IP Library Granted Patent US 7,806,096
Granted Patent B2
US 7,806,096 · App. 11/810,212 · Granted Oct 5, 2010

In-line induction system for internal combustion engine

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,806,096
App. No.
11/810,212
Granted
Oct 5, 2010
Kind
B2
Abstract

In line carburetor ( 104 ) is mounted to a manifold ( 140 ) over the engine ( 800 ). The barrels of the carburetor deliver air/fuel suspensions to concentrated positions ( 152 ) of the manifold, with the concentrated positions being at opposite ends of the engine. The ports leading from the manifold to the runners are equally positioned about the concentrated positions ( 152 ) so that the runners are of substantially equal length and resistance, thereby providing more uniform delivery of the air/fuel suspension to the cylinders.

Claims (58)

1. An induction system for an internal combustion engine that includes combustion cylinders in banks arranged in a V-shaped orientation, said induction system comprising:

a carburetor including;

a plurality of barrels formed through a body of the carburetor, the barrels being aligned along a common plane of alignment such that the barrels are substantially arranged in a row, each barrel having a central axis that extends through substantially a center of the barrel from an entry to an exit of the barrel, the barrels being positioned within the carburetor body such that the central axes are substantially parallel to one another, the central axis of any one of the barrels and the common plane of alignment of all of the barrels that substantially bisects the barrels;

a plurality of butterfly valves, each barrel having one of the butterfly valves, each butterfly valve having a valve control shaft, the valve control shaft being substantially perpendicular to the bisecting plane that substantially bisects the barrels, each butterfly valve being one of a primary butterfly valve or a secondary butterfly valve, the primary butterfly valves beginning to open in advance of the secondary butterfly valves and opening at a slower rotational velocity than the secondary butterfly valves, the butterfly valves being arranged in pairs, each pair including one primary butterfly valve and one secondary butterfly valve, the primary butterfly valve of the pair opening in a direction of opening that is opposite from a direction of opening of the secondary butterfly valve of the pair, the butterfly valves of the pair rotating toward each other while opening to direct air and fuel suspension between the butterfly valves; and

a control linkage coupled to the valve control shafts of the butterfly valves that pivots the butterfly valves within the barrels to move the butterfly valves between opened and closed positions, the butterfly valves pivoting within the bisecting plane that substantially bisects the barrels,

the control linkage including a primary actuating lever for each primary butterfly valve, the primary actuating lever pivoting the valve control shaft of the primary butterfly valve to open the primary butterfly valve, each of the primary actuating levers being coupled together by a primary transfer linkage that transfers the motion of one primary actuating lever to the other primary actuating lever so that the primary butterfly valves open substantially in unison, the control linkage further including a secondary actuating lever for each secondary butterfly valve, the secondary actuating lever pivoting the valve control shaft of the secondary butterfly valve to open the secondary butterfly valve, each of the secondary actuating levers being coupled to the primary actuating lever that corresponds to the primary butterfly valve with which the secondary butterfly valve is a pair, the secondary transfer linkage having a fixed end and a movable end, the fixed end being coupled to a point on the primary actuating lever that moves away from the secondary actuating lever as the primary actuating rotates and the movable end being positioned in a slot on the secondary actuating lever, such that when the primary actuating lever rotates, the movable end translates along the slot toward the primary actuator, catches against the end of the slot and is pulled by the primary actuating lever in a direction of opening that is opposite from the direction of opening of the primary actuating lever, so that the secondary butterfly valve begins opening after the primary butterfly valve, and opens toward the primary butterfly valve; and

an intake manifold including;

a plenum that is about the same length and width as the carburetor body, the plenum having a central axis that is aligned with the bisecting plane of the carburetor and substantially bisects the plenum; and

a plurality of runners that are symmetrically disposed with respect to the bisecting plane, each of the runners being substantially the same length and extending from an opening in the plenum to an intake valve into a cylinder of the engine, the openings into half of the runners being located on either side of the bisecting plane, the openings being spaced along the bisecting plane in groups of two, each opening being substantially the same distance from the bisecting plane, each opening being angled away from the bisecting plane so that a bottom of the opening is farther away from the bisecting plane than a top of the opening;

