge 78 of the smaller cup-shaped member 60 and circulates within the area defined by the rim 82 of the second cup-shaped member 62.
  • it mixes with the secondary combustion air entering the chamber through openings 72 formed by associated louvers 86 within the transverse plate 40.
  • the circumferential array of louvers 86 and the apertures 72 is located radially beyond the series of apertures or holes 70 and between the peripheral rim 78 of the smaller cupshaped member 60 and the peripheral rim 82 of the larger cup-shaped member 62.
  • This airstream has a partial spiral flow path which is introduced as a result of the louver configuration to promote fuel and air mixing.
  • the airstream identified by arrows 84 also creates a low-pressure area especially on the outward radial side thereof so that, as the burning mixture exits from the large cup 62, a portion of the products of combustion moves by way of arrows 95 back toward the support plate 40 and is reentrained into the secondary airflow and therefore moves back into the rear of the large cup-shaped member 62.
  • Recirculation of the combustion products due to the primary airflow, secondary airflow and the positioning and the relationship of the first and second cup-shaped member with respect to the aperture plate 40 is extremely valuable in promoting maximum fuel and air mixing, uniformity of the same and resultant complete combustion. It further permits the heavy fuels to be burned without coking while the heat resulting from combustion is readily radiated back from the two cup-shaped members to aid in vaporizing the fuel at the surface of the wick.
  • Burning is achieved within the center 90 of the larger cupshaped member 62 with the fuel and air mixture swirling in the fashion of arrows 92 prior to moving out of cup-shaped member 62 and into the combustion chamber proper 24 as indicated by the dotted arrow 94 by passing around the rim 82 of the large cup-shaped member 62.
  • the lighter fuels because of the wick and cup arrangement, vaporize muchsooner than in ordinary burners because of the relatively high heat provided by the second cup-shaped member 62' at the back end of the wick. Because thisfuel vaporizes quickly, it does not crack as ordinarily would occur where it is subjected to high surface heat before it had a chance to vaporize and burn. In effect, therefore, both the high heat content and the recirculation provided by the cups enhance burning of the heavy fuels while the lighter fuels are permitted to burn without cracking, vastly extending the range of fuels which are advantageously burned within the assembly of the present invention.
  • Shroud 22 which forms the combustion air inlet housing terminates in a peripheral groove 96 which receives an annular sealing member 98 which seals the combustion air inlet housing to the burner.
  • Plate 40 is provided with a peripheral flange 100 which is reversely turned at 102 and carries an annular sealing member 104 to provide in conjunction with combustion chamber housing or casing 26, and burner mounting and air distribution plate 106, a burner to combustion chamber seal. It is noted that the burner mounting and air distribution plate 106 which is sandwiched between the flange portion 100 of the transverse support plate 40, and the slightly larger diameter combustion chamber casing member 26, has an inwardly inclined downstream portion which tends to deflect the air downstream and inward as it passes over the lip 82 of the large cup-shaped member 62.
  • the transfer support plate 40 is provided with an enlarged diameter aperture 108 which received a disclike spiral electrical resistance heater element 110, from the rear of which protrudes a pair of electrical leads ll2 allowing suitable connection to a source of electrical energy (not shown).
  • the resistance coil 114 itself faces downstream and is spaced slightly from the porous wick member 42 to readily ignite the fuel.
  • the cigar-type resistance heater coil is made of a wire which comprises an alloy of aluminum, iron, chromium, cobalt and tantalate, and is manufactured and sold by the Kanthal Corporation of Bethel, Conn. Since the flat spiral face provides a large area'of high heat intensity in ready contact with the wick, the fuel vaporization and ignition is rapid and assured. This is in contrast with the prior art methods employing either spark electrodes or a helical-type resist nce igniter. In the helical resistance-type heater, it is only e last'loop of the helix that has considerable contact with the vaporized fuel, affording some unreliability especially when he fuel comprises a heavier fuel oil.
  • Du ing operation with the blower motor 16 operating, air is drawrLinto the housing 12, preferably by a ventilating air fan (not s own) near the air inlet of the blower assembly.
  • a part of the air is drawn into the combustion air blower 20 through the opening 116 in-the center of the blower housing 22 and is forced into the primary and secondary air openings 68, 70 and 72 at the upstream end of the heat exchanger.
  • the primary combustion air flows over the surface 48 of the porous wick 42 to rapidly remove vaporized liquid fuel therefrom and mix it readily with the combustion air.
  • Momentary energization of the igniter or. spiral resistance heater 110 through leads 112 achieves immediate ignition of the fuel air mixture with burning being carried on within the area 90 within the cup-shaped member 62. Mixture of the fuel and air is enhanced, and recir- -culation insured by the presence of the small and larger cupefficiently heated prior to discharge through the downstream end 120 of the assembly.
  • the apparatus of the present invention is particularly applicable to the heating of ventilating air for a vehicle; however, the improved recirculating air, liquid fuel burner has application to many other fields requiring burners which operate efficiently with liquid fuels ranging from heavy oils to light gasolines.
  • FIG. 4 an improved igniter assembly is illustrated therein by the reference character 122 for use in'a heater assembly such as and those parts similar or identical to those shown in heater 10 are given the same reference characters.
  • a support plate 40 having a plurality of spaced openings as previously described.
  • a plurality of studs such as 124 extend from the rim of a cup-shaped member 62 and are bolted to the support plate 40 to carry the cup-shaped member 62.
  • the burner cup or member 62 as shown in FIG. 4
  • a fuel inlet spud 44 extends through the central axis of plate 40 and coupling means 46 couples a fuel inlet pipe to the spud.
