CA2535798C - Fuel treatment device using a magnetic field - Google Patents
Fuel treatment device using a magnetic field Download PDFInfo
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- CA2535798C CA2535798C CA2535798A CA2535798A CA2535798C CA 2535798 C CA2535798 C CA 2535798C CA 2535798 A CA2535798 A CA 2535798A CA 2535798 A CA2535798 A CA 2535798A CA 2535798 C CA2535798 C CA 2535798C
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- fuel
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- channel
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- housing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M27/00—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like
- F02M27/04—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like by electric means, ionisation, polarisation or magnetism
- F02M27/045—Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like by electric means, ionisation, polarisation or magnetism by permanent magnets
Abstract
Magnetic fuel treatment devices are disclosed, the devices comprising, in part, a housing (11), cover (30), inner compartment, and magnet (21), the combination of which forming an inner fuel channel (40) through which fuel may flow for treatment therein. Certain aspects of the invention include designs that concentrate fuel flow within magnetic flux densities ranging from about 600 to about 1,200 Gauss.
Description
FUEL TREATMENT DEVICE USING A MAGNETIC FIELD
BACKGROUND AND SUMMARY OF THE INVENTION:
Refining methods employed in the late 20'~ and early 21St centuries produce hydrocarbon fuels and oils that are unstable. Such instability results in polymerization and agglomerations of organic compounds that reduce filterability and clean combustion of diesel fuels and gas-oil. In the case of hydrocarbon fuels, asphaltenes (precursors to heavy hydrocarbon oils) and resins have mechanical affinity for each other and thereby have a tendency to form flocculations or aggregations. As these clusters of large molecules increase in size, they clog fuel filters and can eventually contribute to sludge in fuel storage tanks.
Fuel treatment methods have worked from the premise that filterability problems with diesel fuel were largely due to "bio-fouling" (i.e. microbial activity from fungus, yeast, mold, and aerobic or anaerobic sulfur-reducing bacteria). Although microbial activity plays a role in the deterioration of fuel quality and may contribute to repolymerization, it is not the sole cause of fuel instability.
Magnetic fuel treatment has focused on passing fuel through a weak magnetic field (with flux density of 200 to 500 gauss) for the purpose of improving fuel filtration and alleviating the filter clogging believed to be caused by microbial contaminant build-up. Even though results have shown some improvement in fuel filterability, current methods have not been able to address the larger issues of fuel stability.
Magnetic field flux density varies depending on the magnetic material used, the shape of the magnet, the positioning of the poles, and proximity to the poles.
At the atomic level, inductive forces are transmitted to a fluid passing through magnetic flux, producing an orientation effect on polar molecules in the fuel, and thus discourages clustering of paraffins and other long chain molecules, allowing them, as a consequence, to stay in suspension and thus burn more completely. The strength of this effect depends on the direction of fluid flow relative to flux lines, as well as velocity of flow and magnetic flux density. Research and field trials conducted by the inventor have shown that fuel channel design can be altered to optimize the orientation effect beyond that of current treatment devices, thereby producing unexpected improvements in fuel combustion and filterability.
The present invention, in certain aspects, is directed to a fuel treatment device comprising a housing, the housing further comprising an inner compartment, a fuel entry port, and a fuel exit port. The inner compartment includes a substantially circular side wall, a lower floor integral with the side wall, and a raised platform integral with the floor. The inner compartment further comprises a central post integral with and extending from the platform, with the post having a diameter smaller than the diameter of the platform. The central platform, in combination with the circular side wall and lower floor, form a substantially C-shaped groove defined in a transverse cross-section taken through the housing. The device further includes a circular magnet housed within the inner compartment, the magnet comprising a central opening sufficiently sized to accommodate the central post. The magnet also includes upper and lower surfaces, an outer side surface defining the circumference of the magnet, and a thickness measured vertically from the lower surface to the upper surface along the outer side walls of the magnet, such that when the magnet is placed within the housing, the post is contained within the central opening of the magnet and the lower surface of the magnet is positioned upon the platform. The device also comprises a cover secured to the housing.
The cover has an inner surface comprising a substantially C-shaped groove corresponding to the C-shaped groove of the inner compartment, such that the grooves of the cover and inner compartment, in combination with the outer side surface of the magnet, form a fuel channel through which fuel flows from the entry port and out of the exit port. The fuel channel has an area defined by a vertical cross-section taken through said housing. In this aspect of the invention, the maximum distance between the surfaces of the magnet (i.e. outer side surface and lower surface) and the side wall and lower floor of the inner compartment, respectively, is from about 17% to about 31% of the thickness of the magnet. Moreover, the maximum distance between the upper surface of the magnet and the inner groove of the cover is from about 17% to about 31 % of the thickness of the magnet.
In another aspect of the present invention, the fuel treatment device comprises a housing as described above, with the fuel entry and exit ports oriented in registration with one another through opposite walls of the housing and in communication with the inner compartment. Here, the entry and exit ports each have a port area defined by the formula Er2, wherein r is the radius of the two-dimensional circle defined by the ports. The inner compartment comprises a substantially circular side wall, a lower floor integral with the side wall, and a raised platform integral with the floor, the platform having a centrally positioned, substantially circular portion and an arm integral with and extending from the circular portion of the platform. The arm portion is also integral with a portion of the side wall and positioned between the entry and exit ports. The inner compartment further comprises a central post integral with and extending from the platform as described above, wherein the post has a diameter smaller than the platform diameter, and wherein the central platform, in combination with the circular side wall and lower floor of the inner compartment, form a substantially C-shaped groove defined in transverse cross-section taken through the housing. A circular magnet is housed within the inner compartment as described above such that the magnet completely covers the platform, thereby obstructing fuel flow directly between the entry and exit ports when fuel is introduced therein. The device further includes a cover secured to the housing, the cover configured as described above. The fuel channel formed by the respective grooves of cover and inner compartment in combination with the magnet has an area defined by a vertical cross-section taken through the housing. The fuel channel area:port area ratio in this embodiment ranges from about 0.65:1 to 2.5:1.