wherein the induction system is mounted on the engine having combustion cylinders in banks arranged in a V-shaped orientation, the carburetor being mounted above the intake manifold and the intake manifold being mounted on an engine block of the engine and spanning between two cylinder banks of the engine, such that the common axis of alignment of the carburetor barrels and the central axis of the plenum of the intake manifold are aligned along the bisecting pane, the carburetor creating an air and fuel suspension that is combusted within cylinders positioned within the cylinder banks, the air and fuel suspension being fed from the barrels of the carburetor into the plenum along the central axis and into runners, a path from the central axis to an intake valve of the cylinder being substantially the same length for each runner.

2. An induction system for a V-8 combustion engine having banks of cylinders arranged in a V-shape, with a first four cylinders at one end portion of the engine and a second four cylinders at the other end of the engine, the induction system comprising:

a four barrel carburetor body having in sequence first, second, third and fourth barrels, with the barrels arranged in a row,

a first and third barrels comprising primary barrels and the second and fourth barrels comprising secondary barrels,

butterfly valves in alignment with each of the barrels for controlling the air/fuel streams passing through the barrels,

a valve linkage connected to the butterfly valves and configured for opening the butterfly valves of the primary barrels and for opening the butterfly valves of the secondary barrels after the butterfly valves of the primary barrels are opened.

3. The induction system for a V-8 combustion engine as set forth in claim 2 , wherein the valve linkage is configured to rotate the butterfly valves of the primary barrels in opposite directions from the rotation of the butterfly valves of the secondary barrels.

4. The induction system for a V-8 combustion engine of claim 2 , wherein the barrels are arranged in a common plane and the control linkage is configured to tilt the butterfly valves about axes transverse to the common plane of the barrels.

5. The induction system for a V-8 combustion engine of claim 3 , and further including an intake manifold in communication with the barrels of the carburetor for receiving air/fuel streams from the carburetor, and with induction runners extending from the intake manifold to the cylinders of the engine for delivering air/fuel streams from the intake manifold to the cylinders of the engine.

6. The induction system for a V-8 combustion engine as described in claim 5 , wherein the induction runners are substantially of equal length.

7. The induction system for a V-8 combustion engine as described in claim 5 , wherein:

the intake manifold has opposed first and second ends, with the first end of the intake manifold in communication with the first and second barrels of the carburetor and the second end of the intake manifold in communication with the third and fourth barrels of the carburetor,

the induction runners are arranged in a first group of four runners and a second group of four runners, with the first group of four runners in communication with the first end of the induction manifold and the first four cylinders of the engine and the second group of four runners in communication with the second end of the induction manifold and the second group of four cylinders of the engine.

8. An induction system for an internal combustion engine with an even number of cylinders, the cylinders of the engine being arranged in two banks of cylinders in a V-shaped configuration with one another, with a first half of the cylinders at one end of the engine and a second half of the cylinders at the other end of the engine, said induction system comprising:

a carburetor for mounting to the engine, said carburetor including;

four open ended barrels extending through the carburetor, all of the barrels being aligned along a common plane for extending between the two banks of the engine for passing air/fuel streams to the cylinders of the engine,

a butterfly valve arranged in alignment with each barrel for controlling the flow of air/fuel streams through the barrels of the carburetor,

a control linkage connected to the butterfly valves, said control linkage configured to tilt the butterfly valves about axes transverse to the common plane of the barrels, with two of the butterfly valves being tiltable in clockwise directions from their closed positions toward their open positions and the other two butterfly valves being tiltable in counterclockwise directions from their closed positions to their open positions,

an intake manifold arranged to receive the air/fuel streams from the four open ended barrels, and

induction runners in communication with the intake manifold for extending to the cylinders of the engine and delivering the air/fuel streams to the cylinders of the engine.

9. The induction system for an internal combustion engine of claim 8 , wherein

the barrels of the carburetor are positioned in sequence of first, second, third and fourth barrels, with the barrels arranged in a row, and

the intake manifold has a first end and a second end, the first end of the induction manifold in communication with the first and second barrels and the second end of the intake manifold in communication with the third and fourth barrels, and a first group of the induction runners in communication with the first end of the intake manifold and with the cylinders at a first end of the engine, and a second group of the induction runners in communication with the second end of the intake manifold and with the cylinders at the second end of the engine.