  • a ceramic wick 42 is located adjacent the end of spud 44 and cross bored apertures 47 in spud. 44 serve to deliver fuel from the spud to the wick.
  • the wick 42 is providedwith a central recess 126 at one end in which a pair of washers 56 are seated for butting the wick 42, which is clamped on spud 44 together with a small diameter cup-shaped member 60 by means of a screw 58.
  • a small axially extending opening 128 is provided in the ceramic wick 42 along the vertical axis and above the midplane of the wick 42 and is aligned with openings in the washers 56 for receiving several strands 130 of a loop of conventional wicking material.
  • the strands 130 extend upstream from the member 60 through an opening 132 in the support plate 40. Opening 132 is located above the central axis and along the vertical axis of the support plate 40 so that it is generally aligned with opening 128.
  • the igniter assembly 122 comprises a sheet metal housing 134 having semiannular wall 136 extending upstream from opening 132 and whose end is welded to plate 40 in alignment with the opening 132 with the ends of the semiannular wall 136 connected by a flat wall 138 alignedwith a straight portion of opening 132.
  • the walls 136 and 138 at the ends opposite opening 132 terminate in a short annular wall section 140 extending both upwardly and upstream.
  • wall 140 terminates in a radially inwardly and downwardly directed flange 142 for receiving an igniter 110 having a spiral electrical resistance heater element 114 and similar to the igniter previously described but having a cup-shaped wall which fits snugly within the flange on wall 140 and an annular rear wall 142, which overlaps wall 140 and buttsagainst the end of wall section 140.
  • a wick support or retainer 142 of wire fastened to the flat wall 138 has an upwardly extending leg 144 at the end adjacent opening 132 terminating in a loop for supporting the wick strands 130 in front of the igniter 110 and'a hooklike leg 146 at the opposite or upstream end around which the strands 130 are looped so that the strands are held a short distance in front of the igniter 110.
  • the igniter is biased into the opening defined by wall 140 by a helical spring 148 received in wall 142, which spring together with the igniter leads 112 and are enclosed in an an-. nular housing 150 whose lower end telescopes over the wall 140.
  • the housing 150 together with the fuel inlet pipe for spud 44 extend upwardly through appropriately sealed openings in a shroud 22 serving a similar function to the previously described shroud 22 but having a slightly different configuration.
  • the housing 150 is secured at its upper end by legs such as 152 to a wall 154 extending upwardly from and externally of the shroud 22 for enclosing the housing 150 between the shroud and the outer wall 12.
  • a cup-shaped wall or cap 156 fits telescopingly'in the upper end of housing 150 for restraining the end of spring 148 to apply a force for holding the igniter in the opening defined by wall 140.
  • J-shapedslots such as 158 in the upper end of housing 150 permit the cap 156 to be retainedin position in response to the insertion of a rod or projections 160 on cap 156 in the slots and rotation of the cap to place the projections 160 in the hook portion of slots 158 and effect a bayonet-type connection.
  • a central aperture in the backwall of cap 156 permits the electrical leads 112 to be extended from the igniter through a suitable opening in a removable cover plate 162 carried on the outer burner wall 12 to a suitable power supply.
  • the igniter 110 for easy servicing or replacement is provided by simply removing the cover plate 162 usually after leads 112 are detached from the power source.
  • the cap 156 is rotated to align the rod 160 with the vertical straight leg of the J-slots 158 to permit withdrawal of cap 156 and spring 148 from housing 150.
  • the igniter 110 may then be lifted by means of the leads from housings 150 and 154 and either serviced or replaced as the case may be.
  • the igniter 110 and spring 148 are then simply positioned in housing 150 and the cap 156 replaced to cause the spring 148 to hold the igniter 1 10 in position and the cover plate replaced.
  • the strands of wicking material conduct fuel to the igniter 110 in its recessed position sothat the igniter may initiate the combustion cycle.
  • a flame is established by the igniter in housing 134 a small jet of flame extends through the opening 132 and ignites the fuel transmitted through wick 42 to ignite the main flame.
  • the fuel is vaporized relatively rapidly and does not soak back through strands 130 and into the area in front of the igniter 1 10, so that area stays dry and free of carbon. Since the igniter 110 is relatively remote from the main area of combustion and is located in an area from which heat is conducted, it cools rapidly after combustion is initiated since the flame is transferred from the housing 134 with consequent extension of the igniter life.
  • a fuel burner assembly including casing means forming a combustion chamber and blower means for forcing combustion air longitudinally therethrough, the improvement comprising: a transverse, apertured plate for directing combustion chamber inlet air along prescribed longitudinal paths, a first cup-shaped member coaxially positioned downstream of said plate with the open end thereof directed toward said incoming combustion air, a ceramic wick coaxially carried by said assembly on the downstream side of said plate, within said cup-shaped member and spaced axially and radially therefrom, means for delivering liquid fuel to said porous wick member, and an electrical resistance coil for igniting said fuel lying in a plane located axially upstream from said plate.
  • sistance element comprises a spiral turn of aluminum, iron, chromium, cobalt and tantalate alloy wire.
  • said communicating means comprises an opening in said plate and a first housing extending at one end from said plate opening and having an opening for receiving said igniter at a position spaced from said plate opening.
  • a spring for biasing said igniter toward said housing opening a second housing encircling said spring and having one end telescopingly received by said first housing and encircling each electrical lead extending to said igniter, the opposite end of said housing accessible from a position external said casing, and a cap for said housing other end biased by said spring into locked position and rotatable for disengagement from said other end to facilitate removal of said spring and igniter from said other housing.
