Swirl control system for varying in-cylinder swirl

Claim 2

A swirl control system for varying the swirl of intake air in an internal combustion engine having at least one combustion chamber, comprising: a low swirl helically-shaped primary intake air passage for delivering a primary flow of intake air having a low swift energy level to the combustion chamber, said low swirl primary intake air passage capable of imparting an initial angular momentum to said primary air flow in said primary intake air passage corresponding to said low swirl energy level for producing a low level swirling effect in the combustion chamber; a secondary intake air passage connected to said primary intake air passage for directing a secondary flow of intake air at a predetermined flow rate into said primary air flow so as to constructively interact with said primary air flow to form a combined air flow having a combined angular momentum greater than said initial angular momentum, said secondary air flow entering said primary intake air passage substantially tangential to said primary air flow; a secondary air flow control means for controlling the flow of said secondary air flow into said low swift primary intake air passage to vary said combined angular momentum so as to vary the swirl of intake air in the combustion chamber while substantially avoiding destructive interference between said secondary air flow and said primary flow thereby minimizing air pressure losses through said low swirl helically-shaped primary intake air passage.

Claim 3

The swirl control system of claim 1, wherein said secondary air flow control means is operable to increase the flow of said secondary air flow for increasing said combined angular momentum to increase the swirl of intake air in the combustion chamber.

Claim 4

The swift control system of claim 2, wherein said primary intake air passage includes an outer annular wall and an inner annular wall formed radially inward from said outer annular wall, said secondary intake air passage including a tubular portion connected to said outer annular wall of said primary intake air passage.

Claim 5

The swirl control system of claim 3, wherein said tubular portion extends from said outer annular wall at an acute angle to a horizontal plane extending across the combustion chamber.

Claim 6

The swirl control system of claim 3, wherein said tubular portion is formed integrally with said outer annular wall.

Claim 7

The swift control system of claim 4, wherein said tubular portion is pivotally connected to said outer annular wall, said tubular portion pivotable so as to vary said acute angle.

Claim 8

A swift control system for varying the swift of intake air in an internal combustion engine having at least one combustion chamber, comprising: a helically-shaped low swift primary intake air passage for delivering a primary flow of intake air to the combustion chamber, said helically-shaped primary air passage imparting an initial low swift energy level to said primary air flow resulting in a low level swirling effect in the combustion chamber; a secondary intake air passage connected to said primary intake air passage for directing a secondary flow of intake air at a predetermined flow rate into said primary air flow so as to constructively interact with said primary air flow to form a combined air flow having a combined swirl energy level greater than said low swirl energy level, said secondary air flow entering said helically-shaped primary air passage substantially tangential to said primary air flow; a secondary air flow control means for controlling the flow rate of said secondary air flow into said helically-shaped low swirl primary air intake passage to vary said combined swirl energy level while substantially avoiding destructive interference between said secondary air flow and said primary air flow thereby minimizing air pressure losses through said helically-shaped low swirl primary intake air passage.

Claim 9

A swift control system for varying the swift of intake air in an internal combustion engine having at least one combustion chamber, comprising: a helically-shaped low swift primary intake air passage for delivering a primary flow of intake air to the combustion chamber, said helically-shaped primary air passage imparting an initial low swift energy level to said primary air flow resulting in a low level swirling effect in the combustion chamber; a secondary intake air passage connected to said primary intake air passage for directing a secondary flow of intake air at a predetermined flow rate into said primary air flow so as to constructively interact with said primary air flow to form a combined air flow having a combined swirl energy level greater than said low swirl energy level, said secondary air flow entering said helically-shaped primary air passage substantially tangential to said primary air flow; a secondary air flow control means for controlling the flow rate of said secondary air flow into said helically-shaped low swirl primary air intake passage to vary said combined swirl energy level while substantially avoiding destructive interference between said secondary air flow and said primary air flow thereby minimizing air pressure losses through said helically-shaped low swirl primary intake air passage.

Claim 10

The swirl control system of claim 7, wherein said secondary air flow control means is operable to increase said flow rate of said secondary air flow so as to increase said combined swirl energy level.

Claim 11

The swirl control system of claim 8, wherein said low swirl primary intake air passage includes an outer annular wall and an inner annular wall formed radially inward from said outer annular wall, said secondary intake air passage including a tubular portion connected to said outer wall of said low swirl primary intake air passage.

Claim 12

The swirl control system of claim 9, wherein said tubular portion extends from said outer annular wall at an acute angle to a horizontal plane extending across the combustion chamber.

Claim 13

The swirl control system of claim 9, wherein said tubular portion is formed integrally with said outer annular wall.

Claim 14

The swirl control system of claim 10, wherein said tubular portion is pivotally connected to said outer annular wall, said tubular portion pivotable so as to vary said acute angle.

Claim 15

A swirl control system for varying the swirl of intake air in an internal combustion engine having at least one combustion chamber, comprising: a low swirl helically-shaped primary intake air passage for delivering a primary flow of intake air having a low swirl energy level to the combustion chamber, said low swirl primary intake air passage capable of imparting an initial angular momentum to said primary air flow in said primary intake air passage corresponding to said low swirl energy level for producing a low level swirling effect in the combustion chamber; a secondary intake air passage connected to said primary intake air passage for directing a secondary flow of intake air at a predetermined flow rate into said primary air flow to form a combined air flow having a combined angular momentum greater than said initial angular momentum, said secondary air flow entering said primary intake air passage substantially tangential to said primary air flow; a secondary air flow control means for controlling the flow of said secondary air flow into said low swift primary intake air passage to vary said combined angular momentum so as to vary the swift of intake air in the combustion chamber while minimizing air pressure losses through said low swirl helically-shaped primary intake air passage; said secondary air flow control means being operable to increase the flow of said secondary air flow for increasing said combined angular momentum to increase the swift of intake air in the combustion chamber; wherein said primary intake air passage includes an outer annular wall and an inner annular wall formed radially inward from said outer annular wall, said secondary intake air passage including a tubular portion connected to said outer annular wall of said primary intake air passage.

Claim 16

A swirl control system for varying the swirl of intake air in an internal combustion engine having at least one combustion chamber, comprising: a low swirl helically-shaped primary intake air passage for delivering a primary flow of intake air having a low swirl energy level to the combustion chamber, said low swirl primary intake air passage capable of imparting an initial angular momentum to said primary air flow in said primary intake air passage corresponding to said low swirl energy level for producing a low level swirling effect in the combustion chamber; a secondary intake air passage connected to said primary intake air passage for directing a secondary flow of intake air at a predetermined flow rate into said primary air flow to form a combined air flow having a combined angular momentum greater than said initial angular momentum, said secondary air flow entering said primary intake air passage substantially tangential to said primary air flow; a secondary air flow control means for controlling the flow of said secondary air flow into said low swift primary intake air passage to vary said combined angular momentum so as to vary the swift of intake air in the combustion chamber while minimizing air pressure losses through said low swirl helically-shaped primary intake air passage; said secondary air flow control means being operable to increase the flow of said secondary air flow for increasing said combined angular momentum to increase the swift of intake air in the combustion chamber; wherein said primary intake air passage includes an outer annular wall and an inner annular wall formed radially inward from said outer annular wall, said secondary intake air passage including a tubular portion connected to said outer annular wall of said primary intake air passage.