10. The induction system for an internal combustion engine of claim 8 , wherein the first and second barrels of the carburetor intersect each other and the third and fourth barrels of the carburetor intersect each other.

11. The induction system for an internal combustion engine of claim 10 wherein the second and third barrels are spaced from each other.

12. The induction system for an internal combustion engine of claim 8 , wherein the first and second barrels of the carburetor are positioned to be mounted adjacent the cylinders at one end of the engine, and the third and fourth barrels of the carburetor are positioned to be mounted adjacent the cylinders at the other end of the engine.

13. The induction system for an internal combustion engine of claim 8 , wherein the control linkage is configured to tilt the butterfly valves about axes transverse to the common plane of the barrels, such that the butterfly valves of each pair of butterfly valves rotate in opposite directions so that their upper surfaces tilt toward a facing relationship and direct major portions of the air/fuel streams between the butterfly valves and toward a concentrated area beyond the butterfly valves into the intake manifold.

14. An induction system for an internal combustion engine having combustion cylinders, the cylinders of the engine being arranged in two banks of cylinders in a V-shaped configuration with one another, with a first half of the cylinders at one end of the engine and a second half of the cylinders at the other end of the engine, said induction system comprising:

an intake manifold for mounting to the engine,

a carburetor mounted to the intake manifold,

said carburetor including;

four open ended barrels extending through the carburetor, all of the barrels being aligned along a common plane for extending between the two banks of the engine for passing air/fuel streams to the cylinders of the engine,

a butterfly valve arranged in alignment with each barrel for controlling the flow of air/fuel streams through the barrels of the carburetor,

a control linkage connected to the butterfly valves, said control linkage configured to tilt the butterfly valves about axes transverse to the common plane of the barrels, with two of the butterfly valves being tiltable in clockwise directions from their closed positions toward their open positions and the other two butterfly valves being tiltable in counterclockwise directions from their closed positions to their open positions,

an intake manifold arranged to receive the air/fuel streams from the four open-ended barrels, and

induction runners in communication with the intake manifold for extending to the cylinders of the engine and delivering the air/fuel streams to the cylinders of the engine.

15. The induction system for an internal combustion engine of claim 13 , wherein the first and second barrels of the carburetor are positioned to be mounted adjacent the cylinders at one end of the engine, and the third and fourth barrels of the carburetor are positioned to be mounted adjacent the cylinders at the other end of the engine.

16. The induction system for an internal combustion engine of claim 14 , wherein the runners are connected to opposite ends of the manifold for connection to the cylinders at opposite ends of the engine.

17. An induction system for an internal combustion engine having combustion cylinders, with a first half of the cylinders at one end of the engine and a second half of the cylinders at the other end of the engine, said induction system comprising:

an intake manifold for mounting to the engine,

a carburetor mounted to the intake manifold,

said carburetor including;

at least two pairs of open ended barrels extending through the carburetor, all of the barrels being aligned along a common plane for passing air/fuel streams to the cylinders of the engine,

each pair of barrels including a primary barrel and a secondary barrel,

a butterfly valve arranged in alignment with each barrel for controlling the flow of air/fuel streams through the barrels of the carburetor,

a control linkage connected to the butterfly valves, said control linkage configured to tilt the butterfly valves about axes transverse to the common plane of the barrels, with the butterfly valves of the primary barrels being tiltable in a first direction from their closed positions toward their open positions to have their top surfaces face the secondary barrels, and the butterfly valves of the secondary barrels being tiltable in the opposite direction from their closed positions to their open positions to have their top surfaces face the primary barrels,

the intake manifold arranged to receive the air/fuel suspension from each of the pairs of open-ended barrels at spaced positions along the length of the manifold,

induction runners in communication with the intake manifold adjacent the spaced positions along the length of the manifold for extending from the spaced positions in the manifold to the cylinders most closely adjacent to the spaced positions in the manifold at each end of the engine and delivering the air/fuel streams to the cylinders of the engine,

such that the induction runners are of substantially equal lengths.