  • a plate adjacent said one end of said chamber with said plate having a plurality of apertures therein at one radial distance from the axis of said plate and with a second plurality of apertures therein at a different radial distance from said axis for passing combustion air, a fuel inlet conduit passing through the axis of said plate and terminating in said chamber, a wick in said chamber and extending radially from said conduit, means for communicating fuel from said conduit to said wick, a shield spaced adjacent the downstream end of said wick and having a greater radial dimension than said wick, a cup-shaped member spaced downstream from said shield and extending radially beyond said shield with the open end of said cup facing upstream, and a coil located upstream of said plate and spaced from said plate for igniting the fuel transmitted from said conduit to said wick.
  • housing means extending through said airstream, and manually movable means in said housing means for retaining said coil in said plane and operable for enabling withdrawal of said coil through said housing to a position external said assembly.
  • a fuel assembly having a wall defining a combustion chamber and blower means for driving air in a stream from one end of said chamber toward the other end, the improvementcomprising a plate adjacent said one end of said chamber, means associated with said plate forpassing both combustion air and fuel into said chamber to develop a flame in said chamber, a coil of electrical resistance wire arranged solely in a spiral to initiate said flame, and means detachably fixing said coil upstream from said plate.
  • a fuel burner assembly having a wall defining a combustion chamber and blower means for driving air in a stream from one end of said chamber toward the other end, the improvement comprising a plate adjacent said one end of said chamber, means associated with said plate for passing both combustion air and fuel into said chamber upstream of said plate to develop a flame in said chamber, a coil of electrical resistance wire arranged solely in a spiral to initiate said flame and located upstream of said plate, and means for passing fuel from said chamber through said plate to the vicinity of said coil.
  • said means for passing fuel to said chamber includes a wick in said chamber, and said means for passing fuel through said plate comprises an opening in said plate, a housing having an open end connected to said opening, and a wicking material interconnected with said wick and extending through said opening into said housing.
  • housing means communicating with the end of said housing opposite said open end and extending through said airstream, manually movable means in said housing means for retaining said spiral coil adjacent the end of said housing opposite said open end and operable for enabling withdrawal of said spiral coil through said housing to a position external said assembly.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wick-Type Burners And Burners With Porous Materials (AREA)

Abstract

The use of paired, concentric, axially spaced and nested coaxial cup-shaped members downstream of an apertured plate carrying a porous conical fuel wick to promote recirculation of the forced combustion air within the combustion chamber. Additionally, a spiral-type igniter is used in a position recessed from the combustion chamber and to which a short wicking material is extended for initiating combustion.

Description

United States Patent Inventors Jesse B; Mellett Zlonsville; Tllford W. Sutterfield, Indianapolis, both 7 of, 1nd. Appl. No. 874,130 Filed Nov. 5, 1969 Patented Aug. 31, 1971 Assignee Stewart-Warner Corporation Chicago, 111.
Continuation-impart of application Ser. No. 741,738, July 1, 1968, now Patent No. 3,523,004,
RECIRCULATING FUEL BURNER [50] FieldofSearch 43l/l15, l16,300;l26/1l6 [56] References Cited UNlTED STATES PATENTS 2,850,004 9/1958 Fairbanks 126/116 3,402,985 9/1968 Galvin 431/116 Primary E xaniineF-Edward G. Favors Auorneys-Augustus G. Douvas, William J. Newman and Norton Lesser ABSTRACT: The use of paired, concentric, axially spaced and nested coaxial cup-shaped members downstream of an apertured plate carrying a porous conical fuel wick to aims 6 Drawmg Figs promote recirculation of the forced combustion air within the U.S.Cl 431/116, combustion chamber. Additionally, a spiral-type igniter is 431/300 used in a position recessed from the combustion chamber and lnt.Cl F231 1/00, to which a short wicking material is extended for initiating F 231 7/00 combustion.
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J es I i 1,
PATENTED was] I97! 3.602.621
SHEET 2 0F 2 RECIRCULATINGFUEL autumn CROSS-REFERENCE TO RELATED APPLlCATlON This application is a continuation-in-part application of ap- Forced air liquid fuel burners conventionally include a blower at the forward end of the burner casing which forces combustion air towards the combustion chamber portion and about the fuel inlet means to promote rapid and efficient mixing of the fuel with the air and vaporization of'the same: prior to combustion of the fuel-air mixture in the combustion chamber. The degree of vaporization of the liquid fuel and mixing of the same with the forced combustion air not only determines the overall efficiency of the fuel burner, but also the ability of the fuel burner to burn a range of liquid fuels from heavy oils to lighter gasolines.
Attempts have been made tocause the'pressurizedair to swirl during its movement into the combustion chamber and about the liquid fuel delivery means. Some attempts have been made to redirect the combustion'products along a reverse path to facilitate vapor pickup and more intimate mixing of the same with the combustion air prior to reaching the'flame front in the combustion :chamber. The reliability andefficiency of the liquid fuel burner is also dependent somewhat on the ability of the fuel and air mixture to be readily ignited especially when using heavy liquid-fuel as diesel'fuel, commonly known as DF2 or arctic grade fuel.
It is therefore a primary object of this invention to provide an improved liquid fuel burner of the recirculating type which burns fuel ranging from heavy oilsto gasoline with increased efficiency.
It is the further object of this invention to provide an improved recirculating liquid fuel bumer which is characterized by fast startup and ignition.
it is a further object of this invention to provide an improved recirculating liquid fuel. burner which advantageously radiates the heat of combustion to a fuelled porous wick to increase vaporization of the fuel.
