CA2361730C - Fuel air magnetic system - Google Patents
Fuel air magnetic system Download PDFInfo
- Publication number
- CA2361730C CA2361730C CA 2361730 CA2361730A CA2361730C CA 2361730 C CA2361730 C CA 2361730C CA 2361730 CA2361730 CA 2361730 CA 2361730 A CA2361730 A CA 2361730A CA 2361730 C CA2361730 C CA 2361730C
- Authority
- CA
- Canada
- Prior art keywords
- fuel
- magnets
- magnet
- inlet line
- magnetic system
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- 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
A fuel-treating device called Fuel Air Magnetic System comprises two pairs of magnets, one paired positioned on each inlet for fuel and oxygen so that the incoming fuel is exposed to a magnetic field. Each pair of magnets are positioned diametrically opposed about the inlet line with the north magnetic pole of each magnet placed upstream closest to the mixing zone.
Description
Fuel Air Magnetia System Device ftELD OF THE tNENE11L310N
i,Uo-.J The present Fnverrtion relates generafly an improvement in fuel combustion chamber to a longitudinal magnetic field_ The invention more particularly relates to ptacing a pair magnets substantially diametricafly opposed around the fuel and oxygen inlet lines so that the north magnetic pole ofeach magnet is thrthest from the combustion chamber_ ~n j3AGKGROUND OF THE INVENTION
i,Uo-.J The present Fnverrtion relates generafly an improvement in fuel combustion chamber to a longitudinal magnetic field_ The invention more particularly relates to ptacing a pair magnets substantially diametricafly opposed around the fuel and oxygen inlet lines so that the north magnetic pole ofeach magnet is thrthest from the combustion chamber_ ~n j3AGKGROUND OF THE INVENTION
(002] With the increase in fuel cost and the increase In environmental consciousness, many devices to improve fuef economy or to reduce pollution have arisen_ From our investigations many patents requests have been using magnetism to improve combustion with not a great amount of success. After many attempts of designing the positioning of the magnets and devetopment of manufacturing of the magnet the last three3 years, it was found that by using the north pole of the magnets to treat the fuel in the southem hemisphere and the south pole of the magnet to treat the air in the norihem hemisphere, fuel economy is improved_ Other samples of dewices that have deployed rnagnetism to improve fuel combustion are:
-M3] U.S. PatNo_ 4,050,426 Sanderson M4] U.S. Pat No. 3,349,354 'M'rya'ta 5[0053 U.S. Pat No. 3,266,7$3 KrrigFrt '[0p6] U.S. Pat_ No_ 3,177,633 Mc'Donald ['0073 U.S. f'at. 'No. 3,118,726 Kwartz 10081 U.S Pat No. 3,059,910 91orrya SUMMARY OF TWE 94VEN'TtaN
1.010091 A fuel air magnetic system device for a cambustion chamber with a hydrocarbonfuel inlet line and an oxygen inlet line has a pair of substantially diametrically opposed magnets longitudinally positioned around the fuel fFntet Eine with the north rrragnetic pole of each magnet located the closest to the combustion chamber.
15f0010l In a preferred enybodiment, non magnetic spacers to retain the magnets substantially diametricaRy opposed.
-M3] U.S. PatNo_ 4,050,426 Sanderson M4] U.S. Pat No. 3,349,354 'M'rya'ta 5[0053 U.S. Pat No. 3,266,7$3 KrrigFrt '[0p6] U.S. Pat_ No_ 3,177,633 Mc'Donald ['0073 U.S. f'at. 'No. 3,118,726 Kwartz 10081 U.S Pat No. 3,059,910 91orrya SUMMARY OF TWE 94VEN'TtaN
1.010091 A fuel air magnetic system device for a cambustion chamber with a hydrocarbonfuel inlet line and an oxygen inlet line has a pair of substantially diametrically opposed magnets longitudinally positioned around the fuel fFntet Eine with the north rrragnetic pole of each magnet located the closest to the combustion chamber.
15f0010l In a preferred enybodiment, non magnetic spacers to retain the magnets substantially diametricaRy opposed.
(OOf 1) In an a-temate errrbodiment; eacri rrragrret is an electromagnet.
[0012] The pairs of magnets are positioned about the inlets with clamps.
[()01;i] In yet another embodiment of the fuel air magnetic system device for an automobile intemal combustion engine having a combustion chamber, a 5 hydrocarbonfuef inlet line, and an air inlet Gne, there is a pair of substantialty diametricaly opposed, longitudinal, permanent magnets longitudinally positioned around the fuel inlet iine, with the north magnetie pole of each magnet located closest to the combustion chamber. A pair Qf substantiaily diarnetricafly opposed, iongituqinal, permanent magnets IongitudinaNy posiiioned around the air inlet line, with the south magnetic pole of each rtldgnet located closest to the combustion chamber, wherein each rrtagnet has a curie temperature sufficiently high that the magnet retains its magnetic characteristics at the Qperafrng temperatures of the engine and wherein each magnet is positioned as close to the combustion chamber.
