Compressor with ribbed cooling jacket

1. A method comprising:

forming a compressor housing with an inner jacket and an outer jacket;

assembling a compressor rotor radially inward of the inner jacket;

forming a structural rib on a portion of the inner jacket, wherein a non-ribbed portion of the inner jacket has a thickness defined as a thin walled structure, wherein the thin walled structure includes a thickness such that the thickness if extended across an axial length of the inner jacket wall would, in the absence of the one or more ribs, result in at least one of (1) warping of the inner jacket wall during operation of a compressor having the compressor housing, (2) yielding of the inner jacket wall during operation of a compressor having the compressor housing, (3) mechanical interference between the compressor rotor and the inner jacket wall during operation of a compressor having the compressor housing, and (4) rubbing between the compressor rotor and the inner jacket wall during operation of a compressor having the compressor housing; and

forming a coolant flow channel between the inner and outer jackets.

2. The method of claim 1 , wherein the rib and the inner jacket are separately formed and subsequently attached.

3. A compressor comprising:

a housing structure configured to support a compressor rotor, the compressor rotor structured to increase a pressure of a working fluid;

a cooling chamber formed within the housing structure about a portion of the compressor rotor, the cooling chamber configured to contain a cooling fluid;

an inner cooling jacket wall and outer cooling jacket wall defining inner and outer walls respectively of the cooling chamber; and

a plurality of ribs formed with the inner cooling jacket wall, the ribs defined by portions of the inner cooling jacket wall projecting radially outward toward the cooling chamber;

wherein portions of the inner jacket wall between the adjacent ribs have a thickness such that the thickness if extended across an axial length of the inner jacket wall would, in the absence of the plurality of ribs, result in at least one of (1) warping of the inner jacket wall during operation of the compressor rotor; (2) yielding of the inner jacket wall during operation of the compressor rotor; (3) mechanical interference between the compressor rotor and the inner jacket wall during operation of a compressor having the compressor housing; and (4) rubbing between the compressor rotor and the inner jacket wall during operation of a compressor having the compressor housing.

4. The compressor system of claim 3 , wherein the ribs of the inner cooling jacket wall define a wall thickness that is greater than a wall thickness of the inner jacket wall at other locations.

5. The compressor system of claim 3 , wherein a cooling fluid is disposed within the cooling chamber to receive and remove heat from the compressor.

6. The compressor system of claim 5 , wherein the cooling fluid includes one of a water based solution and an oil based solution.

7. The compressor system of claim 3 , wherein portions of the inner jacket wall having the ribs formed thereon is more than twice a thickness of the non-ribbed portions.

8. The compressor system of claim 3 , wherein portions of the inner jacket wall having the ribs formed thereon is less than twice a thickness of the non-ribbed portions.

9. The compressor system of claim 3 , wherein a width of at least one of the ribs is greater than a distance between an adjacent pair of ribs.

10. The compressor system of claim 3 , wherein a width of at least one of the ribs is less than a distance between an adjacent pair of ribs.

11. The compressor system of claim 3 , wherein the compressor rotor is in the form of a screw compressor.

12. The compressor system of claim 3 , wherein the ribs are oriented in one of a circumferential direction, a transverse direction or combinations thereof relative to an axis of rotation.

13. An apparatus comprising:

a housing including a fluid compression cavity;

a compressor rotor rotatably supported at least partially within the fluid compression cavity;

an inner wall encompassing the fluid compression cavity, wherein the inner wall includes a portion defined as a thin walled structure; and

an outer wall spaced radially outward of the inner wall;

a cooling chamber formed in a space between the inner and outer walls; and

one or more ribs formed on the inner wall projecting into the cooling chamber;

wherein the thin walled structure includes a thickness such that the thickness if extended across an axial length of the inner jacket wall would, in the absence of the one or more ribs, result in at least one of (1) warping of the inner jacket wall during operation of the compressor rotor; (2) yielding of the inner jacket wall during operation of the compressor rotor; (3) mechanical interference between the compressor rotor and the inner jacket wall during operation of the compressor rotor; and (4) rubbing between the compressor rotor and the inner jacket wall during operation of the compressor rotor.

14. The apparatus of claim 13 , wherein each of the one or more ribs is integrally formed with the inner wall.

15. The apparatus of claim 13 , wherein each of the one or more ribs is separately formed and attached to the inner wall.

16. The apparatus of claim 13 , wherein a width of at least one of the one or more ribs is greater than a distance defined between a pair of adjacent ribs.

17. The apparatus of claim 13 , wherein a height of at least one rib extending in a radial direction from a surface of the inner wall is greater than a wall thickness of the inner wall between an adjacent pair of ribs.

18. The apparatus of claim 13 , wherein a height of at least one rib extending in a radial direction from a surface of the inner wall is less than a wall thickness of the inner wall between an adjacent pair of ribs.

19. The apparatus of claim 13 , wherein the compressor rotor includes a screw profile section operable for compressing a fluid.