Direct drive refrigerant screw compressor with refrigerant lubricated rotors

Patent metadata

Field	Value
Publication number	US-12385491-B2
Application number	US-202318524682-A
Country	US
Kind code	B2
Filing date	Nov 30, 2023
Priority date	May 20, 2019
Publication date	Aug 12, 2025
Grant date	Aug 12, 2025

Abstract

Disclosed is a direct-drive refrigerant screw compressor, having: a housing; a compression chamber in the housing; a pair of rotors, each rotor of the pair of rotors being rotationally disposed in the compression chamber and including an outer surface with a screw-geared profile; a fluid being disposed in the compression chamber, the fluid consisting of a working fluid for providing lubrication to each rotor; a first port extending through the housing and configured for directing the fluid toward the compression chamber; and when the compressor is activated, each rotor rotates and the fluid is distributed about each rotor to lubricate each rotor.

First claim

What is claimed is:

1. A direct-drive refrigerant screw compressor, comprising:
a housing;
a compression chamber in the housing;
a pair of rotors, each rotor of the pair of rotors being rotationally disposed in the compression chamber and including an outer surface with a screw-geared profile;
a fluid being disposed in the compression chamber, the fluid consisting of a working fluid for providing lubrication to each rotor, wherein the working fluid is refrigerant delivered from a condenser conduit to the compressor for providing lubrication to compressor;
a first port extending through the housing and configured for directing the fluid toward the compression chamber;
wherein:
when the compressor is activated, each rotor rotates and the fluid is distributed about each rotor to lubricate each rotors
for each of the rotors, the compressor includes a plurality of bearing packs disposed within a respective plurality of bearing chambers, the plurality of bearing chambers being structural portions of the housing that are in or proximate the compression chamber, the respective plurality of bearing chambers being configured to securely position the respective bearing packs, the plurality of bearing chambers including a forward bearing chamber and an aft bearing chamber for each of the rotors, the forward and aft bearing chambers being fluidly connected with each other through the compression chamber of each of the rotors,
wherein:
the fluid is directed to the forward and aft bearing chambers for each of the rotors within the compressor that are fluidly coupled to the compression chamber; and
upon activation of the compressor, the fluid is injected to one side of the plurality of bearing chambers and flows through the plurality of bearing chambers to lubricate each of the plurality of bearing packs and is distributed about the rotors; and
the condenser conduit includes a forward branch and an aft branch for injecting in parallel the working fluid to the forward bearing chamber and the aft bearing chamber for each of the rotors of the compressor, each of the forward and aft branches of the condenser conduit includes a plurality of sub-branches for injecting in parallel the working fluid to the plurality of bearing chambers on each of the forward and aft branches of the condenser conduit.

2. The compressor of claim 1 , wherein:
the first port includes a flow control orifice.

3. The compressor of claim 1 , wherein:
the first port extends directly into the compression chamber.

4. The compressor of claim 1 , wherein:
the first port is fluidly connected to a passage in one rotor of the pair of rotors that directs the fluid to the compression chamber.

5. The compressor of claim 4 , wherein:
the passage extends between an axial aft port in the one rotor and the outer surface of the one rotor.

6. The compressor of claim 5 , wherein:
the passage includes an axial segment forming a blind hole and a radial segment fluidly connected between the axial segment and a surface port on the outer surface of the one rotor.

7. The compressor of claim 6 , wherein:
the passage includes a plurality of the radial segments fluidly connected to a respective plurality of the surface ports on the outer surface of the one rotor.

8. The compressor of claim 7 , wherein:
the plurality of the surface ports are staggered at regular intervals along the outer surface of the one rotor.

9. The compressor of claim 8 , wherein:
the plurality of the radial segments each include opposing radial portions extending to a respective plurality of the surface ports on the outer surface of the one rotor.

10. A refrigerant system including:
a condenser;
the compressor of claim 1 ; and
the condenser conduit fluidly connecting the condenser and the first port of the compressor, and configured to transport the fluid to the compressor to provide the working fluid to each rotor.

11. A method of directing fluid in a direct drive screw compressor, comprising:
receiving fluid at a first port of a housing of the compressor, wherein the fluid consists of a working fluid for providing lubrication to each rotor of a pair of rotors in the compressor; and
directing the fluid from the first port to a compression chamber in the compressor; and
when the compressor is activated, each rotor rotates and the fluid is distributed about each rotor to lubricate each rotor, wherein the working fluid is refrigerant delivered from a condenser conduit to the compressor for providing lubrication to compressor;
wherein:
for each of the rotors, the compressor includes a plurality of bearing packs disposed within a respective plurality of bearing chambers, the plurality of bearing chambers being structural portions of the housing that are in or proximate the compression chamber, the respective plurality of bearing chambers being configured to securely position the respective bearing packs, the plurality of bearing chambers including a forward bearing chamber and an aft bearing chamber for each of the rotors, the forward and aft bearing chambers being fluidly connected with each other through the compression chamber of each of the rotors;
the fluid is directed to the forward and aft bearing chambers for each of the rotors within the compressor that are fluidly coupled to the compression chamber; and
upon activation of the compressor, the fluid is injected to one side of the plurality of bearing chambers and flows through the plurality of bearing chambers to lubricate each of the plurality of bearing packs and is distributed about the rotors; and
the condenser conduit includes a forward branch and an aft branch for injecting in parallel the working fluid to the forward bearing chamber and the aft bearing chamber for each of the rotors of the compressor, each of the forward and aft branches of the condenser conduit includes a plurality of sub-branches for injecting in parallel the working fluid to the plurality of bearing chambers on each of the forward and aft branches of the condenser conduit.

12. The method of claim 11 , comprising:
controlling flow through the first port with a flow control orifice.

13. The method of claim 11 , wherein:
directing the fluid to the compression chamber includes:
injecting the fluid from the first port directly into the compression chamber.

14. The method of claim 11 , wherein:
directing the fluid to the compression chamber includes:
injecting the fluid from the first port, through a passage in one rotor of the pair of rotors, whereby the fluid is injected into the compression chamber.

15. The method of claim 14 , wherein:
injecting the fluid through the passage includes:
directing the fluid from the first port into an axial aft port in the passage and out an outer surface of the one rotor.

16. The method of claim 15 , wherein:
directing the fluid through the passage further includes:
directing the fluid through an axial segment forming a blind hole in the one rotor and a radial segment fluidly connected between the axial segment and a first surface port on the outer surface of the one rotor.

17. The method of claim 16 , wherein:
directing the fluid through the passage further includes:
directing the fluid though a plurality of the radial segments fluidly connected to a respective plurality of the surface ports on the outer surface of the one rotor.

18. The method of claim 17 , wherein:
the plurality of surface ports are staggered at regular intervals along the outer surface of the one rotor.

19. The method of claim 18 , whe

Assignees

• Carrier Corp

Inventors

• Qiu Yifan
• Vaidya Amit
• Jonsson Ulf J
• Chaudhry Zaffir A
• Rockwell David M

Classifications

• F25B1/047

  of screw type · CPC title

• F04C29/023

  Lubricant distribution through a hollow driving shaft (F04C29/025 takes precedence) · CPC title

• F04C2240/50

  Bearings · CPC title

• F04C2240/20

  Rotors · CPC title

• F04C2210/14

  Lubricant · CPC title