Other aspects of the present invention, either alone or combination with the features described above, include the inner compartment platform, the platform of the inner surface of the cover, and the magnet being dimensioned such that from about 17%
to about 31 % of the magnet's upper and/or lower surface is covered by the one or both platforms. Similarly, device is so dimensioned such that from about 50% to about 70%, preferably about 58%, of all of the magnet's surfaces are exposed to fuel flowing through the device. Such designs serve to concentrate fuel flow within the device to areas of greatest flux density for improved treatment thereof. Finally, in certain aspects of the present invention, fuel flow is concentrated within an area of greatest magnetic flux density, the flux density ranging from about 600 to about 1,200 Gauss.
BRIEF DESCRIPTION OF THE DRAWINGS:
Fig. 1 is a top view of the housing of the device (without cover) showing the magnet contained therein.
Fig. 2 is a side sectional view of the housing illustrated in Fig. 10, with a portion of the magnet cut away to show the fuel entry port.
Fig. 3 is side view identical to that shown in Fig. 2, but referencing additional features of the device.
Fig. 4 is a side sectional view of the housing illustrated in Fig. 1, but without the magnet.
Fig. S is a side sectional view identical to that shown in Fig. 4, but referencing additional features of the device.
Fig. 6 is a sectional view of the fuel channel (hatched lines) illustrated in Fig. 2.
Fig. 7 is a sectional view identical to that shown in Fig. 6, but referencing additional features ofthe device.
Fig. 8 is a top view of the cover.
Fig. 9 is a bottom view of the cover illustrated in Fig. 8, showing the inner surface of the cover.
Fig. 10 is a top view of the device with the cover secured thereto, with the magnet and a portion of the inner compartment shown in phantom.
Fig. 11 is a top view of the magnet.
Fig. 12 is a flow chart of an exemplary engine system employing the inventive fuel treatment device.
DETAILED DESCRIPTION OF THE EMBODIMENTS OF THE INVENTION:
The present invention is directed to a fuel treatment device, in particular a fuel treatment device that utilizes a magnetic field effective in improving combustion and filterability of conventional petroleum-based hydrocarbon fuels (i.e. fossil fuels).
Referring now to the figures, the invention in certain aspects comprises a fuel treatment device 10 comprising a housing 11, the housing further having an inner compartment 12. The housing 11 also has a fuel entry port 13 and a fuel exit port 14, which in the embodiments illustrated in the figures, are in registration with one another.
When the device is installed within a fuel line, the fuel line is split so that it may be connected to the fuel entry and exit parts. Fig. 1 illustrates the fuel entry port 13, for example, as being positioned on the right side of the housing; however, it will be appreciated by the skilled artisan that these fuel ports may be reversed (i.e.
the entry port may be where the exit port 14 is shown). Fig. 2 shows the entry port 13, which has circular configuration. The area of the port is defined by F~, wherein "r" is the radius of the two-dimensional circle of the port formed in cross section (see Fig. 4, for example).
The inner compartment 12 within the device housing has a substantially circular side wall 15 when viewed from the top (Fig. 1). The inner compartment further includes a lower floor 16, and in a preferred embodiment, a central platform 17 integral therewith.
In the embodiments shown herein, the platform has a circular portion 17b and an arm portion 17a integral with and extending therefrom. The arm portion is also integral with a portion of the side wall 15 of the inner compartment and positioned between the fuel entry and exit ports 13,14, as shown in Figs. 1-.4, for example. Extending from the central platform is a post I8 having a diameter Dl smaller than the diameter Di of the platform. As shown in the figures, the combination of the platform 17, side wall 15, and lower floor 16 form a substantially C-shaped groove 20 defined in transverse cross section take through the housing, as best illustrated in Fig. 1.
The device includes a circular magnet 21 (e.g. a ceramic 8 type magnet) housed within the inner compartment (in Figs. 1 and 10, the magnet is shown in phantom). The magnet has a central opening 22 sufficiently sized to accommodate the central post 18 of the housing. The magnet includes upper 23 and lower 24 surfaces as well as an outer surface 25 defining the circumference of the magnet when viewed from above (see Fig.
11 ). When the magnet is placed within the inner compartment of the housing, with the post 18 engaged within the central opening 22, the lower surface of the magnet is positioned upon the platform 17 to completely cover the platform, thereby obstructing fuel flow directly between the entry and exit ports.
