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US4359997A Expired / Lapsed US ⏱️ 0.0 years remaining

Fixed blade turbulence generator

Assignee: HIGHT HENRY
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Filing: 1980-12-24
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Granted: 1982-11-23
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Expires: 2000-12-24
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Abstract

Abstract A device and method for installing a device for improving the fuel/air mixture in internal combustion engines with or without a fuel injection system. An intermediate member operatively dispositioned between the engine intake manifold and the intake port comprises at least two helically twisted blades attached to the inner bore of an intake port opening in the intermediate member; these blades are angled in relation to the fuel/air flow path and twisted so as to impart a swirling to the fuel/air mixture. In fuel injected systems, the swirl is imparted to the air flow just prior to encountering the umbrella mist injected to the intake port by the fuel injector. The swirl mixing of the fuel/air improves engine performance, reduces pollutants, and increases gas mileage. Further, in fuel injection systems, the device reduces or eliminates the common occurrence of a burned intake valve caused by a clogged injector.

Inventors

  • 👤 Norbert G. Lyssy

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 14:54
CPC Classifications
F; F02; F02M; F02M29/00; F02M29/04; F02M29/06

Claims Analysis

Total Claims: 14
Claim 1
Independent Claim 129 words
A device for improving fuel/air mixing in an internal combustion engine comprising: at least two helically twisted blades positioned in an inner bore of an intake port opening, said helically twisted blades being attached to the inner circumference of an opening in an intermediate member operatively dispositioned between an engine intake manifold and an intake port, said helically twisted blades extending into a portion of an intake manifold passage and also extending into a portion of an intake port passage; said helically twisted blades angled between 30° and 60° in relation to a fuel/air flow path through said inner bore and said intermediate member; said helically twisted blades having leading edges at an angle greater than 20°, but less than 60° to trailing edges of said helically twisted blades.
Claim 2
Independent Claim 129 words
A device for improving fuel/air mixing in an internal combustion engine comprising: at least two helically twisted blades positioned in an inner bore of an intake port opening, said helically twisted blades being attached to the inner circumference of an opening in an intermediate member operatively dispositioned between an engine intake manifold and an intake port, said helically twisted blades extending into a portion of an intake manifold passage and also extending into a portion of an intake port passage; said helically twisted blades angled between 30° and 60° in relation to a fuel/air flow path through said inner bore and said intermediate member; said helically twisted blades having leading edges at an angle greater than 20°, but less than 60° to trailing edges of said helically twisted blades.
Claim 3
Dependent Claim 19 words
The device of claim 1 wherein a face of said helically twisted blades is a partial sine wave configuration.
Claim 4
Dependent Claim 14 words
The device of claim 2 wherein said intermediate member is a manifold alignment ring.
Claim 5
Dependent Claim 15 words
The device of claim 2 wherein said intermediate member is an engine intake manifold gasket.
Claim 6
Dependent Claim 23 words
The device of claim 4 wherein said engine intake manifold gasket has multiple bores corresponding to each intake port in a multi-cylinder engine.
Claim 7
Independent Claim 159 words
A device for improving fuel/air mixing in an internal combustion engine incorporating a fuel injection system comprising: at least two helically twisted blades positioned in an inner bore of an intake port opening; said helically twisted blades being attached to the inner circumference of an opening in an intermediate member operatively dispositioned in an oversized intake manifold port opening in an engine intake manifold gasket; said intake manifold gasket being positioned between an engine intake manifold and an intake port; said helically twisted blades extending into a portion of an engine intake manifold passage and also extending into a portion of an intake port passage and being generally angled at 45° in relation to an air flow path through said inner bore and said intermediate member; said helically twisted blades having leading edges being generally angled at 45° to trailing edges of said helically twisted blades; said helically twisted blades having a face in a partial sine wave configuration.
Claim 8
Independent Claim 159 words
A device for improving fuel/air mixing in an internal combustion engine incorporating a fuel injection system comprising: at least two helically twisted blades positioned in an inner bore of an intake port opening; said helically twisted blades being attached to the inner circumference of an opening in an intermediate member operatively dispositioned in an oversized intake manifold port opening in an engine intake manifold gasket; said intake manifold gasket being positioned between an engine intake manifold and an intake port; said helically twisted blades extending into a portion of an engine intake manifold passage and also extending into a portion of an intake port passage and being generally angled at 45° in relation to an air flow path through said inner bore and said intermediate member; said helically twisted blades having leading edges being generally angled at 45° to trailing edges of said helically twisted blades; said helically twisted blades having a face in a partial sine wave configuration.
Claim 9
Independent Claim 197 words