Assignments (24)
RECEIVING PARTY DATA CHANGE OF ADDRESS Recorded Jan 2, 2025
From: HOLLEY PERFORMANCE PRODUCTS, INC.
To: HOLLEY PERFORMANCE PRODUCTS, INC.
Reel/Frame 069813/0457 →
RELEASE OF SECURITY INTEREST Recorded Nov 24, 2021
From: AEA DEBT MANAGEMENT LP, AS SECOND LIEN COLLATERAL AGENT
To: FLOWMASTER, INC.; APR, LLC; ACCEL PERFORMANCE GROUP LLC; MSD LLC; POWERTEQ LLC; RACEPAK LLC; HOLLEY PERFORMANCE PRODUCTS INC.; HOLLEY PERFORMANCE SYSTEMS, INC.; HIGH PERFORMANCE INDUSTRIES, INC.
Reel/Frame 058944/0279 →
RELEASE OF SECURITY INTEREST Recorded Nov 24, 2021
From: UBS AG, STAMFORD BRANCH, AS FIRST LIEN COLLATERAL AGENT
To: FLOWMASTER, INC.; APR, LLC; ACCEL PERFORMANCE GROUP LLC; MSD LLC; POWERTEQ LLC; RACEPAK LLC; HOLLEY PERFORMANCE PRODUCTS INC.; HOLLEY PERFORMANCE SYSTEMS, INC.
Reel/Frame 058948/0926 →
SECURITY INTEREST Recorded Nov 19, 2021
From: HOLLEY PERFORMANCE PRODUCTS INC.; MSD LLC; POWERTEQ LLC; ACCEL PERFORMANCE GROUP LLC; DRAKE AUTOMOTIVE GROUP, LLC; B&M RACING & PERFORMANCE PRODUCTS INC.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 058214/0174 →
CORRECTIVE ASSIGNMENT TO CORRECT THE DELETE PATENT NUMBERS PREVIOUSLY RECORDED AT REEL: 047429 FRAME: 0343. ASSIGNOR(S) HEREBY CONFIRMS THE SECURITY INTEREST. Recorded Nov 18, 2018
From: FLOWMASTER, INC.; APR, LLC; ACCEL PERFORMANCE GROUP LLC; MSD LLC; POWERTEQ LLC; RACEPAK LLC; HOLLEY PERFORMANCE PRODUCTS INC.; HOLLEY PERFORMANCE SYSTEMS, INC.
To: UBS AG, STAMFORD BRANCH, AS COLLATERAL AGENT
Reel/Frame 048475/0125 →
SECURITY INTEREST Recorded Nov 18, 2018
From: FLOWMASTER, INC.; APR, LLC; ACCEL PERFORMANCE GROUP LLC; MSD LLC; POWERTEQ LLC; RACEPAK LLC; HOLLEY PERFORMANCE PRODUCTS INC.; HOLLEY PERFORMANCE SYSTEMS, INC.; HIGH PERFORMANCE INDUSTRIES, INC.
To: AEA DEBT MANAGEMENT LP, SECOND LIEN COLLATERAL AGENT
Reel/Frame 048147/0510 →
SECURITY INTEREST Recorded Nov 6, 2018
From: FLOWMASTER, INC.; APR, LLC; ACCEL PERFORMANCE GROUP LLC; MSD LLC; POWERTEQ LLC; RACEPAK LLC; HOLLEY PERFORMANCE PRODUCTS INC.; HOLLEY PERFORMANCE SYSTEMS, INC.
To: UBS AG, STAMFORD BRANCH, AS COLLATERAL AGENT
Reel/Frame 047429/0343 →
RELEASE OF SECURITY INTEREST Recorded Nov 5, 2018
From: CERBERUS BUSINESS FINANCE, LLC
To: HOLLEY PERFORMANCE PRODUCTS INC.; QFT HOLDINGS, INC.; HOLLEY PERFORMANCE SYSTEMS, INC.; MSD LLC; ACCEL PERFORMANCE GROUP LLC; POWERTEQ LLC
Reel/Frame 047419/0953 →
RELEASE OF SECURITY INTEREST IN PATENT COLLATERAL Recorded Sep 24, 2015
From: GENERAL ELECTRIC CAPITAL CORPORATION
To: HOLLEY PERFORMANCE PRODUCTS INC.; DEMON FUEL SYSTEMS, INC.; QFT HOLDINGS, INC.; HOLLEY PERFORMANCE SYSTEMS, INC.