The device also includes a cover 30 having a top surface 31 (Fig. 8) and an inner surface 32 (Fig. 9). The cover may be removably secured to the housing by any conventional fastening means, including, but not limited to, screws, bolts, pins, and the like. If screws 60, for example, are used to fasten the cover to the housing, a series of bores 33 are provided on the cover and a complementary series of threaded bores 34 are provided through the upper surface of the housing (Fig. 1), in registration with the cover bores 33, to engage the screws. As most clearly illustrated in Fig. 9, the inner surface 32 of the cover has a substantially C-shaped groove 35 corresponding to the C-shaped groove 20 of inner compartment of the housing, such that the grooves 20, 35, in combination with the surfaces of the magnet, form a fuel channel 40, as shown in Figs. 2-4. The fuel channel (shown in hatched lines in Figs. 6-7) has an area defined by a two-dimensional vertical cross-section taken through the housing.
O-rings may be used to form a seal between the cover and housing in order to prevent fuel leakage from the housing. In Fig. 9, elastomeric O-rings may be placed in circular grooved areas 50, 51.
In previous devices known in the art, the fuel treatment area (i.e. fuel channel area) had been in the order of 3.5 times larger than the engine's fuel line area (i.e. fuel entry port area). That is, the fuel channel area: fuel line (i.e. fuel entry port) area ratio is around 3.5:1 in some current magnetic fuel treatment devices. In one aspect of the present invention, the fuel channel area is reduced, thereby resulting in an improvement in filterability of the fuel. Thus, a preferred fuel channel to port area ratio is from about 0.65:1 to 2.5:1.
It has fiuther been discovered by the inventor that inducing turbulence in the fluid flow further enhances the combustibility of magnetically treated fuel. Prior devices in the art have aimed to maintain laminar flow of fluid through the device; however, in the present invention, a narrower fuel channel (i.e. a channel width: exposed magnet width w ratio of less than 2.5:1, more preferably about 1.4:1 or less) (Figs. 3 and 6).
Similarly, in previous devices, the maximum distance between the outer surface of magnet and the sides of the fuel treatment channel is from 75% to 300% of the magnet's thickness. In one aspect of the present invention, the range for the maximum distance between the magnet's outer surface and the wall of the fuel channel (designed d2, d3, and d4 in Figs. 6-7 for ease of illustration) is from about 17% to about 30% of the magnet's thickness T. In particular, when this feature is combined with the reduced fuel channel area:fuel entry port area, such that a fuel within the device is concentrated or focused within the area of greatest magnetic flux density (i.e. about 600 to about 1,200 Gauss), with the unexpected result that the asphaltenes and waxes within the fuel (i.e.
organic hydrocarbon compounds in crude oil and refined diesel and fuel-oil) are thereby affected to prevent their aggregation downstream. The inventor has discovered that such compounds are indeed only affected or influenced by magnetic fields stronger than the 200-500 Gauss range found in current magnetic fuel treatment devices.
Consequently, the design of the inventive fuel treatment device provides a stronger magnetic field for fuel treatment, thereby improving combustibility of the treated fuel.
Aspects of the present invention further include a fuel treatment device having a central platform, post, and magnet disposed upon the platform and post as described above; however, the magnet and platform are dimensioned such that about 50% to about 75%, preferably about 68%, of the lower surface of the magnet is covered by the platform. Similarly, the inner surface of the cover, which comprises a C-shaped groove described above that is defined in part by a centrally positioned raised platform 34, is sufficiently sized with respect to the magnet such that about 50% to 75%, preferably about 68%, of the magnet's upper surface is covered by the cover platform 34, thereby concentrating fuel flow within the device to areas of greatest flux density.
Prior embodiments shield only about 19% of the magnet's outer surfaces. In combination, from about 50% to about 70%, more preferably about 58%, of the magnet's entire upper, lower, and outer surfaces are exposed to fuel flowing through the device (compared to up to about 87% average total exposure), thereby concentrating the fuel flow within the device to areas of greatest flux density for the benefits described herein.
The present invention may be used to treat fuel for use in a variety of applications.
The invention may be installed in a motorized vehicle or other system powered by a fuel-operated engine generator. Preferably, the inventive fuel treatment device is installed between the fuel tank and primary filter assembly (Fig. 12). Fuel flows through the fuel entry port, through the fuel channel, and exits the exit port. While in the channel, the fuel is subjected to the magnetic field at a given velocity (e.g. 1-15 ft/sec, preferably 1-6 ft./sec) and dwell time (e.g. 0.1 to 1 second), depending upon the size of the fuel treatment device.
It will be appreciated by those of ordinary skill in the art that the dimensions of the inventive treatment device may be varied, with larger housings, for example, being employed for larger fuel engine systems, although various preferred ratios and percentages described herein remain the same. In a preferred commercial embodiment, the dimensions of the fuel channel, in the cross-section shown in Figs. 6-7, 0.500 in (dl) X 0.265 in (d2) X 0.250 in. (d3) X 0.245 in. (d4) X 0.500 in. (ds). A
preferred size of magnet is 3.38 in (total diameter) X 1.280 in (ring width) X 0.85 in (ring thickness or height), with a total surface area of 24.3 square inches.
The foregoing disclosure and description of the invention are illustrative and explanatory thereof, and various changes with respect to the size, shape, and materials, as well as in the details of the illustrated construction may be made without departing from the spirit of the invention, and therefore fall within the scope of the appended claims even though such variations were not specifically discussed above.
BACKGROUND AND SUMMARY OF THE INVENTION:
Refining methods employed in the late 20'~ and early 21St centuries produce hydrocarbon fuels and oils that are unstable. Such instability results in polymerization and agglomerations of organic compounds that reduce filterability and clean combustion of diesel fuels and gas-oil. In the case of hydrocarbon fuels, asphaltenes (precursors to heavy hydrocarbon oils) and resins have mechanical affinity for each other and thereby have a tendency to form flocculations or aggregations. As these clusters of large molecules increase in size, they clog fuel filters and can eventually contribute to sludge in fuel storage tanks.