A method for retro-fitting an internal combustion engine for improved fuel/air mixing comprising the following steps: a first removing of an engine intake manifold; a second removing of an engine intake manifold gasket; cleaning said engine intake manifold and an engine head on which said engine intake manifold gasket was mounted to provide smooth mating surfaces; installing a device for improving fuel/air mixing, said device comprising at least two helically twisted blades positioned in an inner bore of an intake port opening, said helically twisted blades being attached to the inner circumference of an opening in an intermediate member being secured between the engine intake manifold and intake port, said helically twisted blades extending into a portion of an engine intake manifold passage and also extending into a portion of an intake port passage and being angled between 30° and 60° in relation to a fuel/air flow path through said inner bore of said intake port opening; said helically twisted blades having leading edges at an angle greater than 20° but less than 60° to trailing edges of said helically twisted blades; first reinstalling of said engine intake manifold gasket; second reinstalling of said engine intake manifold.
Claim 10
Independent Claim 197 words
A method for retro-fitting an internal combustion engine for improved fuel/air mixing comprising the following steps: a first removing of an engine intake manifold; a second removing of an engine intake manifold gasket; cleaning said engine intake manifold and an engine head on which said engine intake manifold gasket was mounted to provide smooth mating surfaces; installing a device for improving fuel/air mixing, said device comprising at least two helically twisted blades positioned in an inner bore of an intake port opening, said helically twisted blades being attached to the inner circumference of an opening in an intermediate member being secured between the engine intake manifold and intake port, said helically twisted blades extending into a portion of an engine intake manifold passage and also extending into a portion of an intake port passage and being angled between 30° and 60° in relation to a fuel/air flow path through said inner bore of said intake port opening; said helically twisted blades having leading edges at an angle greater than 20° but less than 60° to trailing edges of said helically twisted blades; first reinstalling of said engine intake manifold gasket; second reinstalling of said engine intake manifold.
Claim 11
Dependent Claim 18 words
The method of claim 7 including shaping a face of said blades in a partial sine wave configuration.
Claim 12
Independent Claim 230 words
A method for retro-fitting an internal combustion engine for improved fuel/air mixing comprising the following steps: a first removing of an engine intake manifold; a second removing of an engine intake manifold gasket; a third removing of a manifold alignment ring; cleaning said engine intake manifold and an engine head on which said engine intake manifold gasket was mounted to provide smooth mating surfaces; a first reinstalling of said engine intake manifold gasket; a second reinstalling of a modified manifold alignment ring for improving fuel/air mixing, said modified manifold alignment ring comprising at least two helically twisted blades, said helically twisted blades being attached to the inner circumference of said modified manifold alignment ring and being located in an inner bore of an intake port opening by said modified manifold alignment ring, said modified manifold alignment ring being secured between said engine intake manifold and said intake port opening, said helically twisted blades extending into a portion of an engine intake manifold passage and also extending into a portion of an intake port passage and being angled between 30° and 60° in relation to a fuel/air flow path through said inner bore of said intake port opening, said helically twisted blades having leading edges at an angle greater than 20°, but less than 60° to trailing edges of said helically twisted blades; a third reinstalling of said engine intake manifold.
Claim 13
Independent Claim 230 words
A method for retro-fitting an internal combustion engine for improved fuel/air mixing comprising the following steps: a first removing of an engine intake manifold; a second removing of an engine intake manifold gasket; a third removing of a manifold alignment ring; cleaning said engine intake manifold and an engine head on which said engine intake manifold gasket was mounted to provide smooth mating surfaces; a first reinstalling of said engine intake manifold gasket; a second reinstalling of a modified manifold alignment ring for improving fuel/air mixing, said modified manifold alignment ring comprising at least two helically twisted blades, said helically twisted blades being attached to the inner circumference of said modified manifold alignment ring and being located in an inner bore of an intake port opening by said modified manifold alignment ring, said modified manifold alignment ring being secured between said engine intake manifold and said intake port opening, said helically twisted blades extending into a portion of an engine intake manifold passage and also extending into a portion of an intake port passage and being angled between 30° and 60° in relation to a fuel/air flow path through said inner bore of said intake port opening, said helically twisted blades having leading edges at an angle greater than 20°, but less than 60° to trailing edges of said helically twisted blades; a third reinstalling of said engine intake manifold.
Claim 14
Dependent Claim 47 words
The method for retro-fitting an internal combustion engine as recited in claim 8 wherein said intermediate member includes gasket means with opening therein for alignment with said inner bore, said gasket means having said helically twisted blades forming a part thereof and being positioned in said opening.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1985-11-22 1986-05-24 1986-11-23 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-11-22 1990-05-24 1990-11-23 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-11-22 1994-05-24 1994-11-23 $7700.00 Window Closed / Lapsed

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