Systems and methods for a bi-valved variable inlet device

Patent metadata

Field	Value
Publication number	US-10190487-B1
Application number	US-201715804397-A
Country	US
Kind code	B1
Filing date	Nov 6, 2017
Priority date	Nov 6, 2017
Publication date	Jan 29, 2019
Grant date	Jan 29, 2019

Abstract

Methods and systems are provided for a variable inlet device of a compressor. In one example, a compressor may include the variable inlet device arranged within an inlet conduit of the compressor. The variable inlet device may be adjustable to control the gas flow through the compressor, the variable inlet including a pair of semi-cylindrical shells that are pivotable, about a set of hinges, between an open and closed position.

First claim

The invention claimed is:

1. A system for an engine, comprising:
a compressor including an impeller rotatable about a central axis and a variable inlet device (VID) arranged upstream of the impeller in an inlet conduit of the compressor, the VID comprising:
a set of semi-cylindrical shells arranged adjacent to one another, each shell of the set of shells having an inlet end arranged upstream in the inlet conduit from an outlet end, where each shell is pivotable, from its inlet end to its outlet end, relative to the central axis; and
an actuator adapted to actuate the VID into an open and closed position, the actuator including an electric motor coupled to two pivotable arms, each arm of the two pivotable arms coupled to an outer surface a respective shell of the two shells; and
a controller including computer readable instructions stored on memory for:
actuating the electric motor to pivot the pivotable arms toward the central axis and move each outlet end of each shell inward, toward the central axis, to move the VID into the closed position in response to a first operating condition; and
actuating the electric motor to pivot the pivotable arms away from the central axis and move each outlet end of each shell outward, away from the central axis, to move the VID into the open position in response to a second operating condition.

2. The system of claim 1 , wherein the first operating condition includes operation of the engine below a surge threshold of the compressor and the second operating condition includes operation of the engine above the surge threshold.

3. A compressor, comprising:
an impeller rotatable about a central axis; and
a variable inlet device (VID) positioned in an inlet conduit upstream of the impeller, and including two semi-cylindrical shells having inner surfaces forming an inner flow passage through the VID aligned with the central axis, each of the two shells being pivotable between open and closed positions about a set of hinges arranged at an inlet end of the VID.

4. The compressor of claim 3 , further comprising an actuator coupled to the two shells and adapted to actuate the VID into the open and closed positions, the actuator including an electric motor coupled to two pivotable arms, each arm of the two pivotable arms coupled to an outer surface of a respective shell of the two shells.

5. The compressor of claim 3 , wherein outer surfaces of the two shells are arranged adjacent to an inner wall of the inlet conduit.

6. The compressor of claim 3 , wherein the inlet end of the VID is formed by a first inlet end of a first shell of the two shells and a second inlet end of a second shell of the two shells, the VID further including an outlet end formed by a first outlet end of the first shell and a second outlet end of the second shell, wherein the inlet end of the VID is arranged upstream of the outlet end of the VID, and wherein the flow passage is formed within the inner surfaces of the two shells, between the inlet end and outlet end of the VID.

7. The compressor of claim 6 , wherein the first shell has a first central region that extends in a straight line from the first inlet end to the first outlet end, and a first side region arranged on an opposite side of the first central region from a second side region, the first and second side regions spaced apart from one another by the first central region, and wherein the second shell has a second central region that extends in a straight line from the second inlet end to the second outlet end, and a third side region arranged on an opposite side of the second central region from a fourth side region, the third and fourth side regions spaced apart from one another by the second central region.

8. The compressor of claim 7 , wherein the first side region of the first shell has a first side wall and the second side region of the first shell has a second side wall, and the first and second side walls each have a first straight portion extending from the first inlet end to a first mid-point of the first shell and each of the first and second side walls has a first angled portion extending from the first mid-point to the first outlet end, wherein the first angled portion of each of the first and second side walls connects a corresponding first straight portion to the first outlet end, wherein the third side region of the second shell has a third side wall and the fourth side region of the second shell has a fourth side wall, and the third and fourth side walls each have a second straight portion extending from the second inlet end to a second mid-point of the second shell and each of the third and fourth side walls has a second angled portion extending from the second mid-point to the second outlet end, wherein each second angled portion connects a corresponding second straight portion to the second outlet end.

9. The compressor of claim 8 , wherein each angled portion is longer than each straight portion.

10. The compressor of claim 6 , wherein the first central region and the first and second side regions of the first shell create continuous and curved outer and inner surfaces of the first shell, and the second central region and the third and fourth side regions of the second shell create continuous and curved outer and inner surfaces of the second shell.

11. The compressor of claim 10 , wherein in the open position, outer surfaces of the two shells are in face-sharing contact with an inner wall of the inlet conduit and each first straight portion of the first shell is in edge-sharing contact with a corresponding second straight portion of the second shell.

12. The compressor of claim 10 , wherein in the closed position, each outlet end of the two shells are pivoted inwards towards the central axis, away from an inner wall of the inlet conduit and each first angled portion of the first shell is in edge-sharing contact with a corresponding second angled portion of the second shell.

13. The compressor of claim 6 , wherein in the closed position the inlet end of the VID has a larger diameter than the outlet end of the VID.

14. The compressor of claim 3 , wherein a first hinge of the set of hinges is arranged at a mid-point of the first inlet end of the first shell and attaches the first inlet end to a base of the VID, and wherein a second hinge of the set of hinges is arranged at a mid-point of the second inlet end of the second shell and attaches the second inlet end to the base.

15. A method, comprising:
actuating pivotable arms of an actuator to adjust a variable inlet device (VID) coupled to the pivotable arms, the VID adjusted between an open position where an inner surface of the VID does not restrict flow from an inlet end to an outlet end of the VID and a closed position where the inner surface narrows along a length of the VID and restricts flow through the VID, the VID positioned in and across an inlet conduit of a compressor, upstream of an impeller, the actuating based on operation of an engine relative to a surge threshold of the compressor.

16. The method of claim 15 , wherein the VID includes a set of adjacently arranged semi-cylindrical shells forming a ring around a central axis of the compressor, where inner surfaces of the adjacently arranged shells form the inner surface of the VID and a flow passage through the VID.

17. The method of claim 16 , wherein the operation of the engine relative to the surge threshold of the compressor comprises the engine transitioning to operating at an engine speed and engine load that is below the surge threshold, and wherein actuating the pivotable arms to adjust

Assignees

• Ford Global Tech Llc

Inventors

• Zeng Tao
• Hu Leon

Classifications

• F02B37/225 Primary

  air passages · CPC title

• F02B39/16

  Other safety measures for, or other control of, pumps · CPC title

• F02D41/0007

  for control of turbo-charged or super-charged engines (control of the pumps per se F02B37/12) · CPC title

• F02D41/26

  using computer, e.g. microprocessor · CPC title

• F04D27/002

  by varying geometry within the pumps, e.g. by adjusting vanes · CPC title