ATMOSPHERIC LAPSE RATE COOLING SYSTEM

• US 20120031119A1
• Filed: 08/03/2010
• Published: 02/09/2012
• Est. Priority Date: 08/03/2010
• Status: Abandoned Application

• Current Assignee: Nadeem Ahmad, Naeem Ahmad
• Original Assignee: Nadeem Ahmad, Naeem Ahmad
• Inventors: AHMAD, NADEEM, AHMAD, NAEEM
• Application Number:
  US12/849,650
• Publication Number:
  US 20120031119A1
• Time in Patent Office: Days
• US Class Current: 62/79
• CPC Class Codes: B64B 1/50 Captive balloons
• CPC Class Codes: F03G 7/04 using pressure differences or thermal differences occurring in nature F03G7/06 takes precedence
• CPC Class Codes: F28D 20/0034 using liquid heat storage material
• CPC Class Codes: F28D 2020/0026 the heat storage material being enclosed in mobile containers for transporting thermal energy
• CPC Class Codes: F28D 2020/0078 Heat exchanger arrangements
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction
• CPC Class Codes: Y02E 60/14 Thermal energy storage

Abstract

A heat transfer fluid can be cooled using the atmospheric thermal lapse rate. The heat transfer fluid can be ascended to a predetermined altitude above ground level where a temperature of the atmosphere is less than a temperature at the ground level. The heat transfer fluid can be cooled to a predetermined temperature by heat exchange between the heat transfer fluid and the atmosphere. The heat transfer fluid can then be descended to ground level while inhibiting heat transfer with the atmosphere tending to warm the cooled fluid.

Claims

1. A method for cooling a heat transfer fluid, comprising:

a) ascending a heat transfer fluid to predetermined altitude above a ground level where a temperature of the atmosphere is lower than a temperature at the ground level;

b) cooling the heat transfer fluid to a predetermined temperature that is lower than a temperature at the ground level by exchange of heat between the heat transfer fluid and the atmosphere; and

c) descending the cooled heat transfer fluid to the ground level while inhibiting heat transfer with the atmosphere tending to warm the cooled fluid.

2. The method of claim 1, wherein step a) comprises:

pumping the heat transfer fluid to a heat exchanger unit located on a tower.

3. The method of claim 2, wherein step c) comprises:

transferring the heat transfer fluid from the heat exchanger unit to a thermal storage container located on the ground level.

4. The method of claim 1, wherein step a) comprises:

ascending a heat exchanger unit with balloons filled with a gas lighter than air and pumping the heat transfer fluid to a heat exchanger unit.

5. The method of claim 4, wherein step c) comprises:

transferring the heat transfer fluid from the heat exchanger unit to a thermal storage container located on the ground level.

6. The method of claim 4, wherein ascending a heat exchanger unit with the balloons filled with a gas lighter than air and a kite attached at the top of the balloons.

7. The method of claim 1, wherein step a) comprises:

ascending a heat exchanger unit with aircrafts; and

pumping the heat transfer fluid to a heat exchanger unit.

8. The method of claim 7, wherein step c) comprises:

transferring the heat transfer fluid from the heat exchanger unit to a thermal storage container located on the ground level.

9. The method of claim 7, wherein ascending a heat exchanger unit with the aircrafts and a kite attached at the top of the balloons.

10. The method of claim 1 further comprising extracting energy as the heat transfer fluid ascends using a tether coupled to a generator and to a mechanism that ascends the heat transfer fluid.

11. The method of claim 1 is performed in a freighter aircraft with a built in heat exchanger unit and a thermal storage container.

12. A cooling system comprising:

means for ascending a heat transfer fluid to a to predetermined altitude above a ground level where a temperature of the atmosphere is less than a temperature at the ground level;

means for descending the heat transfer fluid back to the ground level while inhibiting heat transfer with the atmosphere tending to warm the cooled fluid;

a heat exchanger unit coupled to the means for ascending and descending the heat transfer fluid, wherein the heat exchanger configured to cool the heat transfer fluid by heat exchange with the atmosphere; and

a thermal storage container configured to receive the cooled heat transfer fluid.

13. The system of claim 12, wherein the thermal storage container is located on the ground level.

14. The system of claim 13, wherein the means for ascending and descending the heat transfer fluid comprises an ultra tall tower with the heat exchanger located along the tower.

