Method and apparatus for control of fluid temperature and flow

1. An apparatus for cooling comprising:

a micro channel comprising a wall portion, an inflow opening, and an outflow opening; and

a gas comprising a constituent particle;

wherein the micro channel is configured to accommodate a flow of the gas from the inflow opening to the outflow opening in a first direction substantially perpendicular to a cross section of the micro channel;

wherein the inflow opening has a first cross section area and the outflow opening has a second cross section area substantially different from the first cross section area;

wherein the first cross section area has a value in a first range of about 0.01 μm 2 to 500 μm 2 ;

wherein the second cross section area has a value in a second range of about 0.1 μm 2 to 50,000 μm 2 ; and

wherein the wall portion and the constituent particle are configured such that a velocity component of the constituent particle parallel to the wall portion before a collision between the constituent particle and the wall portion has approximately the same value after the collision and further configured such that energy transfer between the wall portion and the constituent particle occurs through a change in a velocity component of the constituent particle perpendicular to the wall portion.

2. The apparatus of claim 1 wherein at least a portion of the cross section of the micro channel varies as a function of a length in the first direction between the inflow opening and the outflow opening.

3. The apparatus of claim 2 wherein the variation in the cross section of the micro channel as a function of a length in the first direction between the inflow opening and the outflow opening is substantially linear and substantially increasing.

4. The apparatus of claim 2 wherein the variation in the cross section of the micro channel as a function of a length in the first direction between the inflow opening and the outflow opening is substantially abrupt in a region proximal to the inflow opening, is substantially constant between the region proximal to the inflow opening and the outflow opening, and wherein the cross section of the micro channel between the region proximal to the inflow opening and the outflow opening is greater than the cross section of the micro channel in the region proximal to the inflow opening.

5. The apparatus of claim 2 wherein the variation in the cross section of the micro channel as a function of a length in the first direction between the inflow opening and the outflow opening is substantially linear and substantially increasing in a first region and substantially linear and substantially decreasing in a second region, wherein the first region is proximal to the inflow opening and the second region is proximal to the outflow opening.

6. The apparatus of claim 2 wherein the variation in the cross section of the micro channel as a function of a length in the first direction between the inflow opening and the outflow opening is substantially abrupt in a region proximal to the inflow opening, is substantially abrupt in a region proximal to the outflow opening, and is substantially constant between the region proximal to the inflow opening and the region proximal to the outflow opening, and wherein the cross section of the micro channel between the region proximal to the inflow opening and the region proximal to the outflow opening is greater than the cross section of the micro channel in the region proximal to the inflow opening.

7. A method for cooling, comprising:

providing a micro channel comprising a surface, an inflow opening, and an outflow opening, wherein the surface comprises a wall portion, and wherein the inflow opening has a first cross section area and the outflow opening has a second cross section area substantially different from the first cross section area;

providing a gas comprising a constituent particle;

inducing a flow of the gas from the inflow opening to the outflow opening in a first direction substantially perpendicular to a cross section of the micro channel;

wherein the first cross section area has a value in a first range of about 0.01 μm 2 to 500 μm 2 ;

wherein the second cross section area has a value in a second range of about 0.1 μm 2 to 50,000 μm 2 ; and

wherein at least one of the wall portion and the constituent particle is configured such that a velocity component of the constituent particle parallel to the wall portion before a collision between the constituent particle and the wall portion has approximately the same value after the collision and further configured such that energy transfer between the wall portion and the constituent particle occurs through a change in a velocity component of the constituent particle perpendicular to the wall portion.

8. The method of claim 7 wherein at least a portion of the cross section of the micro channel varies as a function of a length in the first direction between the inflow opening and the outflow opening.

9. The method of claim 8 wherein the variation in the cross section of the micro channel as a function of a length in the first direction between the inflow opening and the outflow opening is substantially linear and substantially increasing.

10. The method of claim 8 wherein the variation in the cross section of the micro channel as a function of a length in the first direction between the inflow opening and the outflow opening is substantially abrupt in a region proximal to the outflow opening, is substantially constant between the region proximal to the outflow opening and the inflow opening, and wherein the cross section of the micro channel between the inflow opening and the outflow opening is greater than the cross section of the micro channel in the region proximal to the outflow opening.

11. The method of claim 8 wherein the variation in the cross section of the micro channel as a function of a length in the first direction between the inflow opening and the outflow opening is substantially linear and substantially increasing in a first region and substantially linear and substantially decreasing in a second region, wherein the first region is proximal to the inflow opening and the second region is proximal to the outflow opening.

12. The method of claim 8 wherein the variation in the cross section of the micro channel as a function of a length in the first direction between the inflow opening and the outflow opening is substantially abrupt in a region proximal to the inflow opening, is substantially abrupt in a region proximal to the outflow opening, and is substantially constant between the region proximal to the inflow opening and the region proximal to the outflow opening, and wherein the cross section of the micro channel between the region proximal to the inflow opening and the region proximal to the outflow opening is greater than the cross section of the micro channel in the region proximal to the inflow opening.

13. A system for cooling comprising:

a micro channel comprising a wall portion, an inflow opening, and an outflow opening; and

a gas comprising a constituent particle, the gas being induced to flow through the micro channel through operation of a pressure differential between a first pressure and a second pressure, the first pressure of the gas proximal to the inflow opening being atmospheric and the second pressure of the gas proximal to the outflow opening being substantially less than atmospheric;

wherein the micro channel is configured to accommodate a flow of the gas from the inflow opening to the outflow opening in a first direction substantially perpendicular to a cross section of the micro channel;

wherein the inflow opening has an inflow cross section value in a first range of about 0.01 μm 2 to 500 μm 2 ;

wherein the outflow opening has an outflow cross section value in a second range of about 0.1 μm 2 to 50,000 μm 2 ;

wherein a linear distance between the inflow opening and the outflow opening along a length of the micro channel has a value in a range of about 0.01 mm to 10 m; and

wherein the wall portion and the constituent particle are configured such that a velocity component of the constituent particle parallel to the wall portion before a collision between the constituent particle and the wall portion has approximately the same value after the collision and further configured such that energy transfer between the wall portion and the constituent particle occurs through a change in a velocity component of the constituent particle perpendicular to the wall portion.

14. The system of claim 13 wherein the gas comprises air.

15. A method for cooling, comprising:

providing a micro channel comprising a surface, an inflow opening, and an outflow opening, wherein the surface comprises a wall portion;

providing a gas comprising a constituent particle;

inducing a flow of the gas from the inflow opening to the outflow opening in a first direction substantially perpendicular to a cross section of the micro channel through operation of a pressure differential between a first pressure and a second pressure, the first pressure of the gas proximal to the inflow opening being atmospheric and the second pressure of the gas proximal to the outflow opening being substantially less than atmospheric;

wherein the inflow opening has an inflow cross section value in a first range of about 0.01 μm 2 to 500 μm 2 ;

wherein the outflow opening has an outflow cross section value in a second range of about 0.1 μm 2 to 50,000 μm 2 ;

wherein a linear distance between the inflow opening and the outflow opening along a length of the micro channel has a value in a range of about 0.01 mm to 10 m; and

wherein at least one of the wall portion and the constituent particle is configured such that a velocity component of the constituent particle parallel to the wall portion before a collision between the constituent particle and the wall portion has approximately the same value after the collision and further configured such that energy transfer between the wall portion and the constituent particle occurs through a change in a velocity component of the constituent particle perpendicular to the wall portion.

16. The method of claim 15 wherein the gas comprises air.