Centrifugal compressor with recirculation passage

Patent metadata

Field	Value
Publication number	US-11808277-B2
Application number	US-202217960401-A
Country	US
Kind code	B2
Filing date	Oct 5, 2022
Priority date	Feb 9, 2018
Publication date	Nov 7, 2023
Grant date	Nov 7, 2023

Abstract

An example centrifugal compressor includes a housing that defines an inlet chamber and includes first and second openings that define a recirculation passage in fluid communication with the inlet chamber. An impeller is disposed within the housing and is rotatable about a longitudinal axis to draw fluid into the inlet chamber. The first and second openings are at different axial locations along the longitudinal axis. A plurality of inlet guide vanes are rotatable and situated in the inlet chamber. The centrifugal compressor includes a ring and a controller for moving the ring along the longitudinal axis between a first position and a second position when rotating the inlet guide vanes. The ring obstructs at least one of the first and second openings more in the second position than in the first position.

First claim

What is claimed is:

1. A centrifugal compressor, comprising:
a housing defining an inlet chamber and including at least one first opening and at least one second opening, the at least one first opening and at least one second opening defining a recirculation passage in fluid communication with the inlet chamber;
an impeller within the housing and rotatable about a longitudinal axis to draw fluid into the inlet chamber;
a first ring including at least one ring opening;
a plurality of radial inlet guide vanes that are situated in the inlet chamber and are rotatable about respective axes from an open position to a closed position, wherein the plurality of radial inlet guide vanes restrict a flow of the fluid from the inlet chamber to the outlet passage more in the closed position than in the open position;
a second ring; and
a controller configured to:
rotate the first ring about the longitudinal axis between a first position and a second position to control a flow of fluid through the recirculation passage, wherein the first ring obstructs at least one of the first and second openings more in the second position than in the first position; and
rotate the plurality of radial inlet guide vanes about their respective axes based on rotation of the second ring about the longitudinal axis.

2. The centrifugal compressor of claim 1 , wherein:
the at least one ring opening includes a plurality of ring openings that are circumferentially spaced apart from each other about the longitudinal axis;
the at least one second opening includes a plurality of second openings that are circumferentially spaced apart from each other about the longitudinal axis; and
the plurality of ring openings and the plurality of second openings are more aligned, and the plurality of second openings are thereby less obstructed, in the first position than in the second position.

3. The centrifugal compressor of claim 1 , wherein the at least one ring opening extends through the first ring.

4. The centrifugal compressor of claim 1 , comprising:
a pressure sensor, wherein the controller is configured to rotate the first ring based on measurements from the pressure sensor.

5. The centrifugal compressor of claim 1 , wherein the centrifugal compressor is part of a refrigeration circuit, and the fluid drawn into the inlet chamber by the impeller is refrigerant.

6. A method of operating a centrifugal compressor comprising:
rotating an impeller about a longitudinal axis within a compressor housing to draw fluid into an inlet chamber, the compressor housing having at least one first opening and at least one second opening, the at least one first opening and the at least one second opening defining a recirculation passage in fluid communication with the inlet chamber;
recirculating fluid from the inlet chamber through the recirculation passage and back into the inlet chamber; and
rotating a first ring about the longitudinal axis between a first position and a second position to control a flow of fluid through the recirculation passage, wherein the first ring obstructs at least one of the first and second openings more in the second position than in the first position;
wherein:
the centrifugal compressor comprises a plurality of radial inlet guide vanes that are situated in the inlet chamber and are rotatable about respective axes from an open position to a closed position, wherein the plurality of radial inlet guide vanes restrict a flow of the fluid from the inlet chamber to an outlet passage more in the closed position than in the open position; and
the method comprises rotating the plurality of radial inlet guide vanes about their respective axes based on rotation of a second ring about the longitudinal axis.

7. The method of claim 6 , wherein:
the at least one ring opening includes a plurality of ring openings that are circumferentially spaced apart from each other about the longitudinal axis;
the at least one second opening includes a plurality of second openings that are circumferentially spaced apart from each other about the longitudinal axis; and
the plurality of ring openings and the plurality of second openings are more aligned, and the plurality of second openings are thereby less obstructed, in the first position than in the second position.

8. The method of claim 6 , wherein the at least one ring opening extends through the first ring.

9. The method of claim 6 , comprising:
measuring a pressure of the fluid; and
performing said rotating of the first ring based on fluid measurements from said measuring.

10. The method of claim 6 , wherein the centrifugal compressor is part of a refrigeration circuit, and the fluid drawn into the inlet chamber by the impeller is refrigerant.

Assignees

• Carrier Corp

Inventors

• Sishtla Vishnu M
• Cousins William T

Classifications

• F04D27/0207 Primary

  by bleeding, bypassing or recycling fluids (influencing the boundary layer by an uncontrolled bleeding of the working fluid F04D29/681) · CPC title

• F01D17/162

  for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F04D17/14

  with means for changing the flow-path through the stages, e.g. series-parallel, e.g. side-loads, (surge control F04D27/02) · CPC title

• F04D27/001

  Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring · CPC title

• F04D27/009

  by bleeding, by passing or recycling fluid · CPC title