15. The system of claim 14, wherein the means for ascending and descending the heat transfer fluid further comprises one or more supply lines and return lines connected between the heat exchanger and the thermal storage container for transferring the heat transfer fluid.

16. The system of claim 13 further comprising an aircraft configured to support the tower from above.

17. The system of claim 16, wherein the means for ascending and descending the heat transfer fluid comprises balloons filled with a gas lighter than air.

18. The system of claim 17, wherein the means for ascending and descending the heat transfer fluid comprises a main balloon and balloon clusters, wherein the main balloon is located at a topmost level of the tower.

19. The system of claim 18 wherein the means for ascending and descending the heat transfer fluid further comprises a kite attached on top of the main balloon.

20. The system of claim 17 wherein the balloon clusters include one or more balloons that surround the supply lines and return lines.

21. The system of claim 17 wherein the aircraft holding the thermal storage container is located between the main balloon and the balloon clusters.

22. The system of claim 21 further comprising supply lines and return lines connected between the heat exchanger and the thermal storage container for transferring the heat transfer fluid.

23. The system of claim 16 wherein the means for ascending and descending the heat transfer fluid comprises an aircraft, having a body or fuselage in the shape of an airfoil to which wings and horizontal and vertical stabilizers are attached to the aircraft.

24. The system of claim 23 further comprising a windmill propeller or ducted fan attached to the aircraft, wherein the windmill propeller or ducted fan is mechanically coupled to an electrical generator, whereby electricity is generated when the windmill propeller or ducted fan is turned by the wind

25. The system of claim 23, wherein an aircraft holding the thermal storage container is located underneath of a top aircraft.

26. The system of claim 25 wherein the means for ascending and descending the heat transfer fluid further comprises a kite attached on top of the top aircraft.

27. The system of claim 25 further comprising supply lines and return lines connected between the heat exchanger unit and the thermal storage container for transferring the heat transfer fluid.

28. The system of claim 12, wherein means for ascending and descending the heat transfer fluid comprises a freighter aircraft.

29. The system of claim 28, wherein the heat exchanger unit is built at a bottom of the freighter aircraft with pipes for circulating the fluid exposed to the atmosphere.

30. The system of claim 29, wherein the thermal storage container comprises palletized thermal storage container located on a main deck of the aircraft.

31. The system of claim 30, wherein the thermal storage container comprises palletized thermal storage container is fixed.

32. The system of claim 30, wherein the thermal storage container comprises palletized thermal storage container is removable from the aircraft.

33. The system of claim 30, wherein the thermal storage container comprises palletized thermal storage container is insulated by an insulating layer.

34. The system of claim 33, wherein the insulating layer comprise aerogel.

35. The system of claim 29, wherein the thermal storage container comprises a first thermal storage container located on a main deck of the freighter aircraft and a second thermal storage container located on a lower deck.

36. The system of claim 35, wherein the first and second thermal storage containers are insulted by an insulating layer.

37. The system of claim 36, wherein the insulating layer comprises an aerogel.

38. The system of claim 12 further comprising a generator having a shaft and a tether wound around a reel connected to the shaft, wherein an end of the tether is connected to the means for ascending the heat transfer fluid such that the reel turns the generator shaft as the heat transfer fluid ascends.

39. The system of claim 12, wherein the means for ascending or descending the heat transfer fluid comprises one or more balloons filled with a gas lighter than air.

40. The system of claim 39 wherein the means for ascending and descending the heat transfer fluid further comprises a kite.

41. The system of claim 39, wherein the means for ascending and descending the heat transfer fluid comprises a main balloon and one or more balloon clusters.

42. The system of claim 41 further comprising supply lines and return lines connected between the heat exchanger unit and the thermal storage container for transferring the heat transfer fluid, wherein the balloon clusters include one or more balloons that support the supply lines and return lines.

43. The system of claim 12, further comprising a windmill propeller or ducted fan attached to the means for ascending or descending the heat transfer fluid.

44. The system of claim 43 wherein the windmill propeller or ducted fan is mechanically coupled to an electrical generator, whereby electricity is generated when the windmill propeller or ducted fan is turned by the wind.