Method of gas expansion using liquefied gas expander and integrated Joule-Thomson valve
A cryogenic turbine expander system which consists essentially of a cryogenic liquid pressure vessel, and the vessel further accommodating a turbine expander, an internal bypass configuration, which are operable in parallel, a three-way valve to direct incoming high pressure liquefied gas flow to the turbine expander, or the internal bypass configuration, which further consists a Joule-Thomson valve, when the turbine expander is not operational.
1. A method of liquefied gas expansion, comprising:
providing a cryogenic turbine expander system, comprising:
an inlet pipe,
an outlet pipe, and
a pressure vessel connected to the inlet pipe and the outlet pipe containing a turbine expander, an internal bypass configuration operable in parallel with the turbine expander, and a three-way valve;
directing a high pressure liquefied gas flow through the inlet pipe to the pressure vessel;
flowing the high pressure liquefied gas flow through either the turbine expander or the internal bypass configuration, as selected by the three-way valve, to generate a low pressure liquefied gas flow; and
directing the low pressure liquefied gas flow from the pressure vessel to the outlet pipe.
2. The method of claim 1 , wherein the internal bypass configuration comprises a Joule-Thompson valve.
3. The method of claim 1 , wherein the liquefied gas is flammable.
4. The method of claim 3 , wherein the liquefied gas is selected from the group consisting of: natural gas, methane, propane, ammonia, ethylene.
5. The method of claim 1 , wherein the interior of the pressure vessel is maintained below 240 K.
6. The method of claim 1 , wherein the turbine expander is a constant speed liquefied gas expander.
7. The method of claim 1 , wherein the turbine expander is a variable speed liquefied gas expander.
8. The method of claim 1 , wherein the pressure vessel is made of stainless steel.
9. The method of claim 1 , wherein the three-way valve is configured to direct the high pressure liquefied gas flow through the internal bypass configuration only when the turbine expander is not operational.
10. The method of claim 1 , wherein the three-way valve is configured to direct all of the high pressure liquefied gas flow through the internal bypass configuration when the turbine expander is not operational.
11. The method of claim 1 , wherein the three-way valve is configured to direct a predetermined amount of the high pressure liquefied gas flow through the internal bypass configuration when the turbine expander is not operational at load.
12. The method of claim 1 , wherein the cryogenic turbine expander system further comprises an external bypass configuration.
13. The method of claim 12 , wherein the external bypass configuration further comprises connecting pipes and a Joule-Thompson valve.
14. A method of liquefied gas expansion, comprising:
providing a cryogenic turbine expander system, comprising:
an inlet pipe,
an outlet pipe,
a pressure vessel connected to the inlet pipe and the outlet pipe containing a turbine expander, an internal bypass configuration operable in parallel with the turbine expander, and a three-way valve, and
an external bypass configuration connected to the inlet pipe and the outlet pipe;
wherein the method further includes either,
directing a high pressure liquefied gas flow through the inlet pipe to the pressure vessel,
flowing the high pressure liquefied gas flow through either the turbine expander or the internal bypass configuration, as selected by the three-way valve, to generate a low pressure liquefied gas flow, and
directing the low pressure liquefied gas flow from the pressure vessel to the outlet pipe; or
directing the high pressure liquefied gas from the inlet pipe, through the external bypass configuration, and to the outlet pipe.
15. The method of claim 14 , wherein the external bypass configuration further comprises connecting pipes and a Joule-Thompson valve.
16. The method of claim 14 , wherein the step of directing the high pressure liquefied gas from the inlet pipe, through the external bypass configuration, and to the outlet pipe is only performed when both the turbine expander and the internal bypass configuration are not operational at the same time.
17. The method of claim 14 , wherein the step of directing the high pressure liquefied gas from the inlet pipe, through the external bypass configuration, and to the outlet pipe is performed when either the turbine expander or the internal bypass configuration are not operational.
18. The method of claim 14 , wherein the step of directing the high pressure liquefied gas from the inlet pipe, through the external bypass configuration, and to the outlet pipe includes directing all of the high pressure liquefied gas and is only performed when both the turbine expander and the internal bypass configuration are not operational at the same time.
19. The method of claim 1 , wherein the turbine expander comprises two separate cryogenic turbine expanders, operable in parallel, in series, or individually.
20. The method of claim 19 , wherein the two cryogenic turbo expanders are identical.
21. The method of claim 19 , wherein the two cryogenic turbo expanders are different.
22. The method of claim 19 , wherein the two cryogenic turbo expanders are mounted to an intermediate support plate.