TWO-STAGE HEAT EXCHANGER WITH INTERSTAGE BYPASS

• US 20100206543A1
• Filed: 02/13/2009
• Published: 08/19/2010
• Est. Priority Date: 02/13/2009
• Status: Abandoned Application

• Current Assignee: Sullair, LLC (Hitachi, Ltd.)
• Original Assignee: Sullair, LLC (Hitachi, Ltd.)
• Inventors: Countiss, Robert A., Tylisz, Brian M., McDavid, Andrew
• Application Number:
  US12/370,632
• Publication Number:
  US 20100206543A1
• Time in Patent Office: Days
• US Class Current: 165/297
• CPC Class Codes: F01M 5/002 Cooling
• CPC Class Codes: F01M 5/007 Thermostatic control

Abstract

A fluid cooler comprises a first stage fluid cooler and a downstream second stage fluid cooler. A flow line connects the first and second stages. A valve senses a condition of the fluid in the flow line, and to bypass the second stage fluid cooler if it is determined that additional cooling is not necessary. An air compressor incorporating the cooler is also claimed as is a method of operating a fluid cooler.

Claims

1. A fluid cooler comprising:

a first stage fluid cooler and a downstream second stage fluid cooler, and a flow line connecting said first and second stage fluid coolers; and

a valve for sensing a condition of the fluid in said flow line, and to bypass said second stage fluid cooler if it is determined that additional cooling is not necessary.

2. The fluid cooler as set forth in claim 1, wherein said valve senses the temperature of the fluid.

3. The fluid cooler as set forth in claim 2, wherein a bypass line is connected into said flow line, said bypass line communicating with said valve.

4. The fluid cooler as set forth in claim 1, wherein said valve includes a temperature sensitive sensor, which expands to move the valve to block the bypass when a predetermined temperature is met.

5. The fluid cooler as set forth in claim 1, wherein an oil is passed from a compressor through said fluid cooler.

6. The fluid cooler as set forth in claim 1, wherein there is a discharge manifold at a downstream end of said second stage fluid cooler, and the fluid is bypassed directly into the discharge manifold.

7. The fluid cooler as set forth in claim 6, wherein said second stage fluid cooler also has an inlet manifold, and flow channels are provided between said inlet manifold and said discharge manifold, and allow an included fluid to be cooled by air as it passes through said flow channels.

8. The fluid cooler as set forth in claim 1, wherein said valve is at an upstream end of a bypass line.

9. A compressor comprising:

a compressor having an oil inlet; and

an oil supply line leading to a fluid cooler from said compressor, and a fluid return line leading from said fluid cooler and back to said compressor, said fluid cooler comprising a first stage fluid cooler and a downstream second stage fluid cooler, and a flow line connecting said first and second stage fluid coolers, a valve for sensing a condition of the fluid in said flow line, and to bypass said second stage fluid cooler if it is determined that additional cooling is not necessary.

10. The compressor as set forth in claim 9, wherein said valve senses the temperature of the fluid.

11. The compressor as set forth in claim 10, wherein a bypass line is connected into said flow line, said bypass line communicating with said valve.

12. The compressor as set forth in claim 9, wherein there is a discharge manifold at a downstream end of said second stage fluid cooler, and the fluid is bypassed directly into the discharge manifold.

13. The compressor as set forth in claim 12, wherein said second stage fluid cooler also has an inlet manifold, and flow channels are provided between said inlet manifold and said discharge manifold, and allow an included fluid to be cooled by air as it passes through said flow channels.

14. The compressor as set forth in claim 9, wherein said valve includes a temperature sensitive sensor, which expands to move the valve to block the bypass when a predetermined temperature is met.

15. The compressor as set forth in claim 9, wherein said valve is at an upstream end of a bypass line.