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US4461262A Expired / Lapsed US ⏱️ 0.0 years remaining

Fuel treating device

Assignee: Individual
•
Filing: 1981-01-16
•
Granted: 1984-07-24
•
Expires: 2001-01-16
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Abstract

Abstract A fuel treating device comprises two pairs of magnets, one pair positioned on each inlet for fuel and oxygen so that the incoming fuel is exposed to a magnetic field. Each pair of magnets is positioned diametrically opposed about the inlet line with the south magnetic pole of each magnet placed upstream furthest away from the mixing zone. The magnets are insulated from each other and from the inlet line by nonmagnetic materials, such as Neoprene, which do not disrupt the magnetic field.

Inventors

  • 👤 Edward Chow

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 17:09
CPC Classifications
F; F23; F23K; F23K5/00; F23K5/02; F23K5/08; F02; F02M; F02M27/00; F02M27/04; F02M27/045; F02B; F02B3/00; F02B3/06

Claims Analysis

Total Claims: 16
Claim 1
Independent Claim 77 words
A fuel treating 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 south magnetic pole of each magnet located furthest from the combustion chamber; and a pair of substantially diametrically opposed magnets longitudinally positioned around the oxygen inlet line with the south magnetic pole of each magnet located furthest from the combustion chamber.
Claim 2
Dependent Claim 77 words
A fuel treating 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 south magnetic pole of each magnet located furthest from the combustion chamber; and a pair of substantially diametrically opposed magnets longitudinally positioned around the oxygen inlet line with the south magnetic pole of each magnet located furthest from the combustion chamber.
Claim 3
Dependent Claim 20 words
The fuel treating device as defined in claim 1, further comprising nonmagnetic spacers to retain the magnets substantially diametrically opposed.
Claim 4
Dependent Claim 20 words
The fuel treating device of claim 1 or claim 2 wherein each magnet has a layer of insulation enclosing it.
Claim 5
Dependent Claim 27 words
The fuel treating device of claim 1 or claim 2 wherein the fuel inlet line and oxygen inlet line are insulated from direct contact with the magnets.
Claim 6
Dependent Claim 33 words
The fuel treating device of claim 1 wherein the magnets are permanent magnets having a Curie temperature sufficiently high that they retain their magnetic characteristics at the operating temperature of the combustion chamber.
Claim 7
Dependent Claim 13 words
The fuel treating device of claim 1 wherein each magnet is an electromagnet.
Claim 8
Dependent Claim 19 words
The fuel treating device of claim 1 wherein the combustion chamber is in an internal-combustion engine including a carburetor.
Claim 9
Dependent Claim 27 words
The fuel treating device of claim 7 wherein the magnets are positioned as close to the carburetor as possible without modifying the standard components of the engine.
Claim 10
Dependent Claim 20 words
The fuel treating device of claim 2 wherein the pairs of magnets are positioned about the inlets with hose clamps.
Claim 11
Dependent Claim 130 words
A fuel treating 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 south magnetic pole of each magnet located furthest from the combustion chamber; and a pair of substantially diametrically opposed, longitudinal, permanent magnets longitudinally positioned arount the air inlet line, with the south magnetic pole of each magnet located furthest from 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 as possible without modifying the standard components of the engine.
Claim 12
Dependent Claim 130 words
A fuel treating 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 south magnetic pole of each magnet located furthest from the combustion chamber; and a pair of substantially diametrically opposed, longitudinal, permanent magnets longitudinally positioned arount the air inlet line, with the south magnetic pole of each magnet located furthest from 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 as possible without modifying the standard components of the engine.
Claim 13
Dependent Claim 31 words
The device of claim 10 wherein the device is retrofit to an engine by attaching the magnets in their proper locations on the air and fuel inlets with a suitable clamp.
Claim 14
Dependent Claim 23 words
The deivce of claim 11 wherein the clamp includes means for ensuring that the magnets remain substantially diametrically opposed about their respective inlet.
Claim 15
Dependent Claim 35 words
The device of claim 12 wherein the clamp is a hose clamp, the means for ensuring the positioning include nonmagnetic spacers, and the magnets include a layer of insulation to substantially completely encapsulate each magnet.
Claim 16
Dependent Claim 21 words
The device of claim 13 wherein each inlet includes a layer of insulation in the area where the magnets are positioned.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-07-24 1988-01-23 1988-07-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-07-24 1992-01-23 1992-07-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-07-24 1996-01-23 1996-07-24 $7700.00 Window Closed / Lapsed

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