It is also an object of the present invention to. provide anigniter assembly which contributes to improved reliability, economy and service. I 1
Other objects of this invention will be pointed out in the following detailed description and claim and illustrated in the accompanying drawings which disclose, by way of example, the principle of this invention in the best mode which hasbeen contemplated of applying that principle.
In the drawings:
HO. 1 is a side elevation, partially in section, of the improved recirculating liquid burner of the present invention;
FIG. 2 is a sectional elevation of a portionof the apparatus of P16. 3 taken about lines 2-2;
FIG. 3 is a rear elevational view of theimproved recirculating apparatus or assembly;
F l0. 4 is a sectional view illustrating a recessed igniter assembly contributing to the reliability and service of the igniter;
FIG. 5 is an enlarged fragmentary sectional view illustrating a portion of the igniter assembly; and
FIG. 6 is a sectional view taken generally along the line 6-6 in FIG. 5.
In general, the apparatus of the present invention comprises an improved liquid fuel burner of the recirculating t combustion products type. A blower at the airinlet end of the housing forces combustion air longitudinally therethrough. A transversely extending, aperturedplate, downstream of the blower directs the air along prescribed paths relative to a conical ceramic wick which is carried coaxially of the apertured plate on a downstream side thereof. Paired, concentric, axially spaced cup-shaped members are also'positioned in nested fashion downstream of the porous conical wick with their open ends receiving the combustion air which passes through the plate and across the surface of the porous wick. The cupshap'ed-members reflect heat onto the porous wick surface to promote fuel vaporizationand the recirculated combustion products insureefficient mixing of the vaporized fuel with the air duringcombustion. 7
Anelectrical resistance igniter comparable to an automobile cigar lighter in form, is carried by the aperture plate and "in-juxtaposition to the porous wick for igniting the fuel. The multiple turn resistance igniter, because of the flat spiral face,
provides a large area of high heat to achieve initial fuel vaporization to promote rapid ignition, even when heavy fuel oils'are burned.
vTurningto the drawings,'it is noted in FIG. 1 that the recirculating liquidfuelburner ofthe present invention may be appropriately employed in a vehicle to supply forced heated air.
In this respect, the heater assembly 10 includes an outer cylindrical casing or'housing 12 which carries at the upstream or .air inlet end a blower motor 16 including a combustion air blowerf20. Shroud 22 overlies the blower 20 at the upstream end of the combu'stion 'chamber. A somewhat smaller cylindrical casing casing 26 defined principally the combustion chamber 24, the exhaust gases leave the combustion chamber as indicated by the arrows 28through combustion chamber opening 30 into an annular channel 32 defined by a cylindrical casing35 between the combustion chamber casing 26 and a third annular casing 34', of slightly larger diameter. Casing 34 is spaced inwardly from the main cylindrical casing member 12 to define a narrow annular passage 36 through which heated ventilating air indicated by arrows 38 is directed from the heater at the desired temperature exiting at outlet 120.
"A transversely extending, support plate .40 closes off the combustion chamber fromthe area immediately downstream of the blower of the combustion air blower 20. A conical,
ceramic,.coaxial wick 42 is carried centrally of the support .plate 40."Fuel' is supplied through a fuel inlet tube44, and controlled by valve'means '45 to wick'42. The inlet tube or spud 44;is coupled to the support plate, at the axis thereof, by coupling means 46. The spud-44 is provided with cross bored apertures 47 allowing'the liquid fuel to permeate the porous ceramic wick 42. Th'e 'fuel is vaporized on the surface as a result of the heat of combustionPressurized air in passing over the outer surface 48 of the ceramic wick, picks up the vaporized fuel and mixes with the same. The porous wick'42 is bored at 50 an d'is inserted onto the reduced diameter end 52 of the'fuel inlettube or spud 42 against shoulder 54. Wick retaining washers 56 sandwich the axial ends of the wick 42 while threaded. screw 58 couples the wick and the wick retaining washer 56 to spud 42 and fixes a small diameter cup 1 shaped member60' to the downstream end of the porous conithe smallercup-shaped member 60 and partially encirclesthe ceramic wick 42 while completely encirclingthe smaller cupshaped member 60 to facilitate proper recirculation of the pressurized, moving combustion air. In this respect the wick 42 is partially nested within both the cup-shaped member 60 and the larger cup-shaped member 62, while the smaller cupshaped' member-60 is completely nested within axially and radially spaced from the larger outer cup-shaped member 62. Thelarge'cup-shaped member 62 is coupled to the transverse apertured plate 40 by means of a plurality of cup support legs 64, each threaded at their upstream ends and carrying suitable nuts 66.
The support plate 40 forms an important part of the present invention other than its function to support the ceramic wick 42 and the coaxial nested cup- shaped members 60 and 62. In order to facilitate proper vaporization of the fuel and mixture of the same with the forced combustion air, the transverse plate 40 is apertured in a manner best indicated at FIG. 3 to direct both primary and secondary air along desired circumferential but regularly spaced paths relative to these downstream elements. Combustion air under pressure from blower moves through the apertured plate within three sets of circumferentially arranged apertures 68, 70 and 72. The four circumferentially arranged apertures 68 are spaced close to the fuel tube or spud 44 and directly behind the somewhat cup-shaped conical wick 42. The apertures or holes 68 provide minor amounts of combustion air for the area 74 between the porous-wick 42 and the support plate 40. Primary combustion air of much greater magnitude is forcibly directed through the larger number of circumferentially arranged holes 70 which are spaced radially outward of the four holes 68, the holes 70 being positioned such that the air passing therethrough as indicated by arrows 76 moves along the outer surface 48 of the porous wick 42 but inwardly of the peripheral rim 78 of the smaller cup-shaped member 60. This gives rise to a jet airstream directly adjacent to the wick periphery, part of which goes around the back or rear surface 80 of the wick 42 between the small cup-shaped member 60 and the wick. The larger portion of this air, however, is caused to reverse itself along the outside of the incoming airstream,
towards the rear surface of the support plate and the low pressure which exists on the outside of the jetstream as indicated by arrows 76.