Reel/Frame 036686/0964 →
PATENT SECURITY AGREEMENT Recorded Sep 22, 2015
From: HOLLEY PERFORMANCE PRODUCTS INC.; QFT HOLDINGS, INC.; HOLLEY PERFORMANCE SYSTEMS, INC.; MSD LLC; ACCEL PERFORMANCE GROUP LLC; POWERTEQ LLC
To: CERBERUS BUSINESS FINANCE, LLC, AS COLLATERAL AGENT
Reel/Frame 036664/0148 →
MERGER Recorded May 6, 2014
From: DEMON FUEL SYSTEMS, INC.
To: HOLLEY PERFORMANCE PRODUCTS INC.
Reel/Frame 032826/0413 →
RELEASE OF SECURITY INTEREST Recorded Oct 30, 2013
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS AGENT
To: DEMON FUEL SYSTEMS, INC.
Reel/Frame 031508/0928 →
RELEASE OF SECURITY INTEREST Recorded Oct 30, 2013
From: HAWTHORN FINCO, LLC
To: DEMON FUEL SYSTEMS, INC.
Reel/Frame 031512/0872 →
RELEASE OF SECURITY INTEREST Recorded Oct 30, 2013
From: LBC CREDIT PARTNERS II, L.P.
To: DEMON FUEL SYSTEMS, INC.
Reel/Frame 031513/0841 →
SECURITY AGREEMENT Recorded Oct 25, 2013
From: HOLLEY PERFORMANCE PRODUCTS INC.; DEMON FUEL SYSTEMS, INC.; QFT HOLDINGS, INC.; HOLLEY PERFORMANCE SYSTEMS, INC.
To: GENERAL ELECTRIC CAPITAL CORPORATION, AS AGENT
Reel/Frame 031496/0062 →
SECURITY AGREEMENT Recorded Jun 29, 2012
From: DEMON FUEL SYSTEMS, INC.
To: HAWTHORN FINCO, LLC
Reel/Frame 028487/0941 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN INTELLECTUAL PROPERTY RIGHTS RECORDED AT REEL 027490/FRAME 0852 Recorded Jun 16, 2012
From: WILMINGTON TRUST, NATIONAL ASSOCIATION, AS SUCCESSOR-BY-MERGER TO WILMINGTON TRUST FSB
To: HOLLEY PERFORMANCE PRODUCTS, INC.; DEMON FUEL SYSTEMS, INC.; SNIPER MOTORSPORTS, INC.
Reel/Frame 028388/0916 →
SECURITY AGREEMENT Recorded Jun 8, 2012
From: DEMON FUEL SYSTEMS, INC.
To: LBC CREDIT PARTNERS II, L.P., AS AGENT
Reel/Frame 028342/0295 →
SECURITY AGREEMENT Recorded Jan 6, 2012
From: DEMON FUEL SYSTEMS, INC.
To: WILMINGTON TRUST, NATIONAL ASSOCIATION
Reel/Frame 027490/0852 →
SECURITY AGREEMENT Recorded Jan 4, 2012
From: DEMON FUEL SYSTEMS, INC.
To: WELLS FARGO CAPITAL FINANCE, INC.
Reel/Frame 027480/0708 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 13, 2011
From: HIGH PERFORMANCE INDUSTRIES, INC.
To: DEMON FUEL SYSTEMS, INC.
Reel/Frame 027371/0471 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 8, 2011
From: GRANT, BARRY S.
To: HIGH PERFORMANCE INDUSTRIES, INC.
Reel/Frame 026565/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 21, 2011
From: BRANCH BANKING AND TRUST COMPANY
To: HIGH PERFORMANCE INDUSTRIES, INC.
Reel/Frame 026473/0487 →
SECURITY AGREEMENT Recorded Jan 28, 2009
From: GRANT, BARRY S.
To: BRANCH BANKING AND TRUST COMPANY
Reel/Frame 022162/0214 →