Supercharger device for an internal combustion engine

Claim 2

A turbine for a turbocompressor of a supercharger device of an internal combustion engine, said turbine comprising a turbine wheel, a housing wall internally defining a first part of a scroll in which said turbine wheel is mounted to be rotatable about an axis, said housing wall further defining an aperture laterally disposed relative to said wheel and scroll, a flap movably mounted in said aperture and having a concave surface which defines a second part of said scroll completing said scroll with said first part, said scroll having an inlet for exhaust gases from said engine and a partition element dividing said inlet into two conduits which are respectively for connection to two exhaust pipes, each pipe being connected to exhaust outlets of a respective group of cylinders of the engine, said flap being movable in said aperture between a withdrawn position in which withdrawn position said concave surface of said flap defines a given section of passage of a part of the scroll adjacent to said inlet and a position in which said flap projects from said aperture and said concave surface of said flap defines a section of passage which is smaller than said given section of said part of the scroll adjacent to said inlet, said flap having two extension portions which are respectively cooperative with said two conduits so as to substantially completely open said conduits in said withdrawn position of said flap and to partly close said conduits in said projecting position of said flap.

Claim 3

A turbine according to claim 1, wherein the partition element is a web having a triangular cross-sectional shape and a point which points toward the scroll in the downstream direction relative to the direction of gas flow in the device.

Claim 4

A turbine according to claim 1, wherein the partition element has an extension portion which extends into said aperture and is located between said extension portions of said flap when said flap is in said withdrawn position.

Claim 5

A turbine according to claim 1, wherein the flap is mounted on said housing wall to pivot about an axis of a pivot pin and it has at least one cylindrical surface which has a part-circular section in a plane perpendicular to the axis of rotation of said turbine wheel and is centered on said axis of said pin and is cooperative with a conjugate cylindrical surface formed internally on said housing wall so as to substantially seal said scroll.

Claim 6

A turbine according to claim 4, comprising two cylindrical surfaces on the flap which are located respectively adjacent an upstream end and downstream end of the flap relative to the flow of the gases through the device, two surfaces conjugate with said two surfaces on the flap being provided on said housing wall to substantially seal said scroll.

Claim 7

A turbine according to claim 1, wherein said flap is pivotably mounted on said housing wall and is movable by pivoting about an axis parallel to the axis of rotation of said turbine wheel.

Claim 8

An internal combustion engine in combination with a supercharger device comprising a turbocompressor having a turbine comprising a turbine wheel, a housing wall internally defining a first part of a scroll in which said turbine wheel is mounted to be rotatable about an axis, said housing wall further defining an aperture laterally disposed relative to said wheel and scroll, a flap movably mounted in said aperture and having a concave surface which defines a second part of said scroll completing said scroll with said first part, said scroll having an inlet for exhaust gases from said engine and a partition element dividing said inlet into two conduits, said flap being movable in said aperture between a withdrawn position in which withdrawn position said concave surface of said flap defines a given section of passage of a part of the scroll adjacent to said inlet and a position in which said flap projects from said aperture and said concave surface of said flap defines a section of passage which is smaller than said given section of said part of the scroll adjacent to said inlet, said flap having two extension portions which are respectively cooperative with said two conduits so as to substantially completely open said conduits in said withdrawn position of said flap and to partly close said conduits in said projecting position of said flap, two exhaust pipes respectively connected to said two conduits, each exhaust pipe communicating with exhaust outlets of a respective group of cylinders of said engine.

Claim 9

An internal combustion engine in combination with a supercharger device comprising a turbocompressor having a turbine comprising a turbine wheel, a housing wall internally defining a first part of a scroll in which said turbine wheel is mounted to be rotatable about an axis, said housing wall further defining an aperture laterally disposed relative to said wheel and scroll, a flap movably mounted in said aperture and having a concave surface which defines a second part of said scroll completing said scroll with said first part, said scroll having an inlet for exhaust gases from said engine and a partition element dividing said inlet into two conduits, said flap being movable in said aperture between a withdrawn position in which withdrawn position said concave surface of said flap defines a given section of passage of a part of the scroll adjacent to said inlet and a position in which said flap projects from said aperture and said concave surface of said flap defines a section of passage which is smaller than said given section of said part of the scroll adjacent to said inlet, said flap having two extension portions which are respectively cooperative with said two conduits so as to substantially completely open said conduits in said withdrawn position of said flap and to partly close said conduits in said projecting position of said flap, two exhaust pipes respectively connected to said two conduits, each exhaust pipe communicating with exhaust outlets of a respective group of cylinders of said engine.