Liquid impact pressure control methods and systems
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B64D-037/32
B63B-025/14
출원번호
US-0122515
(2009-10-12)
등록번호
US-8561631
(2013-10-22)
국제출원번호
PCT/US2009/060366
(2009-10-12)
§371/§102 date
20110404
(20110404)
국제공개번호
WO2010/059307
(2010-05-27)
발명자
/ 주소
Yung, Tin Woo
He, Haiping
Sandstrom, Robert E.
출원인 / 주소
ExxonMobil Upstream Research Company
대리인 / 주소
ExxonMobil Upstream Research Company Law Department
인용정보
피인용 횟수 :
3인용 특허 :
8
초록▼
The present invention discloses apparatuses, systems, and methods for controlling liquid impact pressure in liquid impact systems. The liquid impact systems include at least one gas and a liquid, the gas having a density (PG) and a polytropic index (κ) and the liquid having a density (PL). The metho
The present invention discloses apparatuses, systems, and methods for controlling liquid impact pressure in liquid impact systems. The liquid impact systems include at least one gas and a liquid, the gas having a density (PG) and a polytropic index (κ) and the liquid having a density (PL). The methods include the step of calculating a liquid impact load of the liquid on the object by determining a parameter Ψ for the system, wherein Ψ is defined as (PG/PL) (κ−1)/κ. The systems are also configured to utilize the parameter Ψ. The parameter Ψ may be adjusted to increase or reduce the liquid impact load on the system. Automatic, computer-implemented systems and methods may be used or implemented. These methods and systems may be useful in applications such as LNG shipping and loading/off-loading, fuel tank operation, manufacturing processes, vehicles dynamics, and combustion processes, among others.
대표청구항▼
1. A method of controlling a liquid-impact pressure on a solid body in a liquid impact system, comprising: providing a liquid impact system including a gas and a solid body, wherein ρG is a density of the gas, κ is a polytropic index of the gas, and ρL is a density of the liquid;calculating a parame
1. A method of controlling a liquid-impact pressure on a solid body in a liquid impact system, comprising: providing a liquid impact system including a gas and a solid body, wherein ρG is a density of the gas, κ is a polytropic index of the gas, and ρL is a density of the liquid;calculating a parameter Ψ for the system, wherein Ψ is defined as (ρG/ρL)(κ−1)/κ; andadjusting the liquid-impact pressure by changing the parameter Ψ for the system, wherein increasing the value of the parameter Ψ decreases the liquid-impact pressure and decreasing the value of the parameter Ψ increases the liquid-impact pressure. 2. The method of claim 1 wherein changing the parameter Ψ for the system includes changing the composition of the gas in the system. 3. The method of claim 1, wherein changing the parameter Ψ for the system includes a change selected from the group consisting of 1) changing the pressure of the gas in the system, 2) changing the temperature of the gas in the system, 3) changing the composition of the liquid in the system, and 4) any combination thereof. 4. The method of claim 2 or 3 wherein the changing of the parameter Ψ occurs during design of the liquid impact system. 5. The method of claim 2 or 3 wherein the changing of the parameter Ψ occurs during operation of the liquid impact system. 6. The method of claim 2, wherein the method is executed automatically by a programmable computer system. 7. The method of claim 2, wherein the solid body is selected from the group consisting of a container and a surface. 8. The method of claim 2 or 3, wherein the method is applied to a liquid impact system selected from the group consisting of: 1) a liquid storage container system, 2) a fuel container system, 3) a manufacturing process system, 4) a vehicle coming in contact with a fluid surface, 5) a combustion system, and 6) an ink jet printing system. 9. The method of claim 2, wherein the liquid is liquefied natural gas (LNG) in an LNG container and the gas is ullage gas in the LNG container. 10. The method of claim 9, wherein changing the parameter Ψ for the system comprises changing the composition of the ullage gas by increasing the amount of an enhancement gas in the system, wherein the enhancement gas is selected from the group of gasses consisting of helium, neon, nitrogen, methane, argon, and any combination thereof. 11. The method of claim 10, further comprising increasing a release valve pressure level on a release valve on the LNG container. 12. The method of claim 3, wherein the liquid is a jet of ink from an ink jet printer cartridge and the gas is surrounding gas around the jet of ink. 13. The method of claim 3, wherein the liquid-impact pressure is the force applied to an area of a solid surface in cooperation with the liquid impact system. 14. The method of claim 2, wherein the liquid is fuel in a fuel tank and the gas is ullage gas in the fuel tank. 15. The method of any one of claims 9 and 14, wherein changing the parameter Ψ for the system further includes changing the liquid fill level. 16. A method of optimizing a liquid impact pressure of a liquid on an object in a liquid impact system, comprising: a) determining an optimum liquid impact pressure of the liquid on the object;b) selecting an attribute consisting of at least one of a composition of the liquid, a composition of the gas, the temperature of the system, and a gaseous pressure of the liquid impact system;c) calculating a liquid impact pressure of the liquid on the object by determining a parameter Ψ for the system, wherein Ψ is defined as (ρG/ρL)(κ−1)/κ, wherein ρG is a density of the gas, κ is a polytropic index of the gas, and ρL is a density of the liquid;d) comparing the optimum pressure with the calculated pressure;e) selecting one of the following: i) if the calculated pressure is not substantially equal to the optimum pressure: adjusting at least one of the composition of the liquid, the composition of the gas, and a gaseous pressure of the liquid impact system, and repeating steps c)-e); orii) if the calculated pressure is substantially equal to the optimum pressure, selecting the composition of the liquid, the composition of the gas, and the gaseous pressure of the liquid impact system. 