Because of the low pressure created by the jetstream mov ing through the small holes, the portion of rearwardly moving air tends to move back into the jet airstream carrying vaporized, partially burned fuel with it. These products of combustion, for reasons not known, act as a catalyst promoting burning of the vaporized fuel.
A certain portion of the air, of course, exits from the rim or peripheral edge 78 of the smaller cup-shaped member 60 and circulates within the area defined by the rim 82 of the second cup-shaped member 62. Here it mixes with the secondary combustion air entering the chamber through openings 72 formed by associated louvers 86 within the transverse plate 40. The circumferential array of louvers 86 and the apertures 72 is located radially beyond the series of apertures or holes 70 and between the peripheral rim 78 of the smaller cupshaped member 60 and the peripheral rim 82 of the larger cup-shaped member 62. This airstream has a partial spiral flow path which is introduced as a result of the louver configuration to promote fuel and air mixing.'The airstream identified by arrows 84 also creates a low-pressure area especially on the outward radial side thereof so that, as the burning mixture exits from the large cup 62, a portion of the products of combustion moves by way of arrows 95 back toward the support plate 40 and is reentrained into the secondary airflow and therefore moves back into the rear of the large cup-shaped member 62. Recirculation of the combustion products due to the primary airflow, secondary airflow and the positioning and the relationship of the first and second cup-shaped member with respect to the aperture plate 40 is extremely valuable in promoting maximum fuel and air mixing, uniformity of the same and resultant complete combustion. It further permits the heavy fuels to be burned without coking while the heat resulting from combustion is readily radiated back from the two cup-shaped members to aid in vaporizing the fuel at the surface of the wick.
Burning is achieved within the center 90 of the larger cupshaped member 62 with the fuel and air mixture swirling in the fashion of arrows 92 prior to moving out of cup-shaped member 62 and into the combustion chamber proper 24 as indicated by the dotted arrow 94 by passing around the rim 82 of the large cup-shaped member 62.
The lighter fuels, because of the wick and cup arrangement, vaporize muchsooner than in ordinary burners because of the relatively high heat provided by the second cup-shaped member 62' at the back end of the wick. Because thisfuel vaporizes quickly, it does not crack as ordinarily would occur where it is subjected to high surface heat before it had a chance to vaporize and burn. In effect, therefore, both the high heat content and the recirculation provided by the cups enhance burning of the heavy fuels while the lighter fuels are permitted to burn without cracking, vastly extending the range of fuels which are advantageously burned within the assembly of the present invention.
Shroud 22 which forms the combustion air inlet housing terminates in a peripheral groove 96 which receives an annular sealing member 98 which seals the combustion air inlet housing to the burner. Plate 40 is provided with a peripheral flange 100 which is reversely turned at 102 and carries an annular sealing member 104 to provide in conjunction with combustion chamber housing or casing 26, and burner mounting and air distribution plate 106, a burner to combustion chamber seal. It is noted that the burner mounting and air distribution plate 106 which is sandwiched between the flange portion 100 of the transverse support plate 40, and the slightly larger diameter combustion chamber casing member 26, has an inwardly inclined downstream portion which tends to deflect the air downstream and inward as it passes over the lip 82 of the large cup-shaped member 62.
As mentioned previously an important element of the improved assembly resides in the use of an ordinary automobile cigar lighter in the form of a spiral electrical resistance heater coil as a means for starting vaporization and for igniting the fuel. In this respect, the transfer support plate 40 is provided with an enlarged diameter aperture 108 which received a disclike spiral electrical resistance heater element 110, from the rear of which protrudes a pair of electrical leads ll2 allowing suitable connection to a source of electrical energy (not shown). The resistance coil 114 itself faces downstream and is spaced slightly from the porous wick member 42 to readily ignite the fuel. Preferably, the cigar-type resistance heater coil is made of a wire which comprises an alloy of aluminum, iron, chromium, cobalt and tantalate, and is manufactured and sold by the Kanthal Corporation of Bethel, Conn. Since the flat spiral face provides a large area'of high heat intensity in ready contact with the wick, the fuel vaporization and ignition is rapid and assured. This is in contrast with the prior art methods employing either spark electrodes or a helical-type resist nce igniter. In the helical resistance-type heater, it is only e last'loop of the helix that has considerable contact with the vaporized fuel, affording some unreliability especially when he fuel comprises a heavier fuel oil.
Du ing operation, with the blower motor 16 operating, air is drawrLinto the housing 12, preferably by a ventilating air fan (not s own) near the air inlet of the blower assembly. A part of the air is drawn into the combustion air blower 20 through the opening 116 in-the center of the blower housing 22 and is forced into the primary and secondary air openings 68, 70 and 72 at the upstream end of the heat exchanger. The primary combustion air flows over the surface 48 of the porous wick 42 to rapidly remove vaporized liquid fuel therefrom and mix it readily with the combustion air. Momentary energization of the igniter or. spiral resistance heater 110 through leads 112 achieves immediate ignition of the fuel air mixture with burning being carried on within the area 90 within the cup-shaped member 62. Mixture of the fuel and air is enhanced, and recir- -culation insured by the presence of the small and larger cupefficiently heated prior to discharge through the downstream end 120 of the assembly.
