IP Library Granted Patent US 9,261,094
Granted Patent B2
US 9,261,094 · App. 14/303,800 · Granted Feb 16, 2016

Rotary compressor

Inventor: Jason James Hugenroth (Baton Rouge, LA)
Assignee: Caire Inc.
F04C29/02F01C21/104F04C18/322F04C18/3564F04C18/38F04C23/001F04C2230/91
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,261,094
App. No.
14/303,800
Granted
Feb 16, 2016
Kind
B2
Abstract

An aspect of the present disclosure involves a rotary compressor that is primarily optimized for use without the need for liquid lubricants, such as in the flow path of the fluid being compressed, and is efficient and quiet to use. The compressors described herein are efficient, run quietly, use less power, and last longer than those previously known in the art. The compressors are useful for medical applications and other clean gas applications, for instance, where lubricants could contaminate the fluid being compressed and/or increased noise and/or vibration may be problematic.

Claims (39)

1. A system comprising:

a first inlet configured to receive fluid that is to be compressed;

a first piston configured to rotate around a first eccentric of a shaft in an orbital fashion in order to compress the fluid, the first piston being coated with an abradable coating, the fluid being used as a lubricant for lubricating the first piston, the use of the fluid for lubricating and the abradable coating eliminating a need of another lubricant for lubricating the first piston;

a first outlet configured to discharge the compressed fluid;

a second inlet configured to receive, from a separator device, one or more exhaust gases that have been separated from the fluid, the one or more exhaust gases being a subset of gases forming the fluid;

a second piston configured to rotate around a second eccentric of the shaft in the orbital fashion, axial surfaces of the second piston being parallel to axial surfaces of the first piston, the second piston being coated with the abradable coating, the one or more exhaust gases being used as a lubricant for lubricating the second piston, the use of the one or more exhaust gases for lubricating and the abradable coating of the second piston eliminating a need of another lubricant for lubricating the second piston; and

a second outlet configured to exhaust the gases.

2. The system of claim 1 , further comprising:

a first vane connected to the first piston;

a first set of bushings slidingly connected to the first vane; and

a first stator configured to enclose the first piston and the first vane.

3. The system of claim 2 , wherein each bushing of the first set of bushings has a flat surface in contact with a surface of the first vane.

4. The system of claim 2 , wherein the first stator encloses a chamber that includes at least a vane chamber and a bore chamber, the bore chamber comprising a compression chamber and a suction chamber that is sealed from the compression chamber by the first vane and the first set of bushings.

5. The system of claim 4 , wherein the compression chamber and the suction chamber are interchanged during the rotation of the first piston such that the compression chamber performs suction and the suction chamber performs compression.

6. The system of claim 4 , wherein the first vane comprises a cutout vane relief, the vane relief allowing pressure of air within the vane chamber to equalize with pressure in the suction chamber in order to minimize wear of the first set of bushings, the minimized wear of the first set of bushings eliminating a need of another lubricant for lubricating the first set of bushings.

7. The system of claim 2 , further comprising:

a second vane connected to the second piston;

a second set of bushings slidingly connected to the second vane; and

a second stator configured to enclose the second piston and the second vane, the first stator and the second stator being a single machined unit.

8. The system of claim 2 , wherein an outer surface of the first piston comprises dimples that cause a rise of pressure of the fluid within the dimples, the rise of the pressure pushing the first piston away from an inner surface of the first stator so as to minimize contact between the first piston and the first stator, the minimized contact eliminating the need of the another lubricant for providing lubrication between the first piston and the first stator.

9. The system of claim 2 , wherein the first vane comprises a recess that is in fluid communication with a recess within the first piston, a pressure of fluid in the recess within the first piston preventing the recess from contacting the first stator, the prevention of contact between the first piston and the first stator eliminating the need of another lubricant for providing lubrication between the first piston and the first stator.

10. The system of claim 2 , wherein the first piston comprises recesses intersecting an outside diameter of the first piston, the recesses intersecting the outside diameter of the first piston being pressurized such that pressure of the pressurized recesses prevents a contact between the first piston and the first stator, the prevention of contact between the first piston and the first stator eliminating the need of another lubricant for providing lubrication between the first piston and the first stator.

11. The system of claim 1 , further comprising:

a suction endplate that incorporates the first inlet; and

a discharge endplate that incorporates the first outlet.

12. The system of claim 11 , wherein at least one of the first stator, the suction endplate and the discharge endplate are coated with the abradable coating.

13. The system of claim 12 , wherein the abradable coating minimizes friction between the first piston and the first stator, the minimized friction between the first piston and the first stator eliminating the need of another lubricant for lubricating the first piston.

14. The system of claim 1 , wherein the abradable coating comprises a polymer based coating.

15. The system of claim 1 , wherein the fluid that is to be compressed is ambient air, the ambient air being received at the first inlet from an ambient air collecting source.

16. The system of claim 15 , wherein the compressed fluid is pressurized ambient air, the pressurized air going from the first outlet to a separator device.

17. The system of claim 16 , wherein the separator device is a vacuum-pressure-swing-adsorption (VPSA) device.

18. The system of claim 16 , wherein the separator device is a vacuum-swing-adsorption (VSA) device.

19. A method comprising:

receiving ambient air at a first inlet of a rotary compressor powered by a motor;

rotating a first piston of the rotary compressor around a first eccentric of a shaft in an orbital motion to compress the ambient air into compressed gas;

sending, at a first outlet of the rotary compressor, the compressed gas to a separator device configured to separate the compressed gas into a first gas and other gases, the rotary compressor being lubricated by the ambient air and the compressed gas while not requiring another lubricant;

receiving, at a second inlet of a vacuum pump powered by the motor, the other gases from the separator device, the vacuum pump comprising a second piston configured to rotate around a second eccentric of the shaft in the orbital motion, the second piston being radially parallel to the first piston; and

exhausting the other gases at a second outlet of the vacuum pump, the vacuum pump being lubricated by the other gases while not requiring another lubricant.

20. The method of claim 19 , wherein the first gas is oxygen.

Assignments (2)
RELEASE OF SECURITY INTEREST Recorded Dec 20, 2018
From: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
To: CAIRE INC.
Reel/Frame 047968/0666 →
SECURITY INTEREST Recorded Jan 22, 2015
From: CAIRE INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 034793/0277 →
Continuity (3)
Continuation 12879998 · Sep 10, 2010
Provisional Application 61241331 · Sep 10, 2009
Related Publication 20140294639A1 · Oct 2, 2014