Fuel treatment methods have worked from the premise that filterability problems with diesel fuel were largely due to "bio-fouling" (i.e. microbial activity from fungus, yeast, mold, and aerobic or anaerobic sulfur-reducing bacteria). Although microbial activity plays a role in the deterioration of fuel quality and may contribute to repolymerization, it is not the sole cause of fuel instability.
Magnetic fuel treatment has focused on passing fuel through a weak magnetic field (with flux density of 200 to 500 gauss) for the purpose of improving fuel filtration and alleviating the filter clogging believed to be caused by microbial contaminant build-up. Even though results have shown some improvement in fuel filterability, current methods have not been able to address the larger issues of fuel stability.
Magnetic field flux density varies depending on the magnetic material used, the shape of the magnet, the positioning of the poles, and proximity to the poles.
At the atomic level, inductive forces are transmitted to a fluid passing through magnetic flux, producing an orientation effect on polar molecules in the fuel, and thus discourages clustering of paraffins and other long chain molecules, allowing them, as a consequence, to stay in suspension and thus burn more completely. The strength of this effect depends on the direction of fluid flow relative to flux lines, as well as velocity of flow and magnetic flux density. Research and field trials conducted by the inventor have shown that fuel channel design can be altered to optimize the orientation effect beyond that of current treatment devices, thereby producing unexpected improvements in fuel combustion and filterability.
The present invention, in certain aspects, is directed to a fuel treatment device comprising a housing, the housing further comprising an inner compartment, a fuel entry port, and a fuel exit port. The inner compartment includes a substantially circular side wall, a lower floor integral with the side wall, and a raised platform integral with the floor. The inner compartment further comprises a central post integral with and extending from the platform, with the post having a diameter smaller than the diameter of the platform. The central platform, in combination with the circular side wall and lower floor, form a substantially C-shaped groove defined in a transverse cross-section taken through the housing. The device further includes a circular magnet housed within the inner compartment, the magnet comprising a central opening sufficiently sized to accommodate the central post. The magnet also includes upper and lower surfaces, an outer side surface defining the circumference of the magnet, and a thickness measured vertically from the lower surface to the upper surface along the outer side walls of the magnet, such that when the magnet is placed within the housing, the post is contained within the central opening of the magnet and the lower surface of the magnet is positioned upon the platform. The device also comprises a cover secured to the housing.
The cover has an inner surface comprising a substantially C-shaped groove corresponding to the C-shaped groove of the inner compartment, such that the grooves of the cover and inner compartment, in combination with the outer side surface of the magnet, form a fuel channel through which fuel flows from the entry port and out of the exit port. The fuel channel has an area defined by a vertical cross-section taken through said housing. In this aspect of the invention, the maximum distance between the surfaces of the magnet (i.e. outer side surface and lower surface) and the side wall and lower floor of the inner compartment, respectively, is from about 17% to about 31% of the thickness of the magnet. Moreover, the maximum distance between the upper surface of the magnet and the inner groove of the cover is from about 17% to about 31 % of the thickness of the magnet.
In another aspect of the present invention, the fuel treatment device comprises a housing as described above, with the fuel entry and exit ports oriented in registration with one another through opposite walls of the housing and in communication with the inner compartment. Here, the entry and exit ports each have a port area defined by the formula Er2, wherein r is the radius of the two-dimensional circle defined by the ports. The inner compartment comprises a substantially circular side wall, a lower floor integral with the side wall, and a raised platform integral with the floor, the platform having a centrally positioned, substantially circular portion and an arm integral with and extending from the circular portion of the platform. The arm portion is also integral with a portion of the side wall and positioned between the entry and exit ports. The inner compartment further comprises a central post integral with and extending from the platform as described above, wherein the post has a diameter smaller than the platform diameter, and wherein the central platform, in combination with the circular side wall and lower floor of the inner compartment, form a substantially C-shaped groove defined in transverse cross-section taken through the housing. A circular magnet is housed within the inner compartment as described above such that the magnet completely covers the platform, thereby obstructing fuel flow directly between the entry and exit ports when fuel is introduced therein. The device further includes a cover secured to the housing, the cover configured as described above. The fuel channel formed by the respective grooves of cover and inner compartment in combination with the magnet has an area defined by a vertical cross-section taken through the housing. The fuel channel area:port area ratio in this embodiment ranges from about 0.65:1 to 2.5:1.
Other aspects of the present invention, either alone or combination with the features described above, include the inner compartment platform, the platform of the inner surface of the cover, and the magnet being dimensioned such that from about 17%
to about 31 % of the magnet's upper and/or lower surface is covered by the one or both platforms. Similarly, device is so dimensioned such that from about 50% to about 70%, preferably about 58%, of all of the magnet's surfaces are exposed to fuel flowing through the device. Such designs serve to concentrate fuel flow within the device to areas of greatest flux density for improved treatment thereof. Finally, in certain aspects of the present invention, fuel flow is concentrated within an area of greatest magnetic flux density, the flux density ranging from about 600 to about 1,200 Gauss.
BRIEF DESCRIPTION OF THE DRAWINGS:
Fig. 1 is a top view of the housing of the device (without cover) showing the magnet contained therein.
