IP Library Granted Patent US 7,004,185
Granted Patent B2
US 7,004,185 · App. 10/217,741 · Granted Feb 28, 2006

Liquid loading techniques

Assignee: Kistler Aerospace Corporation
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Quick Facts
Patent No.
US 7,004,185
App. No.
10/217,741
Granted
Feb 28, 2006
Kind
B2
Abstract

An improved method for loading propellants into separate tanks on a reusable launch vehicle (RLV) uses three innovative methods. The liquid loading provides three liquid transfer methods, integrated and coordinated to provide less complicated loading and unloading operations, transfers, and cools and controls the liquids to provide a safe, cost effective solution to reusable vehicle tanking and de-tanking under commercial conditions. To insure the density of the propellant is maximized by cooling in a quick liquid loading environment, pre-cooling may be used.

Claims (40)

1. A method of transferring liquid comprising:

a. a elevation differential used to permit the weight of the liquid to move the liquid from one tank to another, and

b. a pressurant gas pressure differential used to push the liquid from one tank to another, and

c. a lower pressure in the pipe created by a pump,

whereby one or more of said combination is used in an integrated method to complete the transfer of mass.

2. The method of claim 1 wherein said elevation difference is controlled by a series of valves and pipes in an integrated and controlled manner.

3. The method of claim 1 wherein said elevation difference could include the pre-cooling of the liquid.

4. The method of claim 1 wherein said elevation difference could include a method of sensing and controlling the level of the liquid in the final tank.

5. The method of claim 1 wherein said pressurant gas pressure differential could include nitrogen.

6. The method of claim 1 wherein said pressurant gas pressure differential could include gaseous oxygen called GOX.

7. The method of claim 1 wherein said pressurant gas pressure differential could include helium.

8. The method of claim 1 wherein said transfer the liquid from one tank to another by a series of valves and pipes in an integrated and controlled manner.

9. The method of claim 1 wherein said moving liquid by elevation differential used to permit the weight of the liquid to move the liquid from one tank to another including a method of sensing and controlling the level of the liquid in the final tank.

10. The method of claim 1 wherein said lower pressure created by the pump is controlled by a method of sensing and controlling the level of the liquid in the final tank.

11. The method of claim 1 wherein said lower pressure created by a pressurant gas pressure differential used to push the liquid from one tank to another controlled by a method of sensing and controlling the level of the liquid in the final tank.

12. A method of sensing and controlling the level of the liquid flow into a tank comprising:

a. an inflow pipe permitting a liquid flow into a tank and,

b. a vent pipe permitting a liquid and gas flow from the tank, and

c. a visual method of sensing the liquid out flow the vent pipe, and

d. a method of calculating and setting the elevation of the vent pipe elevation precisely to accomplish a precise ullage or remaining gas volume in the top of the tank,

whereby said ullage control is integrated into the liquid transfer process.

13. The method of controlling the liquid flow into a tank of claim 12 wherein said method is improved by adding an coordinated series of valves and pipes in an integrated and controlled manner.

14. The method of controlling the liquid flow into a tank of claim 12 wherein said liquid is transferred with an elevation differential used to permit the weight of the liquid to move the liquid from one tank to another.

15. The method of controlling the liquid flow into a tank of claim 12 wherein said liquid is transferred with a pressurant gas pressure differential used to push the liquid from one tank to another.

16. The method of controlling the liquid flow into a tank of claim 12 wherein said liquid is transferred with a lower pressure in the pipe created by a pump.

17. A method of pre-cooling a transferring liquid to include:

a. cooling the liquid in the storage tank, and

b. bubbling cold helium as the ullage gas in the final tank to eliminate the collapse of the ullage volume, and

c. the loading of the liquid from the bottom of the final tank to prevent stagnation and gysering,

whereby said pre-cooling will be used in an used in an integrated method of completing the transfer of mass.

18. The volume of claim 17 wherein said elevation difference could include a method of sensing and controlling the level of the liquid in the final tank.

19. The volume of claim 17 wherein said liquid is transferred with a pressurant gas pressure differential used to push the liquid from one tank to another.

20. The volume of claim 17 wherein said liquid is transferred could include a method of creating a lower pressure in the pipe created by a pump.

21. A method of transferring liquid from a first tank to a second tank using one or more pipes, comprising:

an elevation differential between the first tank and the second tank to permit the weight of the liquid to move the liquid from the first tank to the second tank;

a pressurant gas pressure differential used to move the liquid from the first tank to the second tank; and

a pressure differential in the pipe coupling the first and second tanks created by a pump to move the liquid from the first tank to the second tank, whereby one or more of the elevation differential, the pressurant gas pressure differential and the lower pressure created by the pump is used in an integrated method to complete the transfer of liquid from the first tank to the second tank.

22. The method of claim 21 , further comprising moving the liquid from the second tank to the first tank using one or more of the combination of elevation differential, pressurant gas pressure differential and lower pressure created by the pump.

23. The method of claim 21 wherein the elevation differential is controlled by a series of valves and pipes in an integrated and controlled manner.

24. The method of claim 21 wherein the pressurant gas pressure differential is provided by a gas selected from a group comprising helium, nitrogen and GOX.

Assignments (4)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 12, 2013
From: BLUE SHIFT, LLC
To: BREAKTHROUGH FUTURES, LLC
Reel/Frame 031194/0558 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 11, 2013
From: SCHWITZER, MATTHEW R., MR.
To: BLUE SHIFT, LLC
Reel/Frame 031186/0596 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 9, 2004
From: MUELLER, GEORGE E.; LACKIE, WARREN K.; LIMERICK, CHARLES D.; FAGAN, DONALD L.; TOLSON, BILL A.
To: KISTLER AEROSPACE CORPORATION
Reel/Frame 015545/0917 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 13, 2002
From: MUELLER, GEORGE E.; LACKIE, WARREN K.; LIMERICK, CHARLES D.; FAGAN, DONALD L.; TOLSON, WILLIAM A.; TAYLOR, THOMAS C.
To: KISTLER AEROSPACE CORPORATION
Reel/Frame 013586/0641 →
Continuity (2)
Provisional Application 6031327700 · Aug 17, 2001
Related Publication 20030037819A1 · Feb 27, 2003