The apparatus of the present invention is particularly applicable to the heating of ventilating air for a vehicle; however, the improved recirculating air, liquid fuel burner has application to many other fields requiring burners which operate efficiently with liquid fuels ranging from heavy oils to light gasolines.
In FIG. 4 an improved igniter assembly is illustrated therein by the reference character 122 for use in'a heater assembly such as and those parts similar or identical to those shown in heater 10 are given the same reference characters.
Thus, a support plate 40 is provided having a plurality of spaced openings as previously described. A plurality of studs such as 124 extend from the rim of a cup-shaped member 62 and are bolted to the support plate 40 to carry the cup-shaped member 62. The burner cup or member 62 as shown in FIG. 4
is provided with a short peripheral bead or flange extending radially outwardly with the terminating edge of the flange extending downstream.
A fuel inlet spud 44 extends through the central axis of plate 40 and coupling means 46 couples a fuel inlet pipe to the spud. A ceramic wick 42 is located adjacent the end of spud 44 and cross bored apertures 47 in spud. 44 serve to deliver fuel from the spud to the wick. The wick 42 is providedwith a central recess 126 at one end in which a pair of washers 56 are seated for butting the wick 42, which is clamped on spud 44 together with a small diameter cup-shaped member 60 by means of a screw 58. v
A small axially extending opening 128 is provided in the ceramic wick 42 along the vertical axis and above the midplane of the wick 42 and is aligned with openings in the washers 56 for receiving several strands 130 of a loop of conventional wicking material. The strands 130 extend upstream from the member 60 through an opening 132 in the support plate 40. Opening 132 is located above the central axis and along the vertical axis of the support plate 40 so that it is generally aligned with opening 128.
The igniter assembly 122 comprises a sheet metal housing 134 having semiannular wall 136 extending upstream from opening 132 and whose end is welded to plate 40 in alignment with the opening 132 with the ends of the semiannular wall 136 connected by a flat wall 138 alignedwith a straight portion of opening 132. The walls 136 and 138 at the ends opposite opening 132 terminate in a short annular wall section 140 extending both upwardly and upstream. The upper end of wall 140 terminates in a radially inwardly and downwardly directed flange 142 for receiving an igniter 110 having a spiral electrical resistance heater element 114 and similar to the igniter previously described but having a cup-shaped wall which fits snugly within the flange on wall 140 and an annular rear wall 142, which overlaps wall 140 and buttsagainst the end of wall section 140.
A wick support or retainer 142 of wire fastened to the flat wall 138 has an upwardly extending leg 144 at the end adjacent opening 132 terminating in a loop for supporting the wick strands 130 in front of the igniter 110 and'a hooklike leg 146 at the opposite or upstream end around which the strands 130 are looped so that the strands are held a short distance in front of the igniter 110.
The igniter is biased into the opening defined by wall 140 by a helical spring 148 received in wall 142, which spring together with the igniter leads 112 and are enclosed in an an-. nular housing 150 whose lower end telescopes over the wall 140. The housing 150 together with the fuel inlet pipe for spud 44 extend upwardly through appropriately sealed openings in a shroud 22 serving a similar function to the previously described shroud 22 but having a slightly different configuration.
The housing 150 is secured at its upper end by legs such as 152 to a wall 154 extending upwardly from and externally of the shroud 22 for enclosing the housing 150 between the shroud and the outer wall 12. A cup-shaped wall or cap 156 fits telescopingly'in the upper end of housing 150 for restraining the end of spring 148 to apply a force for holding the igniter in the opening defined by wall 140. J-shapedslots such as 158 in the upper end of housing 150 permit the cap 156 to be retainedin position in response to the insertion of a rod or projections 160 on cap 156 in the slots and rotation of the cap to place the projections 160 in the hook portion of slots 158 and effect a bayonet-type connection.
A central aperture in the backwall of cap 156 permits the electrical leads 112 to be extended from the igniter through a suitable opening in a removable cover plate 162 carried on the outer burner wall 12 to a suitable power supply.
Thus, access to the igniter 110 for easy servicing or replacement is provided by simply removing the cover plate 162 usually after leads 112 are detached from the power source. The cap 156 is rotated to align the rod 160 with the vertical straight leg of the J-slots 158 to permit withdrawal of cap 156 and spring 148 from housing 150. The igniter 110 may then be lifted by means of the leads from housings 150 and 154 and either serviced or replaced as the case may be. The igniter 110 and spring 148 are then simply positioned in housing 150 and the cap 156 replaced to cause the spring 148 to hold the igniter 1 10 in position and the cover plate replaced.
In the arrangement shown in FIGS. 4 and 5 the strands of wicking material conduct fuel to the igniter 110 in its recessed position sothat the igniter may initiate the combustion cycle. When a flame is established by the igniter in housing 134 a small jet of flame extends through the opening 132 and ignites the fuel transmitted through wick 42 to ignite the main flame. With the main flame in operation, the fuel is vaporized relatively rapidly and does not soak back through strands 130 and into the area in front of the igniter 1 10, so that area stays dry and free of carbon. Since the igniter 110 is relatively remote from the main area of combustion and is located in an area from which heat is conducted, it cools rapidly after combustion is initiated since the flame is transferred from the housing 134 with consequent extension of the igniter life.