17. The method of claim 16, wherein changing the parameter Ψ for the system includes a change selected from the group consisting of 1) changing the pressure of the gas in the system, 2) changing the temperature of the gas in the system, 3) changing the composition of the gas in the system, 4) changing the composition of the liquid in the system, and 5) any combination thereof. 18. The method of claim 17, wherein the method is executed automatically by a programmable computer system. 19. The method of claim 18, wherein the object is selected from the group consisting of a container and a surface. 20. The method of claim 19, wherein the method is applied to a liquid impact system selected from the group consisting of: 1) a liquid storage container system, 2) a fuel container system, 3) a manufacturing process system, 4) a vehicle coming in contact with a fluid surface, 5) a combustion system, and 6) an ink jet printing system. 21. The method of claim 17, wherein the liquid is liquefied natural gas (LNG) in an LNG container and the gas is ullage gas in the LNG container. 22. The method of claim 21, wherein changing the parameter Ψ for the system comprises changing the composition of the ullage gas by increasing the amount of an enhancement gas in the system, wherein the enhancement gas is selected from the group of gasses consisting of helium, neon, nitrogen, methane, argon and any combination thereof. 23. The method of claim 21, further comprising increasing a release valve pressure level on a release valve on the LNG container. 24. A method of reducing a liquid impact pressure in a container, comprising: providing a liquid impact system, comprising: a liquid, a first gas, and a container having a liquid volume filled with the liquid, and an ullage volume substantially filled with the first gas, wherein the liquid has a density (ρL) and the gas has a density (ρG) and a polytropic index (κ);determining a parameter Ψ for the two-phase system, wherein the parameter Ψ is defined as (ρG/ρL)(κ−1)/κ, and wherein an increase in the parameter Ψ results in a decrease in the liquid-impact load on the container; andincreasing the parameter Ψ in the system, comprising a step selected from the group consisting of: increasing the pressure of the first gas in the container, replacing a portion of the first gas with a selected gas having a higher parameter Ψ, increasing the liquid volume in the container, decreasing a volume of boil-off gas, wherein the volume of boil-off gas is a result of boil-off from the liquid volume, and any combination thereof. 25. The method of claim 24, wherein the selected gas has a property selected from the group consisting of: a lower boil-off temperature than the liquid, inert, non-toxic, readily available, low solubility with the liquid, and any combination thereof. 26. The method of claim 24, wherein the liquid is liquefied natural gas (LNG). 27. The method of claim 26, wherein the selected gas is selected from the group of gasses consisting of helium, neon, nitrogen, pressurized methane, argon, and any combination thereof. 28. The method of claim 27, wherein the container is an LNG container selected from the group consisting of a membrane tank, a prismatic tank, and a spherical tank. 29. The method of claim 24, further comprising: transporting the liquid in the container;monitoring the parameter Ψ during the transporting step;determining if the parameter Ψ has decreased;increasing the parameter Ψ if the parameter Ψ has decreased. 30. The method of claim 24, further comprising: off-loading the liquid in the container;monitoring the parameter Ψ during the transporting step;determining if the parameter Ψ has decreased;increasing the parameter Ψ if the parameter Ψ has decreased. 31. The method of claim 24, further comprising: on-loading the liquid in the container;monitoring the parameter Ψ during the transporting step;determining if the parameter Ψ has decreased;increasing the parameter Ψ if the parameter Ψ has decreased. 32. The method of any one of claims 30 and 31, wherein the off-loading and on-loading steps occur at an off-shore location. 33. The method of claim 24, wherein the method is executed automatically by a programmable computer system. 34. A system for reducing a liquid impact load in a container, comprising: a liquid impact system, comprising:(i) a volume of liquid in a container, the liquid having at least a density (ρL);(ii) an ullage volume in the container containing at least an initial ullage gas, the initial ullage gas having at least a density (ρG) and a polytropic index (κ);a sensor system configured to determine at least the volume of liquid, the ullage volume, the liquid density (ρL), an ullage gas density (ρG), and an ullage gas polytropic index (κ);a calculator configured to calculate a parameter Ψ for the liquid impact system, wherein Ψ is defined as (ρG/ρL)(κ−1)/κ and an increase in the parameter Ψ results in a decrease in a liquid impact load in the container; anda controller configured to control at least one physical attribute of the liquid impact system to increase the value of the parameter Ψ. 35. The system of claim 34, further comprising a selector operatively connected to the controller, the selector configured to select a low-load ullage gas, wherein the low-load ullage gas is calculated to have a higher parameter Ψ than the ullage gas. 36. The system of claim 35, wherein the physical attributes of the liquid impact system are selected from the group consisting of: the volume of the ullage gas in the ullage volume, the pressure of the ullage gas in the container, the parameter Ψ of the ullage gas, the liquid volume in the container, a volume of boil-off gas, wherein the volume of boil-off gas is a result of boil-off from the liquid volume, and any combination thereof. 37. The system of claim 35, further comprising: an ullage gas storage tank in fluid communication with the container;an ullage gas pump for filling the container with one of the ullage gas and the low-load ullage gas. 38. The system of claim 34, wherein the calculator is an automated computing device and the controller is an automated control system.
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