Fig. 2 is a side sectional view of the housing illustrated in Fig. 10, with a portion of the magnet cut away to show the fuel entry port.
Fig. 3 is side view identical to that shown in Fig. 2, but referencing additional features of the device.
Fig. 4 is a side sectional view of the housing illustrated in Fig. 1, but without the magnet.
Fig. S is a side sectional view identical to that shown in Fig. 4, but referencing additional features of the device.
Fig. 6 is a sectional view of the fuel channel (hatched lines) illustrated in Fig. 2.
Fig. 7 is a sectional view identical to that shown in Fig. 6, but referencing additional features ofthe device.
Fig. 8 is a top view of the cover.
Fig. 9 is a bottom view of the cover illustrated in Fig. 8, showing the inner surface of the cover.
Fig. 10 is a top view of the device with the cover secured thereto, with the magnet and a portion of the inner compartment shown in phantom.
Fig. 11 is a top view of the magnet.
Fig. 12 is a flow chart of an exemplary engine system employing the inventive fuel treatment device.
DETAILED DESCRIPTION OF THE EMBODIMENTS OF THE INVENTION:
The present invention is directed to a fuel treatment device, in particular a fuel treatment device that utilizes a magnetic field effective in improving combustion and filterability of conventional petroleum-based hydrocarbon fuels (i.e. fossil fuels).
Referring now to the figures, the invention in certain aspects comprises a fuel treatment device 10 comprising a housing 11, the housing further having an inner compartment 12. The housing 11 also has a fuel entry port 13 and a fuel exit port 14, which in the embodiments illustrated in the figures, are in registration with one another.
When the device is installed within a fuel line, the fuel line is split so that it may be connected to the fuel entry and exit parts. Fig. 1 illustrates the fuel entry port 13, for example, as being positioned on the right side of the housing; however, it will be appreciated by the skilled artisan that these fuel ports may be reversed (i.e.
the entry port may be where the exit port 14 is shown). Fig. 2 shows the entry port 13, which has circular configuration. The area of the port is defined by F~, wherein "r" is the radius of the two-dimensional circle of the port formed in cross section (see Fig. 4, for example).
The inner compartment 12 within the device housing has a substantially circular side wall 15 when viewed from the top (Fig. 1). The inner compartment further includes a lower floor 16, and in a preferred embodiment, a central platform 17 integral therewith.
In the embodiments shown herein, the platform has a circular portion 17b and an arm portion 17a integral with and extending therefrom. The arm portion is also integral with a portion of the side wall 15 of the inner compartment and positioned between the fuel entry and exit ports 13,14, as shown in Figs. 1-.4, for example. Extending from the central platform is a post I8 having a diameter Dl smaller than the diameter Di of the platform. As shown in the figures, the combination of the platform 17, side wall 15, and lower floor 16 form a substantially C-shaped groove 20 defined in transverse cross section take through the housing, as best illustrated in Fig. 1.
The device includes a circular magnet 21 (e.g. a ceramic 8 type magnet) housed within the inner compartment (in Figs. 1 and 10, the magnet is shown in phantom). The magnet has a central opening 22 sufficiently sized to accommodate the central post 18 of the housing. The magnet includes upper 23 and lower 24 surfaces as well as an outer surface 25 defining the circumference of the magnet when viewed from above (see Fig.
11 ). When the magnet is placed within the inner compartment of the housing, with the post 18 engaged within the central opening 22, the lower surface of the magnet is positioned upon the platform 17 to completely cover the platform, thereby obstructing fuel flow directly between the entry and exit ports.
The device also includes a cover 30 having a top surface 31 (Fig. 8) and an inner surface 32 (Fig. 9). The cover may be removably secured to the housing by any conventional fastening means, including, but not limited to, screws, bolts, pins, and the like. If screws 60, for example, are used to fasten the cover to the housing, a series of bores 33 are provided on the cover and a complementary series of threaded bores 34 are provided through the upper surface of the housing (Fig. 1), in registration with the cover bores 33, to engage the screws. As most clearly illustrated in Fig. 9, the inner surface 32 of the cover has a substantially C-shaped groove 35 corresponding to the C-shaped groove 20 of inner compartment of the housing, such that the grooves 20, 35, in combination with the surfaces of the magnet, form a fuel channel 40, as shown in Figs. 2-4. The fuel channel (shown in hatched lines in Figs. 6-7) has an area defined by a two-dimensional vertical cross-section taken through the housing.
O-rings may be used to form a seal between the cover and housing in order to prevent fuel leakage from the housing. In Fig. 9, elastomeric O-rings may be placed in circular grooved areas 50, 51.
In previous devices known in the art, the fuel treatment area (i.e. fuel channel area) had been in the order of 3.5 times larger than the engine's fuel line area (i.e. fuel entry port area). That is, the fuel channel area: fuel line (i.e. fuel entry port) area ratio is around 3.5:1 in some current magnetic fuel treatment devices. In one aspect of the present invention, the fuel channel area is reduced, thereby resulting in an improvement in filterability of the fuel. Thus, a preferred fuel channel to port area ratio is from about 0.65:1 to 2.5:1.
It has fiuther been discovered by the inventor that inducing turbulence in the fluid flow further enhances the combustibility of magnetically treated fuel. Prior devices in the art have aimed to maintain laminar flow of fluid through the device; however, in the present invention, a narrower fuel channel (i.e. a channel width: exposed magnet width w ratio of less than 2.5:1, more preferably about 1.4:1 or less) (Figs. 3 and 6).