While the invention has been particularly shown and described with reference to a preferred embodiment, it will be understood by those skilled in the art that the foregoing and other changes in the form and details may be made therein without departing from the spirit and scope of the invention.
What is claimed is:
1. In a fuel burner assembly including casing means forming a combustion chamber and blower means for forcing combustion air longitudinally therethrough, the improvement comprising: a transverse, apertured plate for directing combustion chamber inlet air along prescribed longitudinal paths, a first cup-shaped member coaxially positioned downstream of said plate with the open end thereof directed toward said incoming combustion air, a ceramic wick coaxially carried by said assembly on the downstream side of said plate, within said cup-shaped member and spaced axially and radially therefrom, means for delivering liquid fuel to said porous wick member, and an electrical resistance coil for igniting said fuel lying in a plane located axially upstream from said plate.
2. The assembly claimed in claim 1 wherein a strand of wicking material connects fuel from said ceramic wick to said igniter.
3. The assembly as claimed in claim 1 in which said re-.
sistance element comprises a spiral turn of aluminum, iron, chromium, cobalt and tantalate alloy wire.
4. In the assembly as claimed in claim 1, means for communicating fuel through said plate to said igniter.
5. The assembly claimed in claim 2 in which said communicating means comprises an opening in said plate and a first housing extending at one end from said plate opening and having an opening for receiving said igniter at a position spaced from said plate opening.
6. In the assembly claimed in claim 5, a spring for biasing said igniter toward said housing opening, a second housing encircling said spring and having one end telescopingly received by said first housing and encircling each electrical lead extending to said igniter, the opposite end of said housing accessible from a position external said casing, and a cap for said housing other end biased by said spring into locked position and rotatable for disengagement from said other end to facilitate removal of said spring and igniter from said other housing.
7. In a fuel burner assembly having a wall defining a combustion chamber and blower means for driving air in a stream from one end of said chamber toward the other end, the improvement comprising a plate adjacent said one end of said chamber with said plate having a plurality of apertures therein at one radial distance from the axis of said plate and with a second plurality of apertures therein at a different radial distance from said axis for passing combustion air, a fuel inlet conduit passing through the axis of said plate and terminating in said chamber, a wick in said chamber and extending radially from said conduit, means for communicating fuel from said conduit to said wick, a shield spaced adjacent the downstream end of said wick and having a greater radial dimension than said wick, a cup-shaped member spaced downstream from said shield and extending radially beyond said shield with the open end of said cup facing upstream, and a coil located upstream of said plate and spaced from said plate for igniting the fuel transmitted from said conduit to said wick.
8. In the assembly claimed in claim 7, a strand of wicking material extending from said wick through said plate to a position adjacent said coil.
9. In the assembly claimed in claim 7, housing means extending through said airstream, and manually movable means in said housing means for retaining said coil in said plane and operable for enabling withdrawal of said coil through said housing to a position external said assembly.
10. In a fuel assembly having a wall defining a combustion chamber and blower means for driving air in a stream from one end of said chamber toward the other end, the improvementcomprising a plate adjacent said one end of said chamber, means associated with said plate forpassing both combustion air and fuel into said chamber to develop a flame in said chamber, a coil of electrical resistance wire arranged solely in a spiral to initiate said flame, and means detachably fixing said coil upstream from said plate.
11. In a fuel burner assembly having a wall defining a combustion chamber and blower means for driving air in a stream from one end of said chamber toward the other end, the improvement comprising a plate adjacent said one end of said chamber, means associated with said plate for passing both combustion air and fuel into said chamber upstream of said plate to develop a flame in said chamber, a coil of electrical resistance wire arranged solely in a spiral to initiate said flame and located upstream of said plate, and means for passing fuel from said chamber through said plate to the vicinity of said coil.
12. The assembly claimed in claim 11 in which said means for passing fuel to said chamber includes a wick in said chamber, and said means for passing fuel through said plate comprises an opening in said plate, a housing having an open end connected to said opening, and a wicking material interconnected with said wick and extending through said opening into said housing.
13. The assembly claimed in claim 12 in which said coil of spiral wire is located adjacent the end of said housing opposite said open end.
14. In the assembly claimed in claim 7, housing means communicating with the end of said housing opposite said open end and extending through said airstream, manually movable means in said housing means for retaining said spiral coil adjacent the end of said housing opposite said open end and operable for enabling withdrawal of said spiral coil through said housing to a position external said assembly.

Claims (14)

1. In a fuel burner assembly including casing means forming a combustion chamber and blower means for forcing combustion air longitudinally therethrough, the improvement comprising: a transverse, apertured plate for directing combustion chamber inlet air along prescribed longitudinal paths, a first cup-shaped member coaxially positioned downstream of said plate with the open end thereof directed toward said incoming combustion air, a ceramic wick coaxially carried by said assembly on the downstream side of said plate, within said cup-shaped member and spaced axially and radially therefrom, means for delivering liquid fuel to said porous wick member, and an electrical resistance coil for igniting said fuel lying in a plane located axially upstream from said plate.
2. The assembly claimed in claim 1 wherein a strand of wicking material connects fuel from said ceramic wick to said igniter.
3. The assembly as claimed in claim 1 in which said resistance element comprises a spiral turn of aluminum, iron, chromium, cobalt and tantalate alloy wire.
4. In the assembly as claimed in claim 1, means for communicating fuel through said plate to said igniter.
5. The assembly claimed in claim 2 in which said communicating means comprises an opening in said plate and a first housing extending at one end from said plate opening and having an opening for receiving said igniter at a position spaced from said plate opening.
