Granted Patent B2

US 9,726,185 · App. 13/893,675 · Granted Aug 8, 2017

Abstract

Claims (21)

1. A centrifugal compressor for a turbocharger for compressing air to be delivered to an engine air intake, comprising:

a compressor wheel having a hub defining a rotational axis and having a plurality of circumferentially spaced blades each joined to the hub and extending generally radially outwardly to a blade tip, each of the blades having a leading edge and a trailing edge spaced downstream from the leading edge along a flow direction of a main flow of air through the wheel;

a compressor housing in which the compressor wheel is mounted so as to be rotatable about the rotational axis of the compressor wheel, the compressor housing including an inlet duct through which a main flow of air enters in a flow direction generally parallel to the rotational axis of the compressor wheel and is led by the inlet duct into the compressor wheel;

a wheel shroud located radially adjacent the blade tips, the wheel shroud extending upstream from the blades with respect to the main flow proceeding along the flow direction and terminating at a leading edge of the wheel shroud spaced axially upstream of the blade leading edges, the wheel shroud having a radially inner surface wetted by the main flow and having a radially outer surface spaced radially inward of an inner surface of the inlet duct such that an annular space is defined between the radially outer surface of the wheel shroud and the inner surface of the inlet duct;

the wheel shroud defining a port proximate the blade tips and extending generally radially outwardly from the radially inner surface to the radially outer surface of the wheel shroud, into the annular space;

a plurality of circumferentially spaced slots formed in the wheel shroud, each slot extending through the leading edge of the wheel shroud such that the slot is open at the leading edge of the wheel shroud, and extending axially downstream to a position axially spaced from the port in the wheel shroud, and each slot over an entire length thereof extending from the radially inner surface to the radially outer surface of the wheel shroud, such that a portion of air passing through the compressor wheel can flow out through the port into the annular space, then upstream within the annular space, and finally inwardly through the slots so as to be injected, as recirculated air, back into the main flow; and

an annular flow-guiding member that extends from the inlet duct radially inwardly and axially downstream to a trailing edge of the flow-guiding member, said trailing edge being proximate the leading edge of the wheel shroud, the flow-guiding member serving to substantially prevent the main flow of air from passing through the slots while allowing the recirculated air to pass through the slots, wherein the trailing edge of the flow-guiding member is axially spaced from the leading edge of the wheel shroud, such that there is a 360-degree gap between the trailing edge of the flow-guiding member and the leading edge of the wheel shroud.

2. The centrifugal compressor of claim 1 , wherein the slots are angled with respect to a radial direction such that the recirculated air is injected back into the main flow with a swirl component of velocity.

3. The centrifugal compressor of claim 1 , wherein there are at least eight said slots distributed over 360° about the wheel shroud.

4. The centrifugal compressor of claim 3 , wherein the wheel shroud defines a shroud portion extending circumferentially between each slot and a neighboring slot, and wherein each shroud portion, at the radially outer surface of the wheel shroud, has a greater circumferential extent than does each of the slots.

5. A turbocharger, comprising:

a turbine comprising a turbine wheel mounted in a turbine housing and affixed to one end of a shaft that is rotatable about an axis thereof;

a centrifugal compressor for compressing air to be delivered to an engine air intake, comprising a compressor wheel affixed to an opposite end of the shaft and mounted in a compressor housing, the compressor wheel having a hub defining a rotational axis and having a plurality of circumferentially spaced blades each joined to the hub and extending generally radially outwardly to a blade tip, each of the blades having a leading edge and a trailing edge spaced downstream from the leading edge along a flow direction of a main flow of air through the wheel;

the compressor housing including an inlet duct through which a main flow of air enters in a flow direction generally parallel to the rotational axis of the compressor wheel and is led by the inlet duct into the compressor wheel;

a wheel shroud located radially adjacent the blade tips, the wheel shroud extending upstream from the blades with respect to the main flow proceeding along the flow direction and terminating at a leading edge of the wheel shroud spaced axially upstream of the blade leading edges, the wheel shroud having a radially inner surface wetted by the main flow and having a radially outer surface spaced radially inward of an inner surface of the inlet duct such that an annular space is defined between the radially outer surface of the wheel shroud and the inner surface of the inlet duct;

the wheel shroud defining a port proximate the blade tips and extending generally radially outwardly from the radially inner surface to the radially outer surface of the wheel shroud, into the annular space;

a plurality of circumferentially spaced slots formed in the wheel shroud, each slot extending through the leading edge of the wheel shroud such that the slot is open at the leading edge of the wheel shroud, and extending axially downstream to a position axially spaced from the port in the wheel shroud, and each slot over an entire length thereof extending from the radially inner surface to the radially outer surface of the wheel shroud, such that a portion of air passing through the compressor wheel can flow out through the port into the annular space, then upstream within the annular space, and finally inwardly through the slots so as to be injected, as recirculated air, back into the main flow; and

an annular flow-guiding member that extends from the inlet duct radially inwardly and axially downstream to a trailing edge of the flow-guiding member, said trailing edge being proximate the leading edge of the wheel shroud, the flow-guiding member serving to substantially prevent the main flow of air from passing through the slots while allowing the recirculated air to pass through the slots, wherein the trailing edge of the flow-guiding member is axially spaced upstream from the leading edge of the wheel shroud, such that there is a 360-degree gap between the trailing edge of the flow-guiding member and the leading edge of the wheel shroud.

6. The turbocharger compressor of claim 5 , wherein the slots are angled with respect to a radial direction such that the recirculated air is injected back into the main flow with a swirl component of velocity.

7. The turbocharger of claim 5 , wherein there are at least eight said slots distributed over 360° about the wheel shroud.

8. The turbocharger of claim 7 , wherein the wheel shroud defines a shroud portion extending circumferentially between each slot and a neighboring slot, and wherein each shroud portion, at the radially outer surface of the wheel shroud, has a greater circumferential extent than does each of the slots.

Assignments (7)