Similarly, in previous devices, the maximum distance between the outer surface of magnet and the sides of the fuel treatment channel is from 75% to 300% of the magnet's thickness. In one aspect of the present invention, the range for the maximum distance between the magnet's outer surface and the wall of the fuel channel (designed d2, d3, and d4 in Figs. 6-7 for ease of illustration) is from about 17% to about 30% of the magnet's thickness T. In particular, when this feature is combined with the reduced fuel channel area:fuel entry port area, such that a fuel within the device is concentrated or focused within the area of greatest magnetic flux density (i.e. about 600 to about 1,200 Gauss), with the unexpected result that the asphaltenes and waxes within the fuel (i.e.
organic hydrocarbon compounds in crude oil and refined diesel and fuel-oil) are thereby affected to prevent their aggregation downstream. The inventor has discovered that such compounds are indeed only affected or influenced by magnetic fields stronger than the 200-500 Gauss range found in current magnetic fuel treatment devices.
Consequently, the design of the inventive fuel treatment device provides a stronger magnetic field for fuel treatment, thereby improving combustibility of the treated fuel.
Aspects of the present invention further include a fuel treatment device having a central platform, post, and magnet disposed upon the platform and post as described above; however, the magnet and platform are dimensioned such that about 50% to about 75%, preferably about 68%, of the lower surface of the magnet is covered by the platform. Similarly, the inner surface of the cover, which comprises a C-shaped groove described above that is defined in part by a centrally positioned raised platform 34, is sufficiently sized with respect to the magnet such that about 50% to 75%, preferably about 68%, of the magnet's upper surface is covered by the cover platform 34, thereby concentrating fuel flow within the device to areas of greatest flux density.
Prior embodiments shield only about 19% of the magnet's outer surfaces. In combination, from about 50% to about 70%, more preferably about 58%, of the magnet's entire upper, lower, and outer surfaces are exposed to fuel flowing through the device (compared to up to about 87% average total exposure), thereby concentrating the fuel flow within the device to areas of greatest flux density for the benefits described herein.
The present invention may be used to treat fuel for use in a variety of applications.
The invention may be installed in a motorized vehicle or other system powered by a fuel-operated engine generator. Preferably, the inventive fuel treatment device is installed between the fuel tank and primary filter assembly (Fig. 12). Fuel flows through the fuel entry port, through the fuel channel, and exits the exit port. While in the channel, the fuel is subjected to the magnetic field at a given velocity (e.g. 1-15 ft/sec, preferably 1-6 ft./sec) and dwell time (e.g. 0.1 to 1 second), depending upon the size of the fuel treatment device.
It will be appreciated by those of ordinary skill in the art that the dimensions of the inventive treatment device may be varied, with larger housings, for example, being employed for larger fuel engine systems, although various preferred ratios and percentages described herein remain the same. In a preferred commercial embodiment, the dimensions of the fuel channel, in the cross-section shown in Figs. 6-7, 0.500 in (dl) X 0.265 in (d2) X 0.250 in. (d3) X 0.245 in. (d4) X 0.500 in. (ds). A
preferred size of magnet is 3.38 in (total diameter) X 1.280 in (ring width) X 0.85 in (ring thickness or height), with a total surface area of 24.3 square inches.
The foregoing disclosure and description of the invention are illustrative and explanatory thereof, and various changes with respect to the size, shape, and materials, as well as in the details of the illustrated construction may be made without departing from the spirit of the invention, and therefore fall within the scope of the appended claims even though such variations were not specifically discussed above.
Claims (25)
CLAIMED ARE AS FOLLOWS:
1. A fuel treatment device comprising:
a housing, said housing further comprising a housing body, a housing cover, a fuel entry port, a fuel exit port and a generally arcuate fuel channel between the fuel entry port and the fuel exit port;
an annular magnet positioned within the housing, the magnet forming at least a portion of the arcuate fuel channel, the annular magnet having a central axis; and wherein the arcuate fuel channel has a single "C" shaped radial cross-section with respect to a central axis of the magnet, the channel having a radially inward circumferential portion and a radially outward circumferential portion, where the cross-section lies in a plane perpendicular to the central axis, and where surfaces of the magnet, the cover, and the edge of the platform form a portion of the radially inward circumferential portion of the C shaped arcuate fuel channel.
a housing, said housing further comprising a housing body, a housing cover, a fuel entry port, a fuel exit port and a generally arcuate fuel channel between the fuel entry port and the fuel exit port;
an annular magnet positioned within the housing, the magnet forming at least a portion of the arcuate fuel channel, the annular magnet having a central axis; and wherein the arcuate fuel channel has a single "C" shaped radial cross-section with respect to a central axis of the magnet, the channel having a radially inward circumferential portion and a radially outward circumferential portion, where the cross-section lies in a plane perpendicular to the central axis, and where surfaces of the magnet, the cover, and the edge of the platform form a portion of the radially inward circumferential portion of the C shaped arcuate fuel channel.
2. The fuel treatment device of claim 1, wherein a ratio of the radial cross-sectional area of the fuel channel to the cross-sectional area of the inlet port is 2.5:1 or less.
3. The fuel treatment device of claim 1 or 2, wherein the maximum radial distance or axial distance between the magnet and the housing forming the fuel channel is 30% of the thickness of the magnet.
