Compression-evaporation system for liquefied gas

• US 7,406,830 B2
• Filed: 12/16/2005
• Issued: 08/05/2008
• Est. Priority Date: 12/17/2004
• Status: Expired due to Fees

• Current Assignee: Snecma (Safran SA)
• Original Assignee: Snecma (Safran SA)
• Inventors: Feger, Damien, Marchal, Noël, Lagnel, Olivier, Danguy, François, Valentian, Dominique
• Primary Examiner(s): DOERRLER, WILLIAM CHARLES
• Application Number:
  US11/305,367
• Publication Number:
  US 20060222523A1
• Time in Patent Office: 963 Days
• Field of Search: 62/502, 417/313, 606/71, 606/48
• US Class Current: 62/50.2
• CPC Class Codes: F17C 2221/033 Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
• CPC Class Codes: F17C 2223/0161 cryogenic, e.g. LNG, GNL, PLNG
• CPC Class Codes: F17C 2223/033 Small pressure, e.g. for liquefied gas
• CPC Class Codes: F17C 2225/0123 gaseous, e.g. CNG, GNC
• CPC Class Codes: F17C 2225/036 Very high pressure, i.e. above 80 bars
• CPC Class Codes: F17C 2227/0142 with specified pump type, e.g. piston or impulsive type
• CPC Class Codes: F17C 2227/0157 Compressors
• CPC Class Codes: F17C 2227/0316 Water heating
• CPC Class Codes: F17C 2227/0393 using a vaporiser
• CPC Class Codes: F17C 2260/046 Enhancing energy recovery
• CPC Class Codes: F17C 2265/05 Regasification
• CPC Class Codes: F17C 2265/068 Distribution pipeline networks
• CPC Class Codes: F17C 2270/0136 Terminals
• CPC Class Codes: F17C 7/04 with change of state, e.g. vaporisation
• CPC Class Codes: Y02E 20/14 Combined heat and power generation [CHP]

Abstract

The compressor-evaporator system for liquefied gas contained in a tank comprises, in addition to a deice for evaporation by heat exchange with a liquid and devices for conditioning and transferring gas to a pipeline, a motor-driven turbopump comprising a rotary assembly of high bending stiffness on a common shaft line, with at least one high pressure pump, a turbine, and a central electrical machine capable of being used in motor mode or in generator mode. The rotary assembly of the motor-driven turbopump is adapted to present a high speed of rotation, greater than 12,000 rpm, while remaining outside ranges for exciting critical speeds in rotation. All of the internal portions of the motor-driven turbopump are immersed in a cryogenic fluid that is the same as the liquefied gas contained in the tank. The internal cavities of the motor-driven turbopump that are under different thermodynamic conditions are separated by contactless dynamic seals. Electronic power circuits connected to an electricity network control the central electrical machine in motor mode or generator mode.

Claims

1. A compressor-evaporator system for liquefied gas contained in a tank, the system comprising extraction and pump means for extracting and delivering liquefied gas under low pressure outside the tank, high pressure pump means, evaporator means operating by heat exchange with a liquid, and means for conditioning and transferring gas to a gas pipeline,

the system comprising at least one turbomachine constituted by a motor-driven turbopump comprising a rotary assembly having very high bending stiffness on a common shaft line, with at least one high pressure pump comprising an axial suction stage and at least one centrifugal wheel, a turbine, and a central electrical machine capable of being used in motor mode or in generator mode and situated between the high pressure pump and the turbine, said motor-driven turbopump being arranged in compact manner inside a rigid casing that presents static seals only with the surrounding medium, the rotary assembly of the motor-driven turbopump being adapted to present a high speed of rotation, greater than 12,000 rpm, while remaining outside the excitation ranges of critical speeds of rotation, all of the internal portions of the motor-driven turbopump being immersed in a cryogenic fluid that is the same as the liquefied gas contained in the tank, the internal cavities of the motor-driven turbopump that are under different thermodynamic conditions being separated by contactless dynamic seals, and electronic power circuits connected to an electricity network serving to control the central electrical machine in motor mode or generator mode.

2. A system according to claim 1, wherein the speed of rotation of the rotary assembly of the motor-driven turbopump lies in the range 20,000 rpm to 40,000 rpm.

3. A system according to claim 1, including a first heat exchanger and evaporator interposed between the high pressure pump and the turbine to compress and to evaporate the liquefied gas used as the working fluid in the motor-driven turbopump.

4. A system according to claim 3, wherein the high pressure pump means comprise exclusively the high pressure pump of the motor-driven turbopump connected in series between the tank and the pipeline.

5. A system according to claim 3, wherein the means for evaporation by heat exchange with a liquid comprise said first heat exchanger and evaporator interposed between the high pressure pump and the turbine, and a second heat exchanger and evaporator disposed between the turbine and the pipeline to be fed.

6. A system according to claim 1, further comprising a buffer volume disposed at the inlet to the high pressure pump of the motor-driven turbopump.

7. A system according to claim 3, further comprising a buffer volume disposed at the inlet to the high pressure pump of the motor-driven turbopump, a condenser with a first circuit interposed between the outlet of the high pressure pump of the motor-driven turbopump and the first heat exchanger and evaporator, and a second circuit interposed between the outlet of the turbine of the motor-driven turbopump and the buffer volume, the second circuit being in heat exchange with the first circuit to reliquefy the gas leaving said turbine.

8. A system according to claim 6, wherein the high pressure pump means comprise a motor-driven pump having its inlet connected to said extraction and pump means, and having its outlet connected to a first circuit of a condenser, the outlet from said first circuit being connected to the inlet of a heat exchanger and evaporator whose outlet is connected to said pipeline, wherein said buffer volume is in a branch connection connected to the outlet of said motor-driven pump, and wherein the outlet from the turbine of the motor-driven turbopump is connected to the inlet of a second circuit of the condenser, the outlet from said second circuit being connected to said buffer volume, the second circuit being in heat exchange with the first circuit to reliquefy the gas leaving said turbine.

9. A system according to claim 1, wherein the means for evaporation by heat exchange with a liquid comprise means for introducing and evacuating a liquid constituted by water at a temperature that is not less than ambient temperature.

10. A system according to claim 3, wherein the first heat exchanger and evaporator interposed between the high pressure pump and the turbine includes means for introducing and evacuating a liquid constituted by water at a temperature that is not less than ambient temperature.

11. A system according to claim 1, wherein the motor-driven turbopump includes hydrostatic fluid bearings fed with a fluid in the liquid and compressed state that is the same as the fluid available from the outlet of the high pressure pump of the motor-driven turbopump.

12. A system according to claim 11, wherein the motor-driven turbopump includes an active hydraulic device for balancing axial forces, which device is fed with a fluid in the liquid and compressed state that is the same as the fluid available from the outlet of the high pressure pump of the motor-driven turbopump.

13. A system according to claim 11, wherein the motor-driven turbopump includes an axial fluid abutment fed with a fluid in the liquid and compressed state that is the same as the fluid available from the outlet of the high pressure pump of the motor-driven turbopump.

14. A system according to claim 1, wherein the motor-driven turbopump includes active magnetic bearings.

15. A system according to claim 14, wherein the motor-driven turbopump includes a magnetic axial abutment.

16. A system according to claim 1, wherein the motor-driven turbopump includes high speed ball bearings with ceramic balls.

17. A system according to claim 1, wherein the turbine of the motor-driven turbopump comprises a rotor of high-strength titanium alloy of the TA6 V ELI or TA5 E ELI type or of light alloy of the aluminum-lithium type.

18. A system according to claim 1, wherein the high pressure pump of the motor-driven turbopump comprises one or more impellers of high-strength titanium alloy of the TA6 V ELI or TA5 E ELI type or of light alloy of the aluminum-lithium type.

19. A system according to claim 1, wherein the central electrical machine of the motor-driven turbopump comprises a permanent magnet rotor, the electronic power circuit delivering power at a frequency synchronous with the speed of rotation and at variable voltage in motor mode, and converting the variable voltage that is created in generator mode into a rectified constant voltage.

20. A system according to claim 1, wherein the central electrical machine of the motor-driven turbopump has a one-piece rotor with an excitation coil fed by a rotary transformer and a rectifier diode bridge for regulating the excitation of the electrical machine and for providing a constant voltage in generator mode and controlled torque in motor mode.

21. A system according to claim 1, wherein the central electrical machine of the motor-driven turbopump includes a squirrel-cage rotor, the electronic power circuit delivering power at variable voltage and frequency in motor mode and converting the variable voltage that is created in generator mode into a rectified constant voltage.

22. A system according to claim 1, the system being applied to a liquefied gas of the liquefied natural gas type.