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A method and apparatus is disclosed for the production, delivery and control of microscopic quantities of minute solid carbon dioxide (CO2) particles having uniform density and distribution for use in a CO2 Composite Spray process, which employs compression of liquid carbon dioxide to form a supersa

A method and apparatus is disclosed for the production, delivery and control of microscopic quantities of minute solid carbon dioxide (CO2) particles having uniform density and distribution for use in a CO2 Composite Spray process, which employs compression of liquid carbon dioxide to form a supersaturated liquid, which is then condensed via micro-capillaries into minute and highly energetic solid carbon dioxide particles, which are injected into a propellant gas stream.

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1. A spray apparatus for producing a stream of propellant gas and carbon dioxide comprising: the carbon dioxide in a first state, which is a saturated liquid;compressing the carbon dioxide in the first state to form a second state, which is super-saturated at a density greater than 0.9 g/ml;said com

1. A spray apparatus for producing a stream of propellant gas and carbon dioxide comprising: the carbon dioxide in a first state, which is a saturated liquid;compressing the carbon dioxide in the first state to form a second state, which is super-saturated at a density greater than 0.9 g/ml;said compression is adjusted using a high pressure pump;a condensation of the carbon dioxide in the second state within a micro-capillary tube to form a third state, which is a microscopic solid;said propellant gas and said carbon dioxide in the third state are mixed to form the stream of the propellant gas and the carbon dioxide;said carbon dioxide mixing rate is adjusted using a high pressure pump;whereby the stream is used to treat a substrate surface. 2. The apparatus of claim 1 wherein micro-capillary is at least one high-pressure capillary tube for receiving supersaturated carbon dioxide. 3. The apparatus of claim 2 wherein the micro-capillary has a length of from 6 inches to 20 feet, an outer diameter of from 0.020 inch to 0.125 inch, and an inner diameter of from 25 micron to about 0.010 inch. 4. The apparatus of claim 2 wherein the micro-capillary comprises one or more capillaries in a parallel flow arrangement having a length of from 6 inches to 20 feet, an outer diameter of from 0.020 inch to 0.125 inch, and an inner diameter of from 25 micron to 0.010 inch. 5. The apparatus of claim 2 wherein the micro-capillary comprises polyetheretherketone and stainless steel high pressure capillary tubes. 6. The apparatus of claim 1 wherein the carbon dioxide in a first state is compressed to super-saturation using a high pressure pump. 7. The apparatus of claim 6 wherein the high pressure pump compresses the carbon dioxide in the first state into the micro-capillary to form the carbon dioxide in the second state, which is supersaturated. 8. The apparatus of claim 7 wherein the supersaturated carbon dioxide is compressed within the micro-capillary to a pressure between 900 psi and 10,000 psi. 9. The apparatus of claim 8 wherein the supersaturated carbon dioxide is compressed to a pressure between 1,000 psi and 5,000 psi. 10. The apparatus of claim 7 wherein the supersaturated carbon dioxide is thermally controlled at a temperature between 5 degrees C. and 40 degrees C. 11. The apparatus of claim 10 wherein the supersaturated carbon dioxide is thermally controlled at a temperature between 15 degrees C. and 25 degrees C. 12. The apparatus of claim 1 wherein the propellant gas is clean dry air, nitrogen, argon or carbon dioxide. 13. The apparatus of claim 12 wherein the propellant gas is thermally controlled at a temperature between 5 degrees C. and 250 degrees C. 14. The apparatus of claim 1 wherein the propellant gas and the carbon dioxide in the third state are mixed coaxially. 15. The apparatus of claim 1 wherein the propellant gas and the carbon dioxide in the third state are mixed using an adjustable expansion tube for receiving the carbon dioxide in the third state produced by the pressurized micro-capillary. 16. The apparatus of claim 1 wherein the saturated carbon dioxide is at a pressure of between 500 psi and 900 psi. 17. The apparatus of claim 1 wherein the saturated carbon dioxide is at a temperature of between 5 degrees C. and 40 degrees C. 18. The apparatus of claim 1 wherein the supersaturated carbon dioxide is a liquid or a supercritical fluid. 19. A spray apparatus for producing a stream of propellant gas and carbon dioxide comprising: the carbon dioxide in a first state, which is liquid and saturated;a compression of the carbon dioxide in the first state to form a second state, which is super-saturated and at a higher pressure than the first state;a condensation of the carbon dioxide in the second state within a micro-capillary tube to form a third state, which is solid; andsaid propellant gas is mixed with said carbon dioxide in the third state to form the stream of propellant gas and carbon dioxide,whereby said stream is used to treat a substrate surface. 20. A method for producing a spray of propellant gas and carbon dioxide comprising: d. Compressing the carbon dioxide in a first state which is saturated, to form a second state, which is super-saturated at a density greater than 0.9 g/ml;e. Condensing the carbon dioxide in the second state within a micro-capillary tube to form a third state, which is a microscopic solid; andf. Mixing said propellant gas and said carbon dioxide in the third state to form the spray,Whereby said spray is used to treat a substrate surface. 21. The method of claim 20 wherein the propellant gas temperature is between 5 degrees C. to 200 degrees C. 22. The method of claim 20 wherein the propellant gas pressure is between 30 psi and 250 psi. 23. The method of claim 22 wherein the propellant gas is clean dry air, nitrogen, argon, or carbon dioxide. 24. The method of claim 20 wherein a high pressure pump is used to compress the saturated carbon dioxide within the micro-capillary at a pressure between 1,000 psi and 10,000 psi to form the supersaturated carbon dioxide. 25. The method of claim 20 wherein the supersaturated carbon dioxide temperature is adjusted between 5 degrees C. and 40 degrees C. 26. The method of claim 20 wherein the propellant gas and the carbon dioxide in the third state are mixed and projected at the substrate surface using an adjustable expansion tube and mixing nozzle. 27. The method of claim 20 wherein the spray generates a shear stress on the substrate surface at between 10 kPa and 100 MPa. 28. The method of claim 20 wherein the spray produces a temperature on the substrate surface at between −40 degrees C. and 200 degrees C. 29. The method of claim 20 wherein the supersaturated carbon dioxide is injected into the micro-capillary using a high pressure pump to produce carbon dioxide in the third state. 30. The method of claim 29 wherein an injection flow rate of the carbon dioxide in the third state is between 0.1 lbs per hour and 20 lbs per hour.