4. The fuel treatment device of any one of claims 1 to 3, wherein less than 70% of the magnet surfaces form at least a portion of the fuel channel.
5. The fuel treatment device of any one of claims 1 to 4, wherein the annular magnet comprises a first planar surface opposite a second planar surface and an outer cylindrical surface and an inner cylindrical surface, and the fuel channel is formed by at least a portion of the outer cylindrical surface of the magnet.
6. The fuel treatment device of any one of claims 1 to 5, wherein the fuel channel is at least partially formed by a circumferential surface of the magnet, the fuel channel extending about the circumference of the magnet.
7. The fuel treatment device of any one of claims 1 to 6, wherein the magnet has a magnetic flux rating of at least 600 Gauss.
8. The fuel treatment device of any one of claims 1 to 7, wherein the ratio of the maximum radial width of the fuel channel to the radial width of the exposed magnet surface is about 1.4:1 or less.
9. The fuel treatment device of any one of claims 1 to 8, wherein the fuel entry port is separated from the fuel exit port by a baffle for directing the fuel into the arcuate fuel channel.
10. A fuel treatment device comprising:
a housing, said housing further comprising a housing body, a housing cover, a fuel entry port, a fuel exit port and a generally arcuate fuel channel between the fuel entry port and the fuel exit port;
an annular magnet positioned within the housing, the magnet obstructing fuel flow directly between the entry and the exit ports, the magnet forming the entire surface of a radially inward circumferential portion of the arcuate fuel channel, the annular magnet having a central axis;
wherein the arcuate fuel channel has a single "C" shaped radial cross-section with respect to a central axis of the magnet, the channel having a radially inward circumferential portion and a radially outward circumferential portion, where the cross-section lies in a plane perpendicular to the central axis, and where surfaces of the magnet, the cover and the edge of the platform form a portion of the radially inward circumferential portion of the C shaped arcuate fuel channel;
and wherein the maximum radial distance between the magnet and the housing forming the fuel channel is 30% of the thickness of the magnet.
a housing, said housing further comprising a housing body, a housing cover, a fuel entry port, a fuel exit port and a generally arcuate fuel channel between the fuel entry port and the fuel exit port;
an annular magnet positioned within the housing, the magnet obstructing fuel flow directly between the entry and the exit ports, the magnet forming the entire surface of a radially inward circumferential portion of the arcuate fuel channel, the annular magnet having a central axis;
wherein the arcuate fuel channel has a single "C" shaped radial cross-section with respect to a central axis of the magnet, the channel having a radially inward circumferential portion and a radially outward circumferential portion, where the cross-section lies in a plane perpendicular to the central axis, and where surfaces of the magnet, the cover and the edge of the platform form a portion of the radially inward circumferential portion of the C shaped arcuate fuel channel;
and wherein the maximum radial distance between the magnet and the housing forming the fuel channel is 30% of the thickness of the magnet.
11. The fuel treatment device of claim 10, wherein the fuel channel is formed by at least a portion of the outer cylindrical surface of the magnet.
12. The fuel treatment device of claim 10 or 11, wherein the arcuate fuel channel has a"C"
shaped radial cross-section with respect to the central axis of the magnet.
shaped radial cross-section with respect to the central axis of the magnet.
13. The fuel treatment device of any one of claims 10 to 12, wherein the ratio of the radial cross-sectional area of the fuel channel to the cross-sectional area of the inlet port is 2.5:1 or less.
14. The fuel treatment device of any one of claims 10 to 13, wherein 70% or less of the magnet surfaces form at least a portion of the fuel channel.
15. The fuel treatment device of any one of claims 10 to 14, wherein the fuel entry port is separated from the fuel exit port by a baffle for directing the fuel into the arcuate fuel channel.
16. The fuel treatment device of any one of claims 10 to 15, wherein the ratio of the maximum radial width of the fuel channel to the radial width of the exposed magnet surface is 1.4:1 or less.
17. A method for magnetically treating fuel comprising the steps of:
providing fuel treatment device comprising: a housing, said housing further comprising a housing body, a housing cover, a fuel entry port, a fuel exit port and a generally arcuate fuel channel between the fuel entry port and the fuel exit port; an annular magnet positioned within the housing, the magnet obstructing fuel flow directly between the entry and exit ports, the magnet forming at least a portion of the arcuate fuel channel, the annular magnet having a central axis; and wherein the arcuate fuel channel has a single "C" shaped radial cross-section with respect to a central axis of the magnet, the channel having a radially inward circumferential portion and a radially outward circumferential portion, where the cross-section lies in a plane traverse to the housing, and where surfaces of the magnet, the cover, and the edge of the platform form a portion of the radially inward circumferential portion of the C shaped arcuate fuel channel;
attaching a fuel line to the fuel entry port and the fuel exit port of the fuel treatment device;
forcing fuel in the fuel treatment device such that the fuel enters the fuel entry port and enters the arcuate fuel channel;
subjecting the fuel to a magnetic field created by the magnet while the fuel is in the fuel channel; and allowing the treated fuel to exit the fuel treatment device through the fuel exit port.
providing fuel treatment device comprising: a housing, said housing further comprising a housing body, a housing cover, a fuel entry port, a fuel exit port and a generally arcuate fuel channel between the fuel entry port and the fuel exit port; an annular magnet positioned within the housing, the magnet obstructing fuel flow directly between the entry and exit ports, the magnet forming at least a portion of the arcuate fuel channel, the annular magnet having a central axis; and wherein the arcuate fuel channel has a single "C" shaped radial cross-section with respect to a central axis of the magnet, the channel having a radially inward circumferential portion and a radially outward circumferential portion, where the cross-section lies in a plane traverse to the housing, and where surfaces of the magnet, the cover, and the edge of the platform form a portion of the radially inward circumferential portion of the C shaped arcuate fuel channel;
attaching a fuel line to the fuel entry port and the fuel exit port of the fuel treatment device;
forcing fuel in the fuel treatment device such that the fuel enters the fuel entry port and enters the arcuate fuel channel;
subjecting the fuel to a magnetic field created by the magnet while the fuel is in the fuel channel; and allowing the treated fuel to exit the fuel treatment device through the fuel exit port.
