Active swirl device for turbocharger compressor

Patent metadata

Field	Value
Publication number	US-9932991-B2
Application number	US-201615090188-A
Country	US
Kind code	B2
Filing date	Apr 4, 2016
Priority date	Apr 4, 2016
Publication date	Apr 3, 2018
Grant date	Apr 3, 2018

Abstract

Methods and systems are provided for mitigating noise generated by a compressor operating at low flow rates. A swirl device with two concentric flow passages upstream of the compressor directs intake air flow to the compressor through two different flow paths, depending on air flow rates. Angled swirl vanes at an outlet of the swirl device pre-whirl the air flowing to the compressor to reduce noise generation at low air flow rates.

First claim

The invention claimed is:

1. A turbocharger system, comprising:
a flow channel upstream of a compressor, forming an inner flow passage and an outer flow passage, an outlet portion of the inner flow passage fluidically connecting the inner flow passage to the compressor;
a plurality of swirl vanes defining a downstream outlet of the outer flow passage, the downstream outlet fluidically connecting the outer flow passage to the compressor; and
a recessable plate positioned within the inner flow passage;
wherein the recessable plate is coupled to a flat planar wall of the inner flow passage via a hinge and operable between a first position and a second position.

2. The system of claim 1 , wherein the downstream outlet of the outer flow passage is downstream of the recessable plate.

3. The system of claim 1 , wherein the outer flow passage is at least partially concentric to the inner flow passage with the downstream outlet of the outer flow passage extending beyond the inner flow passage.

4. The system of claim 1 , wherein the outer flow passage fluidically connects to the compressor through a plurality of gaps each between adjacent swirl vanes of the plurality of swirl vanes at a downstream portion of the outer flow passage.

5. The system of claim 1 , wherein, in the first position, the recessable plate lays flush with the planar wall within a recess of the planar wall without protruding into the inner flow passage, the inner flow passage further having an upstream and downstream transition between the flat planar wall and circular walls.

6. The system of claim 5 , wherein the recessable plate in the second position is perpendicular to a longitudinal axis of the recess in the planar wall of the inner flow passage, blocking intake air flow through the inner flow passage to the compressor.

7. The system of claim 1 , wherein the recessable plate attached with the hinge to the inner flow passage is adjustable to a desired angular position relative to the recess.

8. The system of claim 1 , further comprising at least one sensor and a controller including instructions stored in a non-transitory computer-readable medium for controlling an actuator of the recessable plate to adjust a recessable plate position between the first position and the second position responsive to operating conditions of the system.

9. The system of claim 8 , wherein the controller includes instructions stored in the non-transitory computer-readable medium to determine an intake air flow rate via the at least one sensor, compare the intake air flow rate to a threshold, and control the actuator of the recessable plate to position the recessable plate to fluidically connect the inner flow passage to the compressor responsive to the operating condition including an intake air flow rate being above the threshold.

10. The system of claim 9 , wherein the controller includes instructions stored in the non-transitory computer-readable medium to control the actuator of the recessable plate to position the recessable plate to block fluidic coupling of the inner flow passage to the compressor responsive to the operating condition including the intake air flow rate being below the threshold.

11. The system of claim 9 ,
wherein the controller includes instructions stored in the non-transitory computer-readable medium to determine a ratio of compressor pressure and intake air flow rate via the at least one sensor, compare the ratio to a threshold ratio, and
responsive to the ratio being above the threshold ratio, control the actuator of the recessable plate to position the recessable plate to block fluidic coupling of the inner flow passage; and
responsive to the ratio being below the threshold ratio, control the actuator of the recessable plate to position the recessable plate to fluidically connect the inner flow passage to the compressor.

12. The system of claim 1 , wherein the outer flow passage is partitioned into a plurality of outer ducts, an inlet of each outer duct fluidically connected to an inlet of the flow channel, and an outlet of each outer duct fluidically connected to the compressor through at least one of the plurality of swirl vanes.

13. The system of claim 1 , wherein the flow channel comprises an inner cylindrical passage that forms the inner flow passage and that is housed within an outer cylindrical passage, and the outer flow passage comprises an annular passage around the inner cylindrical passage.

14. A method, comprising:
determining an operating condition of an engine;
responsive to a first operating condition of the engine, actuating an actuator coupled to a hinged collapsible valve to position the hinged collapsible valve in a first position where the hinged collapsible valve lies flush with a planar wall inside a recess of the planar wall of a central passage, and flowing intake air through the central passage to a compressor inlet; and
responsive to a second operating condition of the engine, actuating the actuator coupled to the hinged collapsible valve to position the hinged collapsible valve in a second position where the hinged collapsible valve spans across a width of the central passage, blocking intake air flow through the central passage to the compressor inlet, and directing intake air flow through a concentric outer flow passage fluidically coupled to the central passage, the intake air exiting the outer flow passage through a plurality of angled swirl vanes and flowing to the compressor inlet.

15. The method of claim 14 , further comprising determining an intake air flow rate via/by at least one sensor and comparing the intake air flow rate to a threshold,
wherein the first operating condition of the engine comprises the intake air flow rate above the threshold; and
wherein the second operating condition of the engine comprises the intake air flow rate below the threshold.

16. The method of claim 14 , further comprising:
determining an intake air flow rate and a compressor pressure via the at least one sensor;
comparing a ratio of the compressor pressure and the intake air flow rate to a threshold ratio,
wherein responsive to a third operating condition of the engine comprises the ratio being below the threshold ratio; and
wherein a fourth operating condition of the engine comprises the ratio being above the threshold ratio;

responsive to the third operating condition of the engine, actuating the actuator coupled to the hinged collapsible valve to position the hinged collapsible valve in the first position, and flowing intake air through the central passage to the compressor inlet; and
responsive to the fourth operating condition of the engine, actuating the actuator coupled to the hinged collapsible valve to position the hinged collapsible valve in the second position, and flowing intake air through the concentric outer flow passage to the compressor inlet.

17. A system, comprising:
an engine;
a turbocharger with a compressor coupled to the engine, the compressor including a housing;
a flow duct upstream of an impeller of the compressor, forming an inner flow passage and an outer flow passage surrounding the inner flow passage;
a plurality of angled swirl vanes defining a most downstream portion of the outer flow passage, upstream of the impeller of the compressor;
a recessable plate attached by a hinge to the inner flow passage,
wherein the recessable plate is coupled to a flat planar wall of the inner flow passage; and

a controller including a non-transitory computer-readable medium storing instructions for regulating a position of the recessable plate.

Assignees

• Ford Global Tech Llc

Inventors

• Wade Robert Andrew
• Knott Tim J

Classifications

• F04D29/444

  Bladed diffusers · CPC title

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title

• F04D29/667 Primary

  by influencing the flow pattern, e.g. suppression of turbulence · CPC title

• F05B2220/40

  in turbochargers · CPC title

• F05B2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title