[0014] The device is retrofit to an engine by attaching the magnets in their locations on the air and fuel iniets with a clamp.
10015.1 The ciamp includes rrreans fvr ensuring that the magnets remain substantiaity diametrkaitiy opposed about their respective iniet.
BRiEE DESCRIPTION Oi' ME DRAWING
[0016] Fig. I Schematic view of the invention.
[0012] The pairs of magnets are positioned about the inlets with clamps.
[()01;i] In yet another embodiment of the fuel air magnetic system device for an automobile intemal combustion engine having a combustion chamber, a 5 hydrocarbonfuef inlet line, and an air inlet Gne, there is a pair of substantialty diametricaly opposed, longitudinal, permanent magnets longitudinally positioned around the fuel inlet iine, with the north magnetie pole of each magnet located closest to the combustion chamber. A pair Qf substantiaily diarnetricafly opposed, iongituqinal, permanent magnets IongitudinaNy posiiioned around the air inlet line, with the south magnetic pole of each rtldgnet located closest to the combustion chamber, wherein each rrtagnet has a curie temperature sufficiently high that the magnet retains its magnetic characteristics at the Qperafrng temperatures of the engine and wherein each magnet is positioned as close to the combustion chamber.
[0014] The device is retrofit to an engine by attaching the magnets in their locations on the air and fuel iniets with a clamp.
10015.1 The ciamp includes rrreans fvr ensuring that the magnets remain substantiaity diametrkaitiy opposed about their respective iniet.
BRiEE DESCRIPTION Oi' ME DRAWING
[0016] Fig. I Schematic view of the invention.
[00171 Fig. 2 f-erspeciive view of a magnet.
(qO18] Fig. 3 Front view of magnets on an air intake fine_ f00191 Fig. 4 Front view of magnets on a fuel intake line, DETAILED DESCRIP DN
(qO18] Fig. 3 Front view of magnets on an air intake fine_ f00191 Fig. 4 Front view of magnets on a fuel intake line, DETAILED DESCRIP DN
5(00201 The fuel air magnetic system device of this invention may be used in any combustion devfce. That is any combustion device where hydrocarbon fuel and an oxygen-containing fluid are mixed prior to combustion. Pairs of magnets are mounted on the isliets before the mixing prior to combustion. Pairs of magnets also are mounted on the inlets before the mixing zone to densify the fuels to promote more efficient combustion.
Fuel economy is increased and polkrEants are decreased. In achieving a system that operates effectively, it has been found that the magnets need to be placed on both the hydrocarbon fuel inlet and the oxygen inlet. Magnetizing only the oxygen or the hydrocarbon inlet fails to achieve the best combustion efficiency. Also, it has been found that the magnets need to be particularly oriented to achieve the optimal efficiency. Referring now to fig. 1, a pair of longitudinat magnets is posiiioned about the fuel fine of an interrtal combustion engine. Each rrtagnet has its north pole upstream from the carburetor or EFI. Fuel passes initially through the {fux of these opposed north poles, and then through the fieid of opposed south poles. The magnets shouid be placed as close to the mixing zone as possible. The magnets on an intemal-combustion engine are positioned after the fuel fifter and fuel pump. If the engine were a diesel they would be placed next to the carburetor or 5 EFI. Because different sizes and types of engines consume at different rates and because various engines have different configuri3rtions, then the amount of magnets depending on the t9ow and size of the pipe results in the magnets giving better fuel economy and performance. As shown in ftg_ 1, for an intemai-combustion engine a pair of magnets is 1(? also positioned on the air line to expose the inlet oxygen to a magnetic field. These pair of magnets have the south pole of each magnet closest upstream to the carbunetor or EFI. The magnets are longitudinally positioned and are substarrEiagy diantetrfcally opposed to one another.
They are placed, as near to the carburetor or EFI as the air scoop will allow. Again, fine-tuning for the optimal positioning wiil be requfred as with the fuel inlet magnets.
[00211 1997 Ford Taurus SE 3.01. 200,000 km. A fuel pass ferrite magnet 40 x 25 x 10 mm using north pole of magnet was installed lengthwise along the length of the fuel line. A similar magnet, but using the south pole was used on the air iine as weiF. The diameter of the air line decides hdw many magnets to instafi_ Magnets irtstaiied on irecoming fuel line after ,o ~
the fi,el pump and fuelf iJter was as civse as possible to the EFI.
