Economizer injection assembly and method

Patent metadata

Field	Value
Publication number	US-9816733-B2
Application number	US-201314655356-A
Country	US
Kind code	B2
Filing date	Dec 31, 2013
Priority date	Dec 31, 2012
Publication date	Nov 14, 2017
Grant date	Nov 14, 2017

Abstract

Embodiments provided herein are directed to systems and methods of re-injecting vaporized flash refrigerant from an economizer into a two-stage compressor. The injection can be through an injection port positioned after the first compression stage. The location of the injection may have a relatively low static refrigerant pressure. The injection port and/or an injection pipe of the economizer may be configured to pre-condition the vaporized flash refrigerant so that a flow velocity and/or direction of the vaporized flash refrigerant flow can be match a flow velocity and/or direction of the refrigerant in the refrigerant conduit.

First claim

What claimed is:

1. A chiller, comprising:
a condenser;
an evaporator;
a compressor including a first compression stage and a second compression stage;
a refrigerant conduit, the refrigerant conduit configured to be in fluid communication with the first compression stage and the second compression stage; and
an economizer,
wherein the economizer is configured to form a fluid communication with the refrigerant conduit between the first and the second compressor stages,
the fluid communication is formed through an injection port,
the injection port has an internal surface feature configured to inject refrigerant from the economizer into a refrigerant flow direction in the refrigerant conduit,
the internal surface feature has a smooth curve configured to direct refrigerant to flow in a direction similar to the refrigerant flow direction in the refrigerant conduit, and
the fluid communication is formed closer to the first compression stage than the second compression stage.

2. The chiller of claim 1 , wherein the fluid communication is formed at a location along the refrigerant conduit with a relatively low static refrigerant pressure.

3. The chiller of claim 1 , wherein the refrigerant conduit is defined by a discharge exit of the first compression stage,
a run-around pipe and an inlet of the second compression stage, and
the fluid communication is formed at the discharge exit of the first compression stage.

4. The chiller of claim 1 , wherein the refrigerant conduit has a section with an increasing diameter from the first compression stage to the second compression stage, and
the fluid communication is formed before the diameter starts to increase along the refrigerant conduit.

5. The chiller of claim 1 , wherein the fluid communication is formed at a lower quarter of a cross section of the refrigerant conduit when viewing from a cross-section of the refrigerant conduit.

6. The chiller of claim 1 , further comprising:
an injection pipe fluidly communicating with the refrigerant conduit and the economizer,
wherein the injection pipe has a diameter that is configured to direct refrigerant from the economizer so that the refrigerant flows in a flow velocity that matches a refrigerant flow velocity in the refrigerant conduit.

7. The chiller of claim 1 , further comprising:
a swirl control device,
wherein the swirl control device is positioned inside the refrigerant conduit before the inlet of the second compression stage, and
the swirl control device is configured to reduce refrigerant swirling in the refrigerant conduit.

8. A chiller, comprising:
a condenser;
an evaporator;
a compressor including a first compression stage and a second compression stage;
a refrigerant conduit, the refrigerant conduit configured to be in fluid communication with the first compression stage and the second compression stage; and
an injection port in fluid communication with the refrigerant conduit between the first and the second compressor stages,
wherein the injection port is configured to direct refrigerant into the refrigerant conduit,
the injection port has an internal surface feature configured to direct refrigerant into a refrigerant flow direction in the refrigerant conduit,
the internal surface feature has a smooth curve configured to direct refrigerant to flow in a direction similar to the refrigerant flow direction in the refrigerant conduit, and
the injection port is positioned closer to the first compression stage than the second compression stage.

9. The chiller of claim 8 , wherein the refrigerant conduit has a section with an increasing diameter from the first compression stage to the second compression stage, and
the injection port is located before the diameter starts to increase along the refrigerant conduit.

10. The chiller of claim 8 , wherein the injection port connects to a lower quarter of a cross section of the refrigerant conduit when viewing from a cross-section of the refrigerant conduit.

11. A compressor with a first compression stage and a second compression stage for a heating, ventilation, and air-conditioning (HVAC) system, comprising: a refrigerant conduit fluidly connecting the first compression stage and the second compression stage; and an injection port in fluid communication with the refrigerant conduit, wherein the fluid communication is formed closer to the first compression stage than the second compression stage, the injection port has an internal surface feature configured to direct refrigerant into a refrigerant flow direction in the refrigerant conduit, the internal surface feature has a smooth curve configured to direct refrigerant to flow in a direction similar to the refrigerant flow direction in the refrigerant conduit.

12. The compressor of claim 11 , wherein the refrigerant conduit has a section of an increasing diameter from the first compression stage to the second compression stage along the refrigerant conduit, and
the injection port is positioned before the section of the increasing diameter.

13. The compressor of claim 11 , further comprising:
a swirl control device,
wherein the swirl control device is positioned inside the refrigerant conduit between the first and the second compression stages.

14. A method of injecting refrigerant vapor between a first compression stage and a second compression stage of a compressor in a heating, ventilation, and air-conditioning (HVAC) system, comprising: directing the refrigerant vapor from an injection port toward a refrigerant conduit fluidly connecting the first compression stage and the second compression staged the injection port has an internal surface feature configured to direct refrigerant into a refrigerant flow direction in the refrigerant conduit, and the internal surface feature has a smooth curve configured to direct refrigerant to flow in a direction similar to the refrigerant flow direction in the refrigerant conduit; directing the refrigerant vapor, by use of the smooth curve of the internal surface feature, so that a flow direction of the refrigerant vapor matches a refrigerant flow direction in the refrigerant conduit; directing the refrigerant vapor into the refrigerant conduit; and mixing the refrigerant vapor with the refrigerant compressed by the first compression stage.

15. The method of claim 14 , further comprising:
directing the refrigerant vapor so that a flow velocity of the refrigerant vapor matches a refrigerant flow velocity in the refrigerant conduit at the injection port.

16. The method of claim 14 , further comprising:
reducing refrigerant swirling in the refrigerant conduit before the second compression stage.

Assignees

• Trane Int Inc

Inventors

• Haley Paul Francis
• James Rick Todd

Classifications

• F04D29/441

  especially adapted for elastic fluid pumps · CPC title

• F04D29/5846

  cooling by injection · CPC title

• F25B1/10 Primary

  with multi-stage compression (with cascade operation F25B7/00) · CPC title

• F25B7/00 Primary

  Compression machines, plants or systems, with cascade operation, i.e. with two or more circuits, the heat from the condenser of one circuit being absorbed by the evaporator of the next circuit (F25B9/00 takes precedence) · CPC title

• F25B1/04

  with compressor of rotary type ({F25B1/005,} F25B1/10 take precedence) · CPC title