18. The method of claim 17 further comprising the step of keeping the fuel within the fuel channel within a maximum radial distance of not more than 31 % of the thickness of the magnet.
19. The method of claim 17 or 18, wherein the step subjecting the fuel to a magnetic field created by the magnet while the fuel is in the fuel channel is accomplished by having the fuel in direct contact with 70 percent or less of the magnet surfaces.
20. The method of any one of claims 17 to 19, wherein in the step of forcing fuel in the fuel treatment device such that the fuel enters the fuel entry port and enters the arcuate fuel channel, the arcuate channel includes an increased cross-sectional area fluid path, as defined by a ratio of the radial cross-sectional area of the fluid channel to the cross-sectional area of the fuel entry port, to not more than 2.5:1.
21. The fuel treatment device of any one of claims 1 to 9, wherein said entry and exit ports each having a port area defined by the formula .pi.r2.
22. The fuel treatment device of any one of claims 2 to 9 and 13 to 16, wherein the ratio of the radial cross-sectional area of the fuel channel to the cross-sectional area of the inlet port is from about 0.65:1 to about 2.5:1.
23. The fuel treatment device of any one of claims 4 to 9 and 14 to 16, wherein from about 50% to about 70% of the magnet surfaces form at least a portion of the fuel channel.
24. The fuel treatment device of claim 23, wherein about 58% of the magnet surfaces form at least a portion of the fuel channel.
25. The fuel treatment device of any one of claims 7 to 9 and 10 to 16, wherein the magnet has a magnetic flux rating ranging from about 600 Gauss to about 1,200 Gauss.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/462,026 US7004153B2 (en) | 2003-06-13 | 2003-06-13 | Fuel treatment device using a magnetic field |
| US10/462,026 | 2003-06-13 | ||
| PCT/US2004/018831 WO2004113708A2 (en) | 2003-06-13 | 2004-06-14 | Fuel treatment device using a magnetic field |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2535798A1 CA2535798A1 (en) | 2005-12-29 |
| CA2535798C true CA2535798C (en) | 2013-01-08 |
Family
ID=33511374
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2535798A Active CA2535798C (en) | 2003-06-13 | 2004-06-14 | Fuel treatment device using a magnetic field |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US7004153B2 (en) |
| EP (1) | EP1646774B1 (en) |
| CA (1) | CA2535798C (en) |
| ES (1) | ES2528480T3 (en) |
| WO (1) | WO2004113708A2 (en) |
| ZA (1) | ZA200510066B (en) |
Families Citing this family (7)
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| US7004153B2 (en) | 2003-06-13 | 2006-02-28 | Wout Lisseveld | Fuel treatment device using a magnetic field |
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| RU2447262C2 (en) | 2007-10-08 | 2012-04-10 | Джон Т. ХЕЙЛ | Method, device and magnet for magnetic treatment of fluids |
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| WO2010033171A1 (en) * | 2008-09-18 | 2010-03-25 | Wayne Roland | Fuel treatment device using heat and magnetic field |
| CA2692680C (en) * | 2010-02-11 | 2011-09-13 | J. William Clements | Magnetic fuel treatment method and apparatus |
| NL1042492B1 (en) * | 2017-08-04 | 2019-02-21 | Vhc Holding Bv | Magnetic treatment device for magnetically treating a fluid |
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-
2003
- 2003-06-13 US US10/462,026 patent/US7004153B2/en not_active Expired - Lifetime
-
2004
- 2004-06-14 EP EP04755171.8A patent/EP1646774B1/en active Active
- 2004-06-14 ES ES04755171.8T patent/ES2528480T3/en active Active
- 2004-06-14 WO PCT/US2004/018831 patent/WO2004113708A2/en active Application Filing
- 2004-06-14 CA CA2535798A patent/CA2535798C/en active Active
-
2005
- 2005-12-12 ZA ZA200510066A patent/ZA200510066B/en unknown
-
2006
- 2006-02-24 US US11/307,837 patent/US7621261B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP1646774B1 (en) | 2014-12-24 |
| ES2528480T3 (en) | 2015-02-10 |
| CA2535798A1 (en) | 2005-12-29 |
| US20060159562A1 (en) | 2006-07-20 |
| ZA200510066B (en) | 2007-03-28 |
| US7621261B2 (en) | 2009-11-24 |
| US7004153B2 (en) | 2006-02-28 |
| WO2004113708A2 (en) | 2004-12-29 |
| WO2004113708A3 (en) | 2005-06-16 |
| EP1646774A4 (en) | 2008-02-20 |
| EP1646774A2 (en) | 2006-04-19 |
| US20040250799A1 (en) | 2004-12-16 |
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