6. In the assembly claimed in claim 5, a spring for biasing said igniter toward said housing opening, a second housing encircling said spring and having one end telescopingly received by said first housing and encircling each electrical lead extending to said igniter, the opposite end of said housing accessible from a position external said casing, and a cap for said housing other end biased by said spring into locked position and rotatable for disengagement from said other end to facilitate removal of said spring and igniter from said other housing.
7. In a fuel burner assembly having a wall defining a combustion chamber and blower means for driving air in a stream from one end of said chamber toward the other end, the improvement comprising a plate adjacent said one end of said chamber with said plate having a plurality of apertures therein at one radial distance from the axis of said plate and with a second plurality of apertures therein at a different radial distance from said axis for passing combustion air, a fuel inlet conduit passing through the axis of said plate and terminating in said chamber, a wick in said chamber and extending radially from said conduit, means for communicating fuel from said conduit to said wick, a shield spaced adjacent the downstream end of said wick and having a greater radial dimension than said wick, a cup-shaped member spaced downstream from said shield and extending radially beyond said shield with the open end of said cup facing upstream, and a coil located upstream of said plate and spaced from said plate for igniting the fuel transmitted from said conduit to said wick.
8. In the assembly claimed in claim 7, a strand of wicking material extending from said wick through said plate to a position adjacent said coil.
9. In the assembly claimed in claim 7, housing means extending through said airstream, and manually movable means in said housing means for retaining said coil in said plane and operable for enabling withdrawal of said coil through said housing to a position External said assembly.
10. In a fuel assembly having a wall defining a combustion chamber and blower means for driving air in a stream from one end of said chamber toward the other end, the improvement comprising a plate adjacent said one end of said chamber, means associated with said plate for passing both combustion air and fuel into said chamber to develop a flame in said chamber, a coil of electrical resistance wire arranged solely in a spiral to initiate said flame, and means detachably fixing said coil upstream from said plate.
11. In a fuel burner assembly having a wall defining a combustion chamber and blower means for driving air in a stream from one end of said chamber toward the other end, the improvement comprising a plate adjacent said one end of said chamber, means associated with said plate for passing both combustion air and fuel into said chamber upstream of said plate to develop a flame in said chamber, a coil of electrical resistance wire arranged solely in a spiral to initiate said flame and located upstream of said plate, and means for passing fuel from said chamber through said plate to the vicinity of said coil.
12. The assembly claimed in claim 11 in which said means for passing fuel to said chamber includes a wick in said chamber, and said means for passing fuel through said plate comprises an opening in said plate, a housing having an open end connected to said opening, and a wicking material interconnected with said wick and extending through said opening into said housing.
13. The assembly claimed in claim 12 in which said coil of spiral wire is located adjacent the end of said housing opposite said open end.
14. In the assembly claimed in claim 7, housing means communicating with the end of said housing opposite said open end and extending through said airstream, manually movable means in said housing means for retaining said spiral coil adjacent the end of said housing opposite said open end and operable for enabling withdrawal of said spiral coil through said housing to a position external said assembly.
US874130A 1969-11-05 1969-11-05 Recirculating fuel burner Expired - Lifetime US3602621A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4105393A (en) * 1973-12-07 1978-08-08 Consultant Gas Engineer Limited Fuel burners
US5249956A (en) * 1992-12-04 1993-10-05 The United States Of America As Represented By The Secretary Of The Army Multifuel heater
EP0594988A1 (en) * 1992-10-28 1994-05-04 Mikuni Adec Corporation A vaporizing type burner
EP0922594A2 (en) * 1997-12-09 1999-06-16 Mikuniadec Corporation Automotive evaporation combustion heater
EP1610061A2 (en) 2004-06-22 2005-12-28 J. Eberspächer GmbH & Co. KG Fuel vaporization device
US20080110157A1 (en) * 2006-04-03 2008-05-15 Thomas Winter Apparatus/method for producing hot gas and diesel particulate filter system

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4105393A (en) * 1973-12-07 1978-08-08 Consultant Gas Engineer Limited Fuel burners
EP0594988A1 (en) * 1992-10-28 1994-05-04 Mikuni Adec Corporation A vaporizing type burner
US5249956A (en) * 1992-12-04 1993-10-05 The United States Of America As Represented By The Secretary Of The Army Multifuel heater
EP0922594A2 (en) * 1997-12-09 1999-06-16 Mikuniadec Corporation Automotive evaporation combustion heater
EP0922594A3 (en) * 1997-12-09 2002-06-19 Mikuniadec Corporation Automotive evaporation combustion heater
EP1610061A2 (en) 2004-06-22 2005-12-28 J. Eberspächer GmbH & Co. KG Fuel vaporization device
EP1610061A3 (en) * 2004-06-22 2008-10-08 J. Eberspächer GmbH & Co. KG Fuel vaporization device
US20080110157A1 (en) * 2006-04-03 2008-05-15 Thomas Winter Apparatus/method for producing hot gas and diesel particulate filter system
US20080202105A1 (en) * 2006-04-03 2008-08-28 Twk Engineering Entwicklungstechnik Gbr Apparatus/method for producing hot gas and diesel particulate filter system
US8001773B2 (en) * 2006-04-03 2011-08-23 Twk Engineering Entwicklungstechnik Gbr Apparatus/method for producing hot gas and diesel particulate filter system
US8020377B2 (en) * 2006-04-03 2011-09-20 Twk Engineering Entwicklungstechnik Gbr Apparatus/method for producing hot gas and diesel particulate filter system

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