EXAMPL,B, 2 i00221 1994 Toyota PiGtcup 22 R 4 cybnder 112 horsepower 330,000km. The same type of installation was done as in example 1.The initial test showed a fuel consumption reduction of over 90%. Future testing wiil be done to examine pollutants.
[0023] As seen in the drawing each pair of magnets is held around the inlet with a clamp, keeping the magnets substantially diametrically opposed. As the clamp is tightened the spacers are compressed to assure that a locking frt is attained. This type of clamp leads to no modifica4on to the engine and are commonly available, and are thus inexpensive.
15[0024] The practical aspect of this invention should not be timited to auto motive engines. The magnets densify the incoming fuels to allow more efficient and cleaner combustion. They may be placed on any inlet line after the fuel pump and the air filter, closer to the carburetor or EFI for a complete bum off aF air and fuel.
[00251 After carefuily looking at our system, it can be seen that there are few modifications to the preferred embodiment shown and described. But this invention should not f'imit itself to what is iESustrated in the fgures.
Fuel economy is increased and polkrEants are decreased. In achieving a system that operates effectively, it has been found that the magnets need to be placed on both the hydrocarbon fuel inlet and the oxygen inlet. Magnetizing only the oxygen or the hydrocarbon inlet fails to achieve the best combustion efficiency. Also, it has been found that the magnets need to be particularly oriented to achieve the optimal efficiency. Referring now to fig. 1, a pair of longitudinat magnets is posiiioned about the fuel fine of an interrtal combustion engine. Each rrtagnet has its north pole upstream from the carburetor or EFI. Fuel passes initially through the {fux of these opposed north poles, and then through the fieid of opposed south poles. The magnets shouid be placed as close to the mixing zone as possible. The magnets on an intemal-combustion engine are positioned after the fuel fifter and fuel pump. If the engine were a diesel they would be placed next to the carburetor or 5 EFI. Because different sizes and types of engines consume at different rates and because various engines have different configuri3rtions, then the amount of magnets depending on the t9ow and size of the pipe results in the magnets giving better fuel economy and performance. As shown in ftg_ 1, for an intemai-combustion engine a pair of magnets is 1(? also positioned on the air line to expose the inlet oxygen to a magnetic field. These pair of magnets have the south pole of each magnet closest upstream to the carbunetor or EFI. The magnets are longitudinally positioned and are substarrEiagy diantetrfcally opposed to one another.
They are placed, as near to the carburetor or EFI as the air scoop will allow. Again, fine-tuning for the optimal positioning wiil be requfred as with the fuel inlet magnets.
[00211 1997 Ford Taurus SE 3.01. 200,000 km. A fuel pass ferrite magnet 40 x 25 x 10 mm using north pole of magnet was installed lengthwise along the length of the fuel line. A similar magnet, but using the south pole was used on the air iine as weiF. The diameter of the air line decides hdw many magnets to instafi_ Magnets irtstaiied on irecoming fuel line after ,o ~
the fi,el pump and fuelf iJter was as civse as possible to the EFI.
EXAMPL,B, 2 i00221 1994 Toyota PiGtcup 22 R 4 cybnder 112 horsepower 330,000km. The same type of installation was done as in example 1.The initial test showed a fuel consumption reduction of over 90%. Future testing wiil be done to examine pollutants.
[0023] As seen in the drawing each pair of magnets is held around the inlet with a clamp, keeping the magnets substantially diametrically opposed. As the clamp is tightened the spacers are compressed to assure that a locking frt is attained. This type of clamp leads to no modifica4on to the engine and are commonly available, and are thus inexpensive.
15[0024] The practical aspect of this invention should not be timited to auto motive engines. The magnets densify the incoming fuels to allow more efficient and cleaner combustion. They may be placed on any inlet line after the fuel pump and the air filter, closer to the carburetor or EFI for a complete bum off aF air and fuel.
[00251 After carefuily looking at our system, it can be seen that there are few modifications to the preferred embodiment shown and described. But this invention should not f'imit itself to what is iESustrated in the fgures.
Claims (7)
1. A fuel air magnetic system device for a combustion chamber having a hydrocarbon fuel inlet line and an oxygen inlet line comprising;
a pair of substantially diametrically opposed magnets longitudinally positioned around the fuel inlet line with the north magnetic pole of each magnet located the closest to the combustion chamber.
a pair of substantially diametrically opposed magnets longitudinally positioned around the fuel inlet line with the north magnetic pole of each magnet located the closest to the combustion chamber.
2. A fuel air magnetic system device as in claim 1 wherein:
non magnetic spacers to retain the magnets diametrically opposed are provided.
non magnetic spacers to retain the magnets diametrically opposed are provided.
3. A fuel air magnetic system device as in claim 1 wherein:
each magnet is an electromagnet.
each magnet is an electromagnet.
4. A fuel air magnetic system device as in claim 2 wherein:
the pairs of magnets are positioned about the inlets with clamps.
the pairs of magnets are positioned about the inlets with clamps.
5. A fuel air magnetic system device for an automobile internal combustion engine having a combustion chamber, a hydrocarbon fuel inlet line, and an air inlet line, comprising:
a pair of substantially diametrically opposed, longitudinal, permanent magnets longitudinally positioned around the fuel inlet line, with the north magnetic pole of each magnet located closest to the combustion chamber;
a pair of substantially diametrically opposed, longitudinal, permanent magnets longitudinally positioned around the air inlet line, with the south magnetic pole of each magnet located closest to the combustion chamber, wherein each magnet has a curie temperature sufficiently high that the magnet retains its magnetic characteristics at the operating temperatures of the engine and wherein each magnet is positioned as close to the combustion chamber.
a pair of substantially diametrically opposed, longitudinal, permanent magnets longitudinally positioned around the fuel inlet line, with the north magnetic pole of each magnet located closest to the combustion chamber;
a pair of substantially diametrically opposed, longitudinal, permanent magnets longitudinally positioned around the air inlet line, with the south magnetic pole of each magnet located closest to the combustion chamber, wherein each magnet has a curie temperature sufficiently high that the magnet retains its magnetic characteristics at the operating temperatures of the engine and wherein each magnet is positioned as close to the combustion chamber.
6. A fuel air magnetic system device as in claim 5 wherein:
the device is retrofit to an engine by attaching the magnets in their locations on the air and fuel inlets with a clamp.
the device is retrofit to an engine by attaching the magnets in their locations on the air and fuel inlets with a clamp.
7. A fuel air magnetic system device as in claim 6 wherein:
the clamp includes means for ensuring that the magnets remain substantially diametrically opposed about their respective inlet.
the clamp includes means for ensuring that the magnets remain substantially diametrically opposed about their respective inlet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA 2361730 CA2361730C (en) | 2001-10-29 | 2001-10-29 | Fuel air magnetic system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA 2361730 CA2361730C (en) | 2001-10-29 | 2001-10-29 | Fuel air magnetic system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2361730A1 CA2361730A1 (en) | 2003-04-29 |
| CA2361730C true CA2361730C (en) | 2009-01-27 |
Family
ID=4170462
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA 2361730 Expired - Fee Related CA2361730C (en) | 2001-10-29 | 2001-10-29 | Fuel air magnetic system |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2361730C (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7918920B2 (en) | 2007-10-01 | 2011-04-05 | David De John | Assembly and process for improving combustion emissions of a combustion apparatus |
-
2001
- 2001-10-29 CA CA 2361730 patent/CA2361730C/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2361730A1 (en) | 2003-04-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4461262A (en) | Fuel treating device | |
| US5129382A (en) | Combustion efficiency improvement device | |
| US4572145A (en) | Magnetic fuel line device | |
| US4538582A (en) | Method of combusting fuel in an internal combustion engine and its apparatus | |
| US6041763A (en) | Fuel line enhancer | |
| US7331336B2 (en) | Power air-fuel levitation compression | |
| MY120017A (en) | Device for reducing toxic exhaust gases of diesel engines | |
| US5127385A (en) | Magnetic apparatus for treating fuel | |
| US6901917B2 (en) | Device for saving fuel and reducing emissions | |
| CA2361730C (en) | Fuel air magnetic system | |
| US5243946A (en) | Apparatus for the magnetic treatment of fuel | |
| GB2155993A (en) | Magnetic treatment of i.c. engine fuel | |
| CN203670035U (en) | Novel emission-reducing and oil-saving booster for internal combustion engine | |
| RU2307258C2 (en) | Device for magnetic treatment of liquid fuel | |
| EP0101515B1 (en) | Device for use with the intake manifold of an internal combustion engine | |
| SU968502A1 (en) | Device for magnetically treating flow of fuel mixture in internal combustion engine | |
| EP0930431A3 (en) | Intake system for an internal combustion engine with at least two cylinders | |
| CN2200057Y (en) | Magnetic fuel-economizing device | |
| CN2338499Y (en) | Apparatus for eliminating pollution and energy-saving for engine | |
| AU2001258057B2 (en) | Device for saving fuel and reducing emissions | |
| SU1213231A1 (en) | Diesel-generator set | |
| CZ20024092A3 (en) | Device for economy of fuel and reduction of emissions | |
| CZ266191A3 (en) | apparatus for magnetic treatment of a gaseous or liquid medium, particularly of fuel | |
| AU2001258057A1 (en) | Device for saving fuel and reducing emissions | |
| PL176686B1 (en) | Method of and apparatus for correlating composition and flow dynamisc of air-fuel mixture with magnetohydrodynamical properties of magnetised fuel in combustion engines |